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NASA CONTRACTOR REPORT e EXPERIMENTAL INVESTIGATION OF A DOUBLE-DIFFUSED MOS STRUCTURE €9'. C. Lin und J. L. Hulsor Prepared by WESTINGHOUSE DEFENSE AND, ELECTRONIC SYSTEMS CENTER Baltimore, Md. for LangleyResearchCenter NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. MAY 1976 https://ntrs.nasa.gov/search.jsp?R=19760017374 2020-06-16T05:06:53+00:00Z

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Page 1: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

N A S A C O N T R A C T O R

R E P O R T

e

EXPERIMENTAL INVESTIGATION OF A DOUBLE-DIFFUSED MOS STRUCTURE

€9'. C. Lin und J. L. Hulsor

Prepared by WESTINGHOUSE DEFENSE AND, ELECTRONIC SYSTEMS CENTER

Baltimore, Md. for Langley Research Center

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. M A Y 1976

https://ntrs.nasa.gov/search.jsp?R=19760017374 2020-06-16T05:06:53+00:00Z

Page 2: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

' TECH LIBRARY KAFB, NM

1. Report No. 3. Recipient's C a t a l o g No. 2. Government Accession No.

NASA CR-2620 4. Title and Subtitle 5. Repart Date

May 1976 Eqerimeni;al Invest igat ion of a Double-Diffused MOS St ruc ture 6. PerForming Organization Code

"" . - .~ ." " . . - . . - . 7. Authods) 8. Performing Organlzation Report No.

H. C. Lin and J. L. Halsor 10. Work Unit No.

9. Performing Organization Name and Address 506-1&1-03 (~4488) Westinghouse Defense and Electronic Systems Center Systems Development Division Advanced Technoloav Laboratories I 11. Contract or' Grant No.

NAS1-12533 Baltimore, Maryland

I"

13. Type of Report and Period Covered

'2. Sponsoring Agency Name and Address Contractor 's Final Report Nat iona l Aeronaut ics & Space A d m i n i s t r a t i o n 14. Sponsoring Agency Code Washington, DC 20546

r5. Supplementary Notes

Langley Technical Monitor: Harry F. Benz

Final Report

16. Abstract Doublediffused MOS (DMOS) t rans is tors a re capable o f high-speed operation because of the

reduced channel length that resul ts when successive n- and ptyp di f fus ions a r e done through the same source window. Th i s e f f ec t ive ly r e su l t s i n a channel length that i s comparable t o t h e base width of a double-diffused bipolar t ransis tor (approx. 0.5 micrometer instead of several micrometers which i s t y p i c a l of standard MOSFET geometry). In addition, for optimwn high frequency performance, it i s d e s i r a b l e t o minimize a r e a and paras i t ic capac i tance assoc ia ted with s tandard metal gate e lectrodes. In this report , se l f -a l ined polysi l icon gate technology i s a p p l i e d t o t h e DMOS cons t ruc t ion in a manner that re ta ins processing s implici ty and effec- t ive ly e l imina tes paras i t ic over lap capac i tance because o f the se l fa l in ing fea ture .

a re in tegra ted . The r a t io l e s s f ea tu re r e su l t s i n sma l l e r dimension load devices, allowing for higher densi ty integrat ion with no increase in the processing complexity of standard MOS technology.

performance and to ve r i fy t he an t i c ipa t ed bene f i t s . The propagation time-power d i s s i p a t i o n prc- duct and process related parameters were measured and evaluated.

This report includes (1) d e t a i l s of the process; (2) t e s t d a t a and design detai ls for t h e DMOS t r ans i s to r , t he l oad dev ice , t he i nve r t e r , t he r i ng o sc i l l a to r , and a sh i f t r eg i s t e r w i th a novel tapered geometry for the output stages; and (3) an analyt ical t reatment of t h e e f f e c t o f t h e d i s t r i b u t e d s i l i c o n g a t e r e s i s t a n c e and capacitance on the speed of DMOS t r a n s i s t o r s .

In th i s repor t deple t ion mode load devices with the same dimensions as t h e DMOS t r a n s i s t o r s

A number of inverters connected as r ing osci l la tors were used as a v e h i c l e t o t e s t t h e

17. Key Words (Suggested by Author(s)) 18. Distribution Statement

Metal Oxide Semiconductor Transistors

F ie ld Shie ld Double-Diffused

U n c l a s s i f i e d - U n l i m i t e d

Subject Category 33 ~

19. Security Classif. (of this report1 22. Price' 21. NO. of Pager 20. Security Classif. (of this p a g e )

Unclassif ied $4.75 78 Unclassif ied ~~ ~~~~~

For sale by the National Technical Information Service, Springfield, Virginia 221 6 1

Page 3: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)
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CONTENTS Page

. . . . . . . 1 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . SILICON GATE DOUBLE-DIFFUSED MOS TRANSISTORS . . . . . . INTEGRATED DOUBLE-DIFFUSED MOS STRUCTURE . . . . . . . . ANALYSIS OF DMOS TRANSISTORS . . . . . . . . . . . . . . DMOS INVERTER . . . . . . . . . . . . . . . . . . . . . .

Switching Transistor Design Considerations . . . . . Load Device Design Considerations . . . . . . . . . .

EFFECT OF SILICON GATE RESISTANCE ON THE FREQUENCY RESPONSE OF MOS TRANSISTORS . . . . . . . . . . . . . . . . . . .

. . . . . . . 2

. . . . . . . 3

. . . . . . . 5

. . . . . . . 7

. . . . . . . 11

. . . . . . . 14

. . . . . . . 17 Silicon Gate as Distributed RC Network . . . . . . . . . . . . . . 18 Frequency.Response of the Distributed RC Network . . . . . . . . . 20 Time Constant of the Silicon Gate . . . . . . . . . . . . . . . . . 21 Characteristics of the Silicon Gate Uniform Channel MOS Transistor . . . . . . . . . . . . . . . . . . . . . . . . . 24

Characteristics of DMOS Transistors . . . . . . . . . . . . . . . . 26 DMOS RING OSCILLATOR . . . . . . . . . . . . . . . . . . . . . . . . . . 31 DMOS SHIFT REGISTER . . . . . . . . . . . . . . . . . . . . . . . . . . 34 AN OPTIMIZED OUTPUT STAGE FOR MOS INTEGRATED CIRCUITS . . . . . . . . . 34

Output Stage Design Principles . . . . . . . . . . . . . . . . . . 36 Area Optimization . . . . . . . . . . . . . . . . . . . . . . . . . 39

Optimum Stage Design . . . . . . . . . . . . . . . . . . . . . . . 40 MASK DESIGN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 FABRICATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55

EXPERIMENTAL RESULTS . . . . . . . . . . . . . . . . . . . . . . . . . . 58

Typical Test Transistor Characteristics . . . . . . . . . . . . . 58

Inverter Characteristics . . . . . . . . . . . . . . . . . . . . . 60

Effect of Silicon Gate Resistance . . . . . . . . . . . . . . . . . 60 Ring Oscillator Performance . . . . . . . . . . . . . . . . . . . . 66

SUMMARY AND CONCLUSIONS . . . . . . . . . . . . . . . . . . . . . . . . 69

iii

I

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.. . ._ ............. .

Page

APPENDIX . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 72 Frequency Response of Distributed RC Lines . . . . . . . . . . . . 72 Transient Response . . . . . . . . . . . . . . . . . . . . . . . . 72

REFEmNCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 74

i V

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I h

FIGURES

Page

1. 2.

3.

4. 5. 6.

7.

a. 9. 10.

11.

12.

13.

14.

15.

16.

17.

18.

19.

DMOS Structure -. . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Computed Drain Output DMOS Characteristics Velocity Saturating . . . . . . . . . . . . . . . . . . . . . . . 8 Computed Drain Output DMOS Characteristics Velocity not Saturating < . . . . . . . . . . . . . . . . . . . . . 9 Computed Drain Output MOS Characteristics . . . . . . . . . . . . . 10

DMOSInverter . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

Threshold Voltage as Function of Substrate Concentration . . . . . 16

Silicon Gate MOS Transistor . . . . . . . . . . . . . . . . . . . 19 Distributed RC Network . . . . . . . . . . . . . . . . . . . . . . . 19

Equivalent Circuif of a Silicon Gate MOS Transistor . . . . . . 19

Small-signal Response of Distributed RC Network Amplitude Response in dB vs. Normalized Frequency with Position as a Parameter . . . . . . . . . . . . . . . . . 22

Small-signal Response of Distributed RC Network Phase Response in Degrees VS. Normalized Frequency with Position as a Parameter . . . . . . . . . . . . . . . . . . 23

Transient Response of Distributed RC Network. Normalized Gate Voltage vs . Normalized Time with Position as a Parameter. (Computed results in solid line; simulated results in dashed lines.) . . . . . . . . . . . . 25

Computed Response of Silicon Gate MOS Transistor (Load Resistance fi: 0) . . . . . . . . . . . . . . . . . . . . . . 27 Computed Response of Silicon Gate MOS Transistor (Load Resistance ~ 0) . . . . . . . . . . . . . . . . . . . . . . 28 Computed Response of a Loaded Silicon Gate MOS Transistor (Load Resistance = 100 Ohms) . . . . . . . . . . . . . . . . . . . 29 Equivalent Circuit of Silicon Gate DMOS Transistor . . . . . . . . 30 Computer Response of Silicon Gate DMOS Transistor (Load Resistance = 100 Ohms) . . . . . . . . . . . . . . . . . . . 32

Inverter Layout for Ring Oscillator . . . . . . . . . . . . . . . . 33 Shift Register . . . . . . . . . . . . . . . . . . . . . . . . . . 35 (a) Schematic Diagram (b) Clock Timing Diagram

Page 7: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

Page 2 0 . 21 . 22 . 23 . 24 . 25 . 26 . 27 . 28 . 29 . 3 0 . 31 . 32 . 33 . 34 . 35 . 36 . 37 . 38 . 39 . 40 . 41 . 42 .

Cascade MOS Stages . . . . . . . . . . . . . . . . . . . . . . . . 38 Normalized Propagation Delay. Normalized Area. and Figure of Merit F. vs . Number of Stages for M = 100. K = 2 . . . . . . . . . 41

Normalized Propagation Delay and Area-Propagation Delay Square Product. F. vs . Number of Stages . . . . . . . . . . . . . . 43

Optimum Number of Enlarged Output Stages for Different Load to Node Capacitance Ratios . . . . . . . . . . . . . . . . . 45 Miniuwm Propagation Delay Obtainable for a Given Area and a Fixed Load to Node Ratio of 100 . . . . . . . . . . . . . . . . . 46

Composite Layout of the Shift Register Cell . . . . . . . . . . . . 47

Overall Interconnection Mask . . . . . . . . . . . . . . . . . . . 48

P- Channel-Stop Diffusion Mask . . . . . . . . . . . . . . . . . . 4 9

N Diffusion Mask . . . . . . . . . . . . . . . . . . . . . . . . 50

P Diffusion Mask . . . . . . . . . . . . . . . . . . . . . . . . 51

Silicon Etch Mask . . . . . . . . . . . . . . . . . . . . . . . . 52

+

Contact Mask . . . . . . . . . . . . . . . . . . . . . . . . . . . 53

Interconnection Mask . . . . . . . . . . . . . . . . . . . . . . . 54

Si Gate DMOS IC Structure . . . . . . . . . . . . . . . . . . . . . 56

DMOS Integrated Inverter . . . . . . . . . . . . . . . . . . . . . 59

Transistor V-I Characteristic of DMOS Inverter . . . . . . . . . . 61 Effect of Substrate Bias on Load Device Characteristics . . . . . . 62

DMOS Inverter Characteristics in 5V Operation . . . . . . . . . . 6 3

DMOS Inverter Characteristics in 3V Operation . . . . . . . . . . 6 4

Photomicrograph of DMOS Transistor Showing 2 Gate Contacts . . . . . 65

Ring Oscillator . . . . . . . . . . . . . . . . . . . . . . . . . 67

Ring Oscillation . . . . . . . . . . . . . . . . . . . . . . . . . 68

Propagation Time and Power Dissipation of DMOS Inverters . . . . . . 70

vi

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I

MPERIMENTAL INVESTIGATION OF A DOUELE-DIFFUSED

SHIELDED METAL-OXIDE SEMICONDUCTOR (DMOS) STRUCTURE

By H. C. Lin and J. L. Halsor Westinghouse Electric Corporation Advanced Technology Laboratories

INTRODUCTION

Double-diffuse2 MOS (DMOS) transistors are capable of high-speed operation

because of the reduced channel length that results when successive n and p-type

diffusions are done through the same source window. This effectively results

in a channel length that is comparable to the base width of a double-diffused

bipolar transistor (% 0.5 micrometer instead of several micrometers which is

typical of standard MOSFET geometry). In addition, for optimum high-frequency

performance, it is desirable to minimize area and parasitic capacitance asso-

ciated with s,tandard metal gate electrodes. In this work, we developed and

applied self-aligned polysilicon gate technology to the DMOS construction in a

manner that retains processing simplicity and effectively eliminates parasitic

overlap capacitance because of the self-aligning feature.

In this work, we also designed and developed integrated depletion mode

load devices with the same dimensions as the DMOS transistors. This ratio-

less feature results in smaller dimension load devices allowing for higher

density integration with no increase in the processing complexity of standard MOS techno 1 ogy .

A s a vehicle to test the performance and to verify the anticipated bene- fits, we designed and fabricated a number of inverters connected as ring

oscillators. The propagation time-power dissipation product and process

related parameters were measured and evaluated.

In the course of the investigation, a number of other technical advances

were also made and published. This report is a description of these advances

Page 9: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

--- - I and includes (1) d e t a i l s of the process; (2) test data and des ign de ta i l s for

the DMOS t ransis tor , the load device, the inverter , the r ing osci l la tor , and a

sh i f t r eg i s t e r w i th a novel tapered geometry for the output stages; and (3) an

analytical treatment of t he e f f ec t of the d i s t r ibu ted s i l i con ga te res i s tance

and capacitance on the speed of DMOS t rans is tors .

SILICON GATE DOUBLE-DIFFUSED MOS TRANSISTORS

The progress of electron devices has been earmrked with ever increasing

frequency performance. In the realm of semiconductor amplifying devices, the

f ie ld has been dominated by bipolar t ransis tors . The f i e ld e f f ec t t r ans i s to r s

have generally been conceded as infer ior to the bipolar t ransis tor in high-

frequency response.

Let us examine the reason for th i s in fer ior i ty : One f igure of merit of a

high-frequency electron device i s the gain-bandwidth product GB (=g /2& ),

where g i s the transconductance and C i s the input capacitance. For a bi-

po lar t rans is tor (where the junction capacitance can be made negl igible by

small geometry)

m i n

m i n

where p i s the minority carrier mobili ty, W i s the base width, k i s Boltzmann's

constant, T i s the absolute temperature, and q i s the electronic charge. b

For a f i e l d e f f e c t t r a n s i s t o r

where L i s the channel length, Vp i s the pinchoff voltage (voltage where drain

cur ren t sa tura tes ) , and VG i s the gate voltage.

In ordinary operation, the magnitude of kT/q i s only a f rac t ion of a

vol t . Hence

Page 10: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

The inequal i ty should favor the f ie ld e f fec t t rans is tors for h igher ga in band-

width product. However, in s ta te -of - the-ar t FET's, the channel length L i s

much larger than the base width of bipolar t ransis tors because the la teral

L-dimension i s determined by photolithographical techniques, while W i s con-

t ro l l ed i n t he f r ac t iona l micrometer range by diffusion techniques. In

prac t ice , W can be well controlled in the fractional micrometer range while L

can only be controlled to one order of magnitude higher. Since the gain band-

width product has a reciprocal square-law dependence on these dimensions, the

ne t r e su l t i s tha t b ipolar t rans is tors a re fas te r than f ie ld e f fec t t rans is tors

by two orders of magnitude.

b

b

Another reason for a lower limit to the channel length i s the voltage

punch-through ef fec t resu l t ing from the widening of the deplet ion layer when

the drain vol tage becomes appreciable. This punch-through e f f ec t i s p a r t i -

cu la r ly pronounced f o r FET's with low background impurity concentration. If

means can be devised t o reduce L and to grade the background channel substrate

doping concentration along the channel to reduce the punch-through effect, the

high frequency capabilities for FET's can be significantly extended.

A narrow channel length and a higher punch-through voltage can be achieved

by double diffusion in much the same way as the convent ional bipolar t ransis tor .

Such approaches have been pursued by Tarui, Cauge , and others. However, the

structures described do not have a s i l i con ga te . Nor do they contain an

e lec t ros ta t ic sh ie ld to p revent f ie ld invers ion in the a reas ou ts ide the ga tes .

'Ilhis work i s an a t tempt to fabr ica te an in tegra ted c i rcu i t us ing s i l i con ga te

double-diffused transistors with a f ie ld shield to prevent surface inversion

between devices.

I 2

MTEGRATED DOUBLE-DIFFUSED MOS STRUCTURE

A cross-section of a double-diffused N-channel MOS s t ruc ture i s shown i n

f igure 1. The substrate can be e i t h e r p or n-type. The window defining the

source region i s diffused sequentially with both an n-type dopant and a lower

concentration p-type dopant. The window defining the drain region i s diffused

with only n-type dopant as i n conventional transistors. With double diffusion,

the channel i s the p-type diffused region and the length can be made very short,

3

Page 11: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

Figure I. DMOS Structure

4

Page 12: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

say less than l p m . A t the same time, because of the diffusion, the p-type

doping i s more concentrated toward the source and thus reduces the punch-

through effect.

ANALYSIS OF DMOS TRANSISTORS

I n our previous work, we analyzed the double-diffused MOS t r a n s i s t o r a s a n

idea l i zed i n t ha t a zero res is t ivi ty metal gate was used and no

ve loc i ty sa tura t ion e f fec t was considered. When the effective channel i s very

short ( in the micrometer o r submicrometer range), the high electric field along

the channel can saturate the carrier velocity. In our approach of using a

s i l i con ga te , the nonzero res i s t iv i ty of the polycrystal l ine s i l icon gate can

adversely affect the frequency response of the t rans is tor . A more detai led

analysis i s made on t h i s e f f e c t .

For the analysis of the DMOS transistor, the device can be divided into a

number of incremental t ransis tors of variable threshold voltage in much the

same way an an electr ical t ransmission l ine. The basic equation w e used i n

our, previous work is:

ID - - VCG [V, - V,(X) - V ( X ) l dV

where p = mobility

CG = gate capacitance

L = total channel length

VG = gate vo l tage ( re la t ive to subs t ra te )

VT(x) = threshold a t a distance x from the edge of source

V(x) = voltage of the channel a t any point x 4 The r e s u l t s of our computation, which were reported in our previous report

as wel l as an IEEE publication3, were arrived at by considering a constant

mobili ty. If the mobili t ies are l inearly dependent on e l ec t r i c f i e ld , t he cu r -

rent i s less than expected a t high fields. For a conventional MOS t r ans i s to r ,

the current tends to depart from the square-law relationship and become more

l inear ized. Such an effect i s taken into account in cer ta in models and 5

Page 13: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

incorporated in some computer-aided design programs. 3i.

The characteristic of a DMOS transistor can be computed by connecting a

number of incremental transistors of different threshold voltages in series. The number of divisions depends on the accuracy desired. If too many divisions

are used, it is uneconomical from the standpoint of computation time. Ne found

that five divisions were sufficient to give a reasonable accuracy.

The computer-aided

transistor used in this

NApiE - VTO Threshold UB Low Field

design program used is M-SINC. The model of an MOS program should contain the following information

*

DEFAULT PARAMETER CONDITION

Voltage with Source Grounded 0 Mobility Value 450

ECRIT Critical Field 6 .E4 c1 Empirical Hatching Coefficient for Mobility 0 COX Oxide Capacitance per sq. cm. 3E-8

DNB Doping Concentration in Substrate 1E15

X J D (XJS) Overlap of Drain Length Under Gate (Source) 0 GOS Choice of Depletion Equation 0

0 - No Channel Length Depletion 1 - Square Root Dependence Thick Oxide Device 2 - Fringing Field Thin Oxide Device

First Fringing Field Coefficient

Second Fringing Field Coefficient Saturation Current of Junction Diode

Parameter Definition Temperature The,electric field is considered in the term

cul cu2

css TEMP

0.2

0.6

1E-14

3 00

where Es is the electric field and E is the critical electric field above which the mobility is affected. If the electric field effect is neglected,

so

* M-SINC Computer-Aided Analysis Program developed by Stanford University.

" .. .

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the exponent C1 is set at zero. For practical MOS transistors C1 = 0.15 for p-channel devices C1 = 0.35 for n-channel devices.

The results of the computation are shwn in figure 2, and the results for no velocity saturation (C = 0) are shown in figure 3. Generally, the effect of velocity saturation is to reduce the drain current. "he reduction is greater at higher gate voltages. This effect also makes the transconductance constant as compared to conventional MOS transistors whose transconductance increases linearly with increasing gate voltage.

1

In our previous analy~is,~ it was pointed out that the DMOS transistor itself has a tendency toward constant transconductance even without considering carrier velocity saturation. This will be brought about by the following argu- ment. The DMOS transistor can be considered to be an enhancement mode short channel transistor in series with a depletion mode transistor with a longer channel. The channel resistance is the series resistance of the two transis- tors and is then dominated by the higher of the two resistances. At low gate voltages, the enhancement mode transistor with high transconductance dominates the characteristics. At high gate voltages, the enhancement mode transistor has lower resistance, and the lower transconductance of the depletion mode transistor dominates the characteristics. The net result is to make the com- posite transconductance nearly constant. Thus, the DMOS transistor has two

effects tending to lower the transconductance at high gate voltage and to make

it more nearly constant. The computer results of a transistor with uniform background is shown in

figure 4. Note that at low gate voltages, the transconductance of a DMOS

transistor is much greater than that of a conventional uniform background MOS

transistor. However, at high gate voltages the superiority becomes less pro- nounced because of the linearization of the TlMOS characteristics. For this reason, it is most advantageous to use the DMOS integrated circuit for low-

voltage operation.

DMOS INVERTER

The DMOS transistor can be used in conjunction with a depletion-mode

7

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I I

I

* 4

I + * + * * + * w G = N * * * * * ................................... 1 I * I I

+ * I I I I * I

1 I I * *

' I * I *

00 .................... + ...... * : ........................... I ................... + I * * I I I I

I I 4

I *; * * - I I . ! * 4 . + * * - * * ! * * * + . * * * * ! v ~ ~

* * * I 4 4 * * I G

I I 20 : ........ 3.; *:.* . A................ : ......................................

& t 1 * * * - * I I I

1 I I I I

I * I I I t

I ** I I 1 I ......................................................... I ................... t

1 2 3 4v

Drain Voltage, v

Figure 2. Computed Drain Output DMOS Characteristics Velocity Saturating

8

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v e 5V 1Wl .................. 8 . .................. I .................. 1 .................. 1

I 1 I I 1 I 1 I 1

I I I 0 . 1

I 1 + I I

* * + V d V + * * * I G

160 I' ..................................... I ................ :. ................... , * I I * I + I I

1 I I I I

I I + I I I

I I 1 . I I

140 ................... I ................. .. * .............. I .................. I

1 I I * I I 1 I 1 I

1 I I I I I 1 . 1 I

4

120 .................................. :... ................... I ................... I I * I 1- I

1 I I 1 I

I , I 1 I

I I I I +

5 100 .......................................................................... U

B

r r * * r . . * * . V ~ ~ y I * . . I * G . *

2 I I I I

+ I + I * * I I

C I

n

4 2 80 ................................ * .: ....................................... . a 1 I +

I I

I * 1 I I I

I I . I 1 I

60 ............................................................................. I * I 1 I

I * 4 I I I

I .+ I I I

I I . . I I I

I . I I I 1

4 * I I I I

* * . .

20 I ..... ' C .. ...... 1 .................. I .................. , .................. * * I I I I I

I . I I I I

1 0 1 I I I

I * 1 I I I ................... I .................. I .................. , .......... "i. .... I 1 2 3 4

Drnin Volr.tge. v

Figure 3. Computed Drain Output DMOS Characteristics Velocity not Saturating

9

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- .......... I

....................................... ...t .............. I .................. 1 I I I 1 I I I I I I VG"SV ' * . * - * * * I I 1

160 ........................................................................... * l " - 1 I I I I I I I I I I 1 I I I I I I I I

140 ....................................... + .*, ................................. I

I I I I

1 I I 1 I

1 I I I I

1 I I I

120 ............................ ......" .........................................

.

*

I I 1 I I I I I I I

I r I I I

I I I I I

100 ......... ................................................ I .................. I I I

I

I G v =4v I *

* * * * * * . + * * * * * * * * I I * *

I I I

I I * * I I

I

I BO ................... I ............ :. ....................... I .................. I ' *

I + I I

I I I

I I + I I I

I I . I 1 I

60 ,..........,*.-.'...I, ................................... I .................. I I I I I I I I I I

I I I I

I * I I I I

40 ......................................................................... . . . . . . . . . . . . . . . . . . . . . . . . VG33V

* I

I

I +

1 * I

I

I - * - I I I I

I * I I I 1

20 ....... *..* ............................................ I .................. I I I I I I *

1 ..* * - . * * ~ * . * - * ~ * . * - * . - * - * - * * * * - * . * I I 1

I . I I I I ......................................................... I .................. I 1 2 3 4

* * ' vc=2v -.e

Drain Voltage, v

Figure 4 . Computed Drain Output MOS Characteristics

I O

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transistor as an inverter as shown in figure 5. The depletion mode transistor

is then used as a load device. The advantages of a depletion-mode load are

well known. It increases the speed and lowers the supply voltage. In combina- tion with the speed of an active DMOS transistor, a very low-speed power product

can be expected. In conventional integrated circuits, a depletion mode load

requires an extra diffusion or ion implantation to obtain the proper background impurity concentration while the original substrate provides the background to

obtain the proper threshold voltage., In our DMOS integrated circuit, no such

extra processing step is required because the substrate is chosen to yield a

depletion-mode load device and the threshold voltage for the enhancement-mode

DMOS transistor is already provided by the double-diffusion. Besides this

advantage, the load device can be made to have the same length-to-width aspect

ratio as the active DMOS transistor. This ratioless geometry results in further

reducing the area of an integrated circuit.

6

Switching Transistor Design Considerations

The choice of surface and background concentration is determined by the

threshold voltage and the breakdam voltage. The threshold voltage is a

function of surface state density and background concentration. For (l,O,O } oriented crystals, the surface state density is typically 2.5 x 10 /cm . A

threshold voltage of 2V requires a concentration of 2.5 x 10 atoms/cm as

calculated from equation (2).

11 2

16 2

where the following terminology is used. 3n

Gate-background work function difference = - In KT 4 x 10'" N(x), 2 ni

(for an n-doped Si gate with an assumed effective doping

concentration of 4 x atoms/cm . Intrinsic concentration = 1.5 x lolo atoms/cm at 27OC Surface-state density

Fermi level associated with a given doping concentration

3

3

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+"DO

& Depletion-Hose Load Device

OUT

I N +T- ( a ) Inverter Circuit

DKOS

-

ID

Points

Figure 5. DMOS Inverter

12 -

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.. "_ .

C = Gate capacitance per unit area E ox ox/tox* = Dielectric constant of oxide = 4 x 8.85 x 10 f/cm. = Gate oxide thickness.

= Dielectric constant of silicon = (11.7 x 8.85 x 10 f/cm).

- 14 ox

ox - 14 E si

The concentration n(x) for determining the threshold voltage is the value at the n + p junction formed by double diffusion and can be obtained by proper

choice of surface concentration and junction depth as indicated in equation (5). In our previous work,3 it was shmn that for the same threshold voltage,

the o.,lJ) crystal orientation gives a higher gain-bandwidth product than the

..(1,0,0') crystal orientation. The reason is that <1,1,1) orientation has higher surface states and hence make the channel more conductive near the

drain. This higher conductance accounts for the higher transconductance. The

penalty for the higher gain-bandwidth product is the lower breakdown voltage

at the isolation junction, as shown in table I, because the surface concentra- tion of the p-type isolation layer m s t be higher (at least as high as the

concentration at the drain channel junction) to avoid surface inversion. How-

ever, this is not a problem when we use low voltages.

Table I TRANSISTOR DESIGN PARAMETERS

(1 ,O,OJSi (NSS=2.5x10 /cm ) 1 (1,l ,I). (Nss = 10 /cm ) 11 2 12 2

p-type surface 3.3~10'~ 1 .5x1017 8.85~10'~:

p-type background 10 atoms/cm

6.3~10'~ 3.6~10'~ 2.1~10'~

2 vm 1.5 um 1 wn 2 um 1.5 um 1 vm n type junction

3 lJm 2.5 prn 1 lJm p-type junction 3 urn 2.5 rn 2 w

Surface concen- 2.5~1 0l6 atoms/cm

concentration

concentration

depth

depth

t r a t i o n a t source junction

15 3 15 3 10 atoms/cm

+

3 1 x1 o1 atoms/cm 3

Breakdown vol tage 28V 26V 24V 0.78V Threshold voltage 0.78V

13V 12v 11v

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Load Device Design Considerations

The load i s an n-channel depletion mode device. The cha rac t e r i s t i c of the

load device i s dependent upon the substrate impurity concentration and the

crystal or ientat ion. For most economical design, i t i s desirable that the

geometry of both the load device and the switch be minimum. The saturated

drain current of the load device for the "high" output (I DSAT)L1 and for the

"low" output ( I ) should sat isfy the condi t ions (see f igure 5): DSAT LO

where and (IDsAT)so are the saturated drain currents of the act ive

switching device for the high and low output respectively. To sat isfy equat ion

(6), the load device must be in deple t ion mode; i.e., the threshold voltage

must be negative. It should be kept i n mind that the threshold voltage for the

load device i s d i f f e ren t from the zero-substrate bias value because of the

"body effect". The "body effect" i s due to the reverse bias on the substrate

with respect to the source.

source of the load device i s

the output voltage i s high.

the negative of the pinchoff

where V i s the reverse bias

output terminal). R

As shown i n f i g u r e 4 , the output terminal or the

reverse biased with respect to the substrate when

Under this condition, the threshold voltage or

voltage Vp i s given as

ox r L ox

of the substrate re la t ive to the source ( the

The body e f f ec t i s different for dif ferent output condi t ions. I f the

source of the switching t ransis tor i s grounded and the output i s a t t h e low

state (or the switch i s on), the source of the load device i s near the ground

and i s not reverse biased with respect to the substrate. When the output i s

a t the h igh s ta te , the source of the load device i s reverse biased with

respect to the substrate , and the pinchoff voltage i s decreased. Thus, i n

equation (6), the should be calculated with substrate reverse

14

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biased by approximately V volts; substrate bias nearly equal to zero in equation (7). If the substrate is not the same potential as the source of the load device (i.e., not at " 0

level") but is reverse biased by V then the threshold voltage in equation (8) should be increased correspondingly. If we choose V = 5V, which is the supply voltage and

DD (IDSAT~LO should be calculated with a

R' R

4 x 10'' Nn 20F - - k T l " q

'9

Vn should be negative if the load device is to be in depletion mode. The saturated drain current of the DMOS can be represented by

where L is the effective channel length of a DMOS transistor which should be considerably shorter than the geometrical length. The saturated drain current of the load device is

ef f

The value of V is a l so given in equation ( 8 ) . Since the effective channel P length ¶ Lef f ¶ of the DMOS is always less than the geometrical length, L, the condition that I DS >IDL can be satisfied if

Figure 6 is a plot of the threshold voltage (or the pinchoff voltage) as

a function of the substrate concentration with different substrate bias Vp and surface state densities Nss based on equation (8). The surface states range from 101'/cm2 to 1012/crn2, which are representative of practical oxidized silicon surfaces. The reverse biases were 0, 3 , and 5V. The OV bias curves

15

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Substrate Concentration, tl1

Figure 6. Threshold Voltage as Function of Substrate Concentration

16

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are useful for designing the DMOS switch; the 3 and 5V curves are useful for the load device corresponding to two different supply voltages. For the load device to be in depletion mode, the threshold voltage must be negative with

respect to a substrate bias approximately equal to the drain supply voltage.

At the same time, the magnitude of the pinchoff voltage at zero bias must be

less than IVG - VTI to satisfy equation (12) keeping in mind that V can at

most rise up to V For instance, from figure 6, if Nss = 5 x 10 /cm for

6,1&} orientation, V of the switching device = 1V and VDD = 3V, to satisfy equations (6).and (12) the substrate concentration N must be 2.2 x 10 15

(point c) < N < 7 x (point a ) atomslcm . On the other hand, if we choose Nss = 10 /cm for (loo) orientation, then N < 7 x atoms/cm

(point a') which corresponds to a resistivity of 20 ohm-cm which is not easily controlled to a tight tolerance. This reasoning favors a moderate surface

state density; i.e., a higher N {l,l,l) substrate is more suitable than a

lower Nss <1,0,0> substrate.

1E 2 DD'

T

2

11 2 3

v

Ir

ss

At the other extreme, if one increases N = 10 /cm , then there is no 12 2 ss

N which can satisfy a 3V operation. Thus VDD = 5V must be increased to give

4 x (point c") < N 1.5 x (point a") atoms/cm . l7 3 v

From these considerations, we choose a p type ( l,l,l) substrate with

= 2 t o 5 ohm-cm

= 5 x 10 /cm 11 2 Nss

VT = 1v

EFFECT OF SILICON GATE RESISTANCE ON THE FREQUENCY RESPONSE OF MOS TRANSISTORS7

Self-aligned silicon-gate MOS transistors have smller dimensions and, therefore, are supposed to have a higher frequency response owing to the high

g and the low gate-to-drain feedback capacitance. However, a silicon gate

has much higher resistivity than a metallic gate. The nonzero resistivity can

have an adverse effect on the frequency response. This effect will be

explained in the following discussion.

m

17

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Silicon Gate as Distributed RC Network

Figure 7 shows the structure of a polycrystalline silicon gate MOS transis- tor. For high transconductance and gain bandwidth product, a small gate length L (typical < 1qLm) should be used. This dimension is often limited by the reproducible photoengraving capability of the process line used. The same photoengraving capability also limits the dimensions of the contact windows for the gate. If the gate contact were placed above the active area, it might short-circuit the gate to the source or the drain. This problem may be avoided in practice by not locating the gate contact directly above the active gate area but to the end where the polycrystalline silicon area may be conveniently enlarged as shown in figure 7.

Polysilicon gate material is not even approximately metallic and hence has nonzero resistivity. For a typical heavily doped, few thousand Angstrom thick silicon gate, the sheet resistivity may be in the order of tens of ohms per square and the series resistance to a far removed portion of a gate in the order of hundreds of ohms.

There are parasitic capacitances associated with the gate such as the gate-to-source capacitance, the gate-to-substrate capacitance, and the gate- to-drain capacitance. The silicon gate can then be considered as a uniformly

distributed RC transmission line as shown in figure 8. The distributed transistor can be considered as a number of lumped transistors with connnon drains and sources as shown in figure 9, but with their gates tapped from the distributed RC network. Because of their time delay along the distributed

network, the effective gate voltages of each lumped transistor, V are pro-

gressively delayed from the input signal, V.. This effect is particularly noticeable toward the end of the network. The drain currents, since they are

a monotonic function of gate voltages, are therefore progressively delayed.

The total drain current is the sununation of these time delayed from the input signal. For one lumped section of the RC distributed network, the small- signal voltage gain Av is given as

8

‘9’ 1

18

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Figure 7. Silicon Gate MOS Transistor

Figure 8. Distributed RC Network J

I 1 1

Figure 9. Equivalent Circuit of a Silicon Gate MOS Transistor

- _ 19

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where gm is the transconductance, R (= Xr ) is the series resistance, g 8

C (= Cc) is the input capacitance, and C is the load resistance. Any increase

in R or C will reduce the voltage gain. g

Frequency Response of the Distributed RC Network

The distributed RC network can be analyzed both for small-signal response

and transient response. For small signal analysis, a one-dimensional distri-

buted RC network is a good approximation because the enlarged metal contact area has very small sheet resistance and is sufficiently far from the source and drain diffusions compared to the oxide thichess such that the fringing

capacitance is negligible. The mathematics is straightforward and is

derived in the Appendix.

For small signal analysis, the voltage V (x), from figure 8, along the 8

width W of the distributed RC network is derived in the Appendix as equation

(A10) as

V,(x) = vi COSh fi W(1 - x / W ) cosh W

where r and c are the resistance and capacitance respectively per unit length

in the x direction. With manipulation, the amplitude and phase responses of

this expression can be found to be

V cosh2 m W ( 1 - x/W) + sin‘ W(1 - x/W> i cosh2 J a W + sin2 W (15)

- arctan [ tanh W tan /u- W ( 1 - x/W)]

These responses are plotted in figures 10 and 11. It can be seen that there is a considerable amount of attenuation and phase shift when the time

constant, RC, of the total resistance R = Wr and total capacitance C = Wc,

is of the order of l h . The transient response of a distributed RC network, as derived in the

20

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Appendix as equation (A16) i s given as

This equation is plot ted as the sol id- curves in f igure 12. It can be seen that the s ignal i s delayed along the line. A t a normalized

2 time of t/w r c = 1, the signal does not reach 90 percent of t h e f i n a l v a l u e a t

any length greater than 20 percent of the total length.

Time Constant of the Si l icon Gate

The time constant of the s i l i con ga te i s a function of the sheet

r e s i s t i v i t y , p,, and the gate oxide thickness. The resis tance per uni t length

i s given as

r = Ps/L

' where p s i s the shee t res i s t iv i ty and L is the source-to-drain distance of the

s i l icon gate . The capacitance per unit length is given as

where cox i s the djlelectric constant of the oxide and t i s the oxide thick-

ness. The time constant RC = W r c i s then obtained from equations (18) and 69). 2 ox

L ox

pS = 28 n/square

= IOOOI = 1 o - ~ cm

rc = sec/cm 2

RC = w rc = w .x sec. 2 2

Thus, fo r a ga te of 0..1 cm width, the t i m e constant i s then 10 ns. This order

of magnitude of gate width i s qui te common f o r d i sc re t e MOS t r a n s i s t o r s and

the output amplifier stages of an MOS integrated c i rcui t . For luw-power

2 1

Page 29: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

Figure 10. Small-signal Response of Distributed RC Network Amplitude Response in dB VS. Normalized Frequency with Position as a Parameter

22

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0 c

i

U" I

a I "-

. ".. . . _ " . .

Figure 11. Small-signal Response of Distributed RC Network Phase Response i n Degrees VS. Normalized Frequency with Position as a Parameter

-23

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in te rna l s tages on an MOS integrated c i rcui t , the gate widths are typical ly

one or two orders of magnftude narrower. - The t i m e constant, RC, which i s

proportional to W , i s then i n t h e subnanosecond o r picosecond range. 2

Charact.erist ics of the Sil icon Gate Uniform Channel MOS Transistor

The charac te r i s t ic of a MOS s i l icon ga te d i s t r ibu ted t rans is tor can be

computed from the equivalent lumped c i r cu i t w i th a number of t r ans i s to r s con-

nected in parallel but with delayed signals applied to the gates as shown i n

f igure 9. The charac te r i s t ics of each individual transistor i s given by the

relat ionship rl

I D = 2 pcG r ( V g - VT) VD - ~ I f o r VDL VD < V - VT ( t r iode opera t ion)

L 9

- pcG 2 I D - ('CJ - VT) f o r VD > V - VT (pentode operation)

(22)

where i s the carr ier mobil i ty , C i s the total gate capaci tance, VT i s the

threshold voltage, and VD i s the drain vol tage. In the present case, V i s a

function of time and distance from the contact as given by equations (11)

and (17).

G

g

The computation can proceed by applying an input voltage at the gate

contact in the equivalent c i rcui t shown i n f i g u r e 9 with given values of

dis t r ibuted gate res is tance and capacitance. The resultant drain current can

then be readi ly computed using a computer-aided-design program. The SPICE

program was used to simulate this relationship. For computational simplicity

and reasonable accuracy, the transistor computed i s divided into f ive incre-

ments. The parameter of each increment i s assumed as follows:

*

L = 10 prn W = 60 urn

* Developed by the University of California, Berkeley.

_- - 24

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"G/" I

g.9

0.8

0.7

0,6

0.5

0,4

0,3

u,2

O b 1

0,c)

.! / / I f

/ 2 T/N ni

0,4 0.3 1.2 1.6 2.0 2.4 2.6 LC

Figure 12. Transient Response of Distributed RC Network. Normalized Gate Voltage vs. Normalized Time with Position as a Parameter. (Computed results in solid line; simulated results in dashed lines.)

25

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The silicon gate sheet resistivity = 25 ohmslsquare. A very small load resis-

tance, 0.01 ohm, was used to sense the current. The transient response of the

drain current with a 6-volt input pulse of nanosecond risetime and 1-nanosecond

falltime, is shown in figure 13. For comparison, a zero sheet resistance

aluminum gate transistor of the same geometry is also computed and the tran-

sient response is plotted in figure 14. The results in Table 11 were obtained.

Table I1 Transient Response Simulation Results

Si Gate A1 Gate

Sheet resistivity 25 ohms square 0

Risetime 4 nsec 0.5 nsec

Fall time 2 nsec 1 nsec It can be seen that the nonzero sheet resistivity of the silicon gate very

markedly slows down the transient response.

A s a check, the gate voltages at the different incremental transistors

were also computed. Two of these results are plotted in figure 12 as dashed

lines to show general agreement.

The nonideal effect associated with the silicon gate is aggravated by the

Miller effect. If there is gate-to-drain overlap capacitance, C

and the load resistance C is appreciable, the input capacitance is effectively increased to C (1 + gm%>. Thus, the time constant of the distributed RC

gate is also increased.

gd , present

gd

To verify this prediction by simulation, the load resistance used in the

computation (as shown in figure 9) was increased from 0.01 to 100 ohms. This

computed transient response is then plotted in figure 15. Note that the rise-

time and falltime are lengthened as compared to that shown in figure 12 and 13, where no Miller effect is present.

Characteristics of DMOS Transistors

The double-diffused MOS (DMOS) transistor is designed for high-frequency operation by virtue of its much narrower effective channel length. The com-

putation of its characteristics was described by Lin et al. Because the

background concentration between the source and the drain is graded, the thres-

hold voltages vary along the channel. The DMOS distributed characteristics can

3

26

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"""

" " _ - . "

Figure 13. Computed Response of Silicon Gate MOS Transistor (Load Resistance 0)

2 7

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L.COC.CC C.OOO.01 L.COC.CC C.OW.00 C.COC.CC

r.coc.cc C.0W.OD L.CoC.CC L.00B.W L.CCC.CO S.OOO.00 L.COC.CC

&.COC.CC C.000.0O

L.Orn.00 L.CCC.CC c.ow.00 L.CCC.EC L.OW.09 I . C O t . C C

L.CCC.CC c.000.00 L.CCC.CC L.OOO.09

L.OW.00 1.CCC.CC L.OW.00 L.cCc.CL L.000.B9 c.ccr.cc s.oac.oo

r.mo.m

r.om-oo

t.rcc.cc

1.CYC.CL L.cCc.cr L.O?0.09 C.l".Et C.O¶C.O'! c.ecc.cc L.OOC.0I C.CCC.CC

L."C.CC

t.?CC.CC L.OOG.00 L.tCC.CC C.OOO.09 C.COC.CC

L.tCC.CC L.OIO.01 S.CCC.CC L.OOO.03 6 .COC.CO c.000.01 C.CCC.LC L.OOO.OO I.CCC.OO L.010.00 S.CCC.CC L.OW.C1 1.C9C.CC L.CCC.CC L.000.00 L.COC.CO L.030.01 C.CCC.CC

C.CCC.CO L.OOO.00

C.OOO.O9 L.COC.CO C.OW.00 6.roc.cc

c.tcc.co L.OW.00

L.0OO.DI

c.ow.00 L.COC.CO c.01c.m L.IOC.CO L.Orn.O¶ 1.rcr.cc L . O O O . 0 ~ L.COC.CO C.OO0.OO

1.COC.LO L.OO0.W

L.0oc.W L.CCC.CC L.OO0.W c.rcc.co

L.CIC.CO L.000.0O

L.000.0¶ 6.CCC.CO

L.coc.CC C.0OO.OO

&.ao2.o?

c.oac.oa

c.oao.o9

c.roc.co

a.roc.co

5.*l*.CC

"""""~"""""""""""~~"""""""" > Y >

"

a Y

> Y

Y

Y > > >

> > > >

> > Y

Y

3 > Y > > ? ? > > ? > > > > > > > > > > Y > > > > ? > > Y Y > > >

3 . . > ,

I

Figurel4. Computed Response of Silicon Gate MOS Transistor (Load Resistance 0)

28

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11ML

Figure

V I U .

I.OO2.CC

" - .

. .

. .

..ccc.c: s.coc.ac -.rrc.e. """"""""""""""""""""

> >

: > : > : > :> > > >: >: >: >: >:

> ? >: >: >: >: >: >: >: >: >: >: > 1 >:

> : >:

> : > : > : > : > : > : > : > : > : > : > ! > ! > I > : > 1 > : > ! I : > :

> >

- .

. .

>: ! > ,

> >

2 9

Page 37: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

'7 "7 "I

Figure 16. Equivalent Circuit of Silicon Gate DMOS Transistor

30

__ - . . . . . . . . . . . 1

Page 38: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

be computed by connecting a number of lumped incremental transistors in series

each with a different equivalent threshold voltage. If a silicon gate is used for the DMOS transistor, a similar adverse effect on the speed can be expected

due to the nonzero gate distributed series resistance.

The computation can be accomplished by using a series-parallel matrix

equivalent circuit as shown in figure 16 for one transistor. Computational

experience has shown that a DMOS can be approximated quite accurately by sub-

dividing it into 5 series increments. For an n-channel DMOS transistor with

background concentration = 10 /cm , the local equivalent threshold voltages, down an array of lumped sections written as a matrix column, were as follows:

VT1 = 2.OV (also the overall threshold voltage), VT2 = 1.2V, VT3 = 0 .4V, VT4 -0.3V, VTs = -0.8V. This computed result is shown in figure 17. A s expected, in comparison with a conventional MOS transistor of the same gate length and same threshold voltage (shown in figure 13), the DMOS transistor shows a faster transient response. However, due to the time constant of the silicon

gate, the risetime and falltime are not in the subnanosecond range.

15 3

- -

DMOS RING OSCILTATOR

A number of inverters can be connected in cascade to form a ring oscil-

lator. To form a ring oscillator, the number of inverters must be in odd number; then, the output level of the last inverter will be out of phase with

the input level of the first inverter forcing the input to change level. The

input signal m s t propagate through n number of inverters before the last inverter changes state. It takes time to propagate and takes two passes to

complete a cycle. The propagation time t of a single inverter is P .

The design layout of each inverter in the ring oscillator is s h a m in

figure 18. The last enhancement-mode DMOS transistor and the depletion-mode

load device have the same aspect (widthjlength) ratio. The lower device is

the DMOS transistor, which can be distinguished by the extra p-type diffusion mask outline, which is lpmwider than the n+ source diffusion windaw. The

drain-to-source spacing is conservatively drawn to l$m. The channel width

36

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. .

O.OC*

" . " " _ 2.000.00

""""""""

. . c,m*w .

" """"- > > > . >

>:

".OW "OCO-IC

x.5oo-CY 1.000-01

?.soD-O9 2.Ooo-0Y

1.0W-OY S.¶OO" a.ow-m

:> >

- . . > >

> 1 .5co-c5 3.oa-09

C.0W-OY 5.5CO-CY

I.5CC-CY

> : > : >: >: >:

> > > > > > > > D Y > > >

.. .

s .m?.cc : *.OL*.rn : L.C.?.CC :

5.RL.OC : S.6CY.W :

S.YOY.01 : 5.YIC.OC : 5.Y31.00 : S . ~ Y . O C :

5.rrs.cc : 5.978.00 :

S.YOY.W : S.?¶?.CC : 5.9Y5.00 : S.?Yl rCC :

s . n s . c c i S.9Y7.00 : L Y Y 9 . 0 0 .

> > > > > > Y > > > > Y > > > > > > > > > > > >

"""" - " - " " - """""""" ""- " "

Figure 17. Computer Response of Silicon Gate DMOS Transistor (Load Resistance = 100 Ohms)

32' '

Page 40: OF A DOUBLE-DIFFUSED MOS STRUCTURE€¦ · Eqerimeni;al Investigation of a Double-Diffused MOS Structure May 1976 6. PerForming Organization Code "" . - .~ ." " . . - . . - . 7. Authods)

Figure 18. Inverter Layout for Ring Oscillator

L

33

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i s drawn t o 30qLm. The smaller dimension of the source and drain diffusions i s

1$m. The smaller dimension of the contact window i s %m. The contact to the

s i l i con ga te i s made outside the active region.

DMOS SHIFT ReGISTER

A DMOS sh i f t reg is te r ce l l des ign can be pa t te rned a f te r a conventional

s t a t i c s h i f t r e g i s t e r cell by use of two inver te rs which are cross-coupled

through transmission gates to form a f l i p - f lop a s shown in f i gu re 19. The

transmission gates serve as active switches and should therefore be enhance-

ment mode devices. When the transmission gate Q i s closed by the clock signal 1

% , information i s coupled into the gate of t h e f i r s t i n v e r t e r and appears as

an inverter s ignal a t the drain output of Q,. During t h i s time, the trans-

mission gates Q and Q7 a r e opened so as not to load the input s ignal . After

the clock pulse a1 i s turned of f , in formt ion i s s tored a t the ga te and the

drain node capacitances of Q,. Then the clock pulse i s appl ied to the

transmission gate Q The information stored a t t h e d r a i n node capacitance

i s t ransferred to the gate of Q (or the input of the second inver te r ) . Thus

a doubly-inverted or in-phase signal appears a t the d ra in ou tput of Q There-

upon, a third clock pulse Q,, slightly delayed from a,, i s applied to the

transmission gate Q t o c lo se i t and latch the cross-coupled f l ip-flop, The

t iming relation of the different clocks i s shown a t t h e bottom of f igure 19.

In the DMOS in tegra ted c i rcu i t made by inve r t e r s and transmission gates

4

4' 5

5'

7

already discussed, only two types of t r ans i s to r s a r e ava i l ab le , e i t he r t he

depletion-mode t r a n s i s t o r , which i s unsuitable for transmission gates or the

enhancement-mode DMOS transmission gates. Thus, i n t h e s h i f t - r e g i s t e r c e l l

shown i n f i g u r e 18, Q,, Q,, Q4, Q,, and Q, a r e DMOS, a.nd the load devices Q3 and Q, a r e of depletion-mode.

AN OPTIMIZED OUTPUT STAGE FOR MOS INTEGRATED CIRCUITS9

In MOS integrated c i rcui ts , the output t ransis tors should be la rge enough

to drive the required load capacitance. I f there i s a s ign i f icant capac i t ive

load of t h i s l a s t ou tpu t t r ans i s to r , i t w i l l capacitively load the previous

34

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1

IN

(a) Schematic Diagram

Figure 19. Shift Register

35

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"- -. . . . . . " - I

stage and slow it down. To improve the propagation time, the driver for the output stage should also be enlarged. Obviously, if every stage is enlarged, excessive area will be consumed. However, if the drivers are tapered in some fashion from a minimm area cell to maximum area output cell as shmn in figure 20, both the propagation time and the area may be conserved. The fol- lowing is an analysis of such a tapered output stage for optimizing propagation time and chip area. This technique is applicable in general to MOS integrated circuits where a high output drive capability is required.

Output Seage Design Principles

To drive typical load capacitances required in an integrated electronic system, the output transistors in an integrated circuit should be of suitable size to provide large charging and discharging currents. Unfortunately, large output transistors load the previous stage, which decreases its operating speed. To improve this situation, the driver for the output stage should also be enlarged. This analysis can obviously be carried bacbard on a stage-by-stage basis.

Consider the output circuit such as the shift register shown in figure 20.

If the load capacitance, 5, is equal to M times the interstage node capaci-

tance, Co, and the MOS devices are of minimm sizes, the propagation delay (which is proportional to load capacitance) through the last two stages is:

where t =

t =

M =

PL PO

% = co -

-

propagation delay through the last two stages

propagation delay at the low level interstage

5 IC, load capacitance interstage node capacitance

The propagation time can be reduced by enlarging t'.le sizes of the MOS

devices of the last stage, 11, by m times. The driver stage, 12, is slowed down because the output transistors now see an m-fold increase in capacitive

load. The propagation delay of the driver and output stages becomes:

36

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TO find the minimm t we differentiate the above with respect t o m and PL ' set the differentiated equation to zero:

or

and

tp (min) = 2M'"t PO

(26)

For shorter propagation time, it is better t o enlarge the sizes of the last few stages. For instance, one may increase stages I by "1 times, increase stage I2 by m2 times the previous stage, I3 by m3 times, etc. Then the propagation delay for the last four stages becomes:

1

M ml m2 t = ( - + - + - + m ) t P4 m1 m3 3 PO

By differentiating t ' we find: P4 '

and

1 /4t tp4, = 4M PO

37

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Figure 20, Cascade MOS Stages

38

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The propagation delay of every stage is:

tpL = M'I4t PO

Note that the propagation time per stage resulting from enlarging the las t

three stages given in equation (30) is shorter than that of enlarging just

the last stage. . Also, the optimum s i zes of the device decreases monotonically

a s M 3'4 , $I4, M1I4 times the miniAm in te rs tage sizes. From t h e l a s t two equations, one may generalize that for an output device

of N stages, the propagation time per stage is

A computer analysis of a 10-stage output device uti l izing a 2-phase

r a t io l e s s l og ic i n t e r s t age .was made. The r e s u l t s of the analysis showed

good agreement of the predicted propagation delay to the computed delay to

within the accuracy of the program used.

Area Optimization

From the above der ivat ion, one can see that the opthum device size

should decrease on the order

mN = 1

When a number of stages are connected in cascade, the area is the sum of

a l l the stages. When the stages are tapered to optimize the speed, each pre-

ceding stage is reduced by a fac tor l / m . I f t h e r e a r e N-1 enlarged stages,

the area of t h e l a s t N stage is

39

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where A is the area of the standard stage (not enlarged). This sumnation is

equal to: 0

. - . . . . . . , . , . . . . N A o , ( m - 1 )

A ~ - , , m - 1 -

(33)

But since M = m N

This i s the r a t io of the enlarged area to the standard cell area. Equation

( 3 4 ) i s p lo t t ed i n f i gu re 2 1 for M = 100. A l s o plo t ted . i s the p ropagat ion

time of stage t which i s normalized: PS ,

From f igure 21 we f ind tha t tha . increased 'a rea ra t io i s of the order of

the load capacitance t o node capacitance ratio, M; . the a rea increases as the

number of enlarged stages N increases; and the propagation time per stage

decreases as the numbers of enlarged stages decreases.

Optimum Stage Design

The optimum design is a compromise between speed and area. The choice is

based on a nebulous parameter, cost, as in any search method. We can arbi t rar-

i l y choose a f igure of merit, F, defined as

where K i s a weighting exponent. I f K i s greater than unity, i t means more

40

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1 M= I00

t I

I I

I I I I I I I I

2 4 6 8 IO 12 14 1 I

NUMBER OFSTAGES,N

Figure 21. Normalized Propagation Delay, Normalized Area, and Figure of Merit F, VS. Number of Stages for M = 100, K = 2

41

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weight is placed on speed than area. .Substituting equations ( 3 4 ) and (35) into ( 3 6 ) :

The minimm F can be found by setting dF/dN to zero, yielding:

For instance, if K = 2: = 2

This has several implications. From equation (35):

t /t = M 1 /N PS PO

The minimum area and propagation delay is achieved when:

tps/tpo = 2 ( 3 9 )

The optimum area is:

Figure 22 is representative of how the figure of merit varies for several load to interstage capacitance values. Below the 'Dptimum value, t decreases

more slowly than the area increases; above this value, t increases more quickly than the area decreases.

PS PS

At some point, however, a large increase in propagation delay occurs. As seen in figure 21, the area-propagation delay square product increases drastical- ly for small values of N. This is not the case for larger values of N. Within the design constraints of a particular circuit, the designer pays a smaller

penalty in the area propagation delay square product by increasing the number

42

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IO

2

NUMBER OF STAGES,N

Figure 22. Normalized Propagation Delay and Area-Propagation Delay Square Product, F , vs. Number of Stages

-43

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F

of stages beyond the optinnzm point than decreasing the number of stages. A 1 so since :

An optimum condition exists when

m = 2 (42)

or when the capacitance ratio per stage doubles. Simply stated, the best compromise between area increase and the square of propagation delay decrease exists when the output device is designed such that each required stage in the output circuit doubles in size or capacitance between the last interstage cir- cuit and the load. Figure 23 shms the number of stages required for a given load to interstage capacitance ratio for optinum performance.

From a design standpoint, it is most economical to minimize the area.

If the entire integrated circuit consists of B number of cells, of which N stages are enlarged, the total area is

A = (B - N) A. +AN (43)

assuming each cell occupies A. area. In most instances, B is large. The enlarged area A does not add any more bits but merely improves the loading

and speed capability. Thus, a compromise exists between speed and area, If (B - N) >> AN/Ao, the addition of enlarged area is insignificant. If AN becomes comparable or larger than (B - N) Ao, the enlarged buffer can add substantially to the area and cost of the integrated circuit. In this case, the design engineer may choose to commit some fraction of the total chip area to an output device. Figure 24 represents the minimm propagation delay obtainable for a given area and a fixed capacitive load.

N

MASK DESIGN

The layout of the basic shift-register cell is shwn in figure 25. Since

the transmission gates are bidirectional devices, it does not matter whether the source should be located at the input or the output side. From a topologi- cal standpoint, it is more convenient dand space saving for two transistors to

44

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10'-

lo"

IO-

IO2-

IO -

2 4 6 8 IO NUMBER OF STAGES,N

12

Figure23 . Optimum Number of Enlarged Output Stages for Different Load to Node Capacitance Ratios

45

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0 a c: B

10-

0 IO0 200 300 NORMALIZED STAGE AREA A,/A,

Figure 24 . Minimum Propagation Delay Obtainable for a Given Area and a F ixed Load t o Node Ratio of 100

45

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j i i f I

m I

Figure 26. Overall Interconnection Mask

48

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I

I += +“ +* +” +”

Figure 27 . P- Channel-Stop Diffusion Mask

49

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Figure 28 . N Diffusion Mask +

50

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\

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Figure 30. Silicon Etch Mask

52

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. . . . . . . . . . . . . .

.

. . . . . . . ' . . . ' .* ". . .. ; " ; . a . . ., : " : . . ' .*

~ ~~ ~~

Figure 31. Contact Mask

53

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I

Figure 32. Interconnection Mask

54

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have counnon sources or cornon drains.

The layout of the integrated c i rcui ts i s shown in f i gu res 26 through 32. There are four versions. Mask 4500-4 i s the fu l l 128 b i t s h i f t r e g i s t e r . The

f i r s t 124 b i t s a r e of low-level stages with minimum device geometry. The l a s t

4 b i t s are progressively enlarged to optimize the speed-area product. The

design has a zigzag path. The f i r s t two have16 b i t s , the next six rows have

18 b i t s each, the eighth row has 3 progressively enlarged stages, and the

l a s t two rows comprise the l a s t stage with the output transistors wrapping

around the bend.

The second vers ion (4500-2) i s a 16-b i t sh i f t reg is te r us ing the f i r s t

row of the low level s tages . The change i s accomplished by changing the

interconnection pattern. The third vers ion (4500-1) i s a 4 -b i t sh i f t r eg i s t e r

consis t ing of only the last four enlarged output stages. The fourth version

(4500-3) i s a 40-b i t sh i f t reg is te r cons is t ing of two rows of low level stages

with 36 b i t s and the last four output stages. I n every version, there i s a

capacitor and a t e s t i n v e r t e r .

There a re s ix masks (see Fabrication section). The masks were generated

by the David Mann pattern generator.

FABRICATION

Double-diffused MOS (DMOS) t ransis tors are capable of high-speed operation

by effectively reducing the channel length using the difference of two succes-

sive diffusions through the same source window. For high transconductance,

double diffusion should not be used for the drain. Thus, the drain window and

the source window are usual ly not cut a t the same time. A s a r e s u l t , s e l f -

alignment of the gate cannot be achieved. For best high-frequency performance,

i t i s desirable to have self-aligned gates to reduce the area and the drain-to-

gate capacitance. This work features a nrethod for achieving self-alignment.

In addi t ion, a depletion mode load device with self-aligned gate i s a l s o

incorporated i n an integrated structure. The desired s t ructure i s achieved by

using a po lys i l i con ga t e i n combination with selective nitr ide masking. 10

The d e s i r e d inverter configurat ion i s shown in f i gu re 5 with a DMOS tran-

s i s tor d r iv ing a depletion load device. Figure 33 shows the processing

55

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P

S i3N4 Poly siop

n n n n S i , N .

I CI

S i3N4 Z?XY

A1 S i 0 2 Poly sio2

Figure 33. Si Gate DMOS IC Structure

56

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sequence. A moderately doped p-type layer i s f i r s t d i f f u s e d i n t o a ,,-type

subs t ra te for i so la t ion . The ga te d ie lec t r ic po lycrys ta l l ine s i l i con and

s i l icon ni t r ide layers are sequent ia l ly deposi ted on the substrate. Windows

f o r N source and drain diffusions are cut through the s i l icon ni t r ide layer .

Another photoengraving follows to open a s l i gh t ly l a rge r window in t he photo-

resist above the source region of the DMOS t rans is tor , permi t t ing the n i t r ide

to serve as a mask fo r removing the po lycrys ta l l ine s i l i con and gate oxide.

+

N e x t , a p-type channel diffusion penetrates into the source windows.

Source windows are oxidized. Plasma etching then removes only the ni t r ide and

polycrys ta l l ine s i l i con layers from the d ra in windows. Now a l l the source and

drain regions are covered only with oxide, which can be readi ly removed for the

n-type diffusion. In this manner, self-alignment i s achieved.

For the depletion-mode load device, the channel i s masked against the

second p-type diffusion. The low ,-type background concentration, together

with the posit ive surface staes, i s su f f i c i en t t o make the MOS t r a n s i s t o r t o

be in deplet ion mode.

The processing parameters of the double diffused MOS are as follows:

a.

b.

C.

d.

e.

f .

g .

h.

i.

j. k.

1.

m.

n.

Substrate: (l,l,l) , p type 10 to 3h/cm.

Thermal Oxtdation: 50002 thick.

Photoengraving for p guard ring. +

p boron diffusion: lOm/square, b m deep

Oxide removal.

Gate d i e l ec t r i c : 10001 si l icon dioxide plus 8001 s i l i con n i t r i de .

Vapor growth of polycrystall ine si l icon bydecomposition of silane:

3 0001.

Diffusion mask growth: 2000x s i l i con n i t r i de p lus 50002 s i l i c o n

dioxide.

Photoengraving for n source and drain windows through top oxide.

Photoengraving fo r p source windows to subs t ra te .

p boron diffusion: 12g/square, 4pm deep.

Plasma etch of polycrystal l ine s i l icon f rom-drain windows and

then removal of oxide from both source and drain windows.

N phosphorous diffusion: lOn/square, 1 . b m deep.

Plasma etch of po lycrys ta l l ine s i l i con to de l inea te d i scre te polysil icon areas.

+

+ +

+

+

57

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0. Photoengraving of contact windows. p. Metalization: 15,OOOg, 70% A1 plus 30% silicon. q. Photoengraving of interconnect pattern. r. Sintering.

EXPERIMENTAL RESULTS

An experimental self-aligned silicon gate DMOS integrated inverter is shwn in figure 3 4 . The DMOS transistor Q, has a length of 7 CLm and a width of 420 Clm. The depletion mode load device Q, has the same dimensions. In DMOS integrated circuits, it is possible to design both devices to have the same dimensions (ratioless) because of the higher conductance of the depletion- mode load device. This ratioless feature allows for higher density.

Typical Test Transistor Characteristics

The V - I characteristics of the DMOS transistor and the load device are shown in figure 3 5 . Note that the transconductance of the DMOS transistor at 8 mA of drain current and 5V of drain voltage is approximately 3 d o . From a theoretical standpoint, the maximum achievable transconductance g (max) =

WC v , where W = channel width = 300 x 10 cm.

5

-4 m

S C = gate capacitance per unit area.

= dielectric constant of oxide/gate oxide thickness

= 3 . 4 x 10 (F/cm)/0.15 x (cm). -13

6 v = scattering limited velocity = 6 x 10 cm/s. S

The theoretical gm (max) using our parameters should be about 4 m h o s . Thus,

our result is approaching the theoretical value.

In the several lots we fabricated, we had a spread of threshold voltages ranging 1 to 5V. However, the maximum transconductance achieved has been quite consistent. The threshold voltage of the DMOS transistor shown in figure 35 is approximately 3.5V.

The characteristics of a load device is shown in figure 3 5 . It was processed in the same run as the DMOS shown in figure 3 5 . Note that the saturated drain current averages about 0 . 5 A. For proper inverter operation, the DMOS "on" current should be larger than the load device current.

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Figure 3 4 . DMOS Integrated Inverter

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F

Because the threshold voltage after fabrication was lower than expected before fabrication, provision was made to reverse bias the substrate to account for process variation, thereby increasing the threshold voltage. The effect of the substrate bias on the load device is to increase the threshold voltage, hence the IDsAT, is shown in figure 36 .

Inverter Characteristics

The characteristic of the test inverter is shown in figures 37 and 38. The transfer characteristics for 3 and 5V operation were tested. The effect of

the substrate bias was also tested as shown in figure 37 and 38. These charac- teristics show that the inverter should work under all these conditions. How-

ever, the 3V operation with 1V substrate bias appears to give the best results

in terms of noise margin.

Effect of Silicon Gate Resistance

The effect of the silicon gate resistance was also investigated. For this experiment, there are two gate contacts as Shawn in figure 39, one at each end of the gate. The gate length is 7 um and the width-to-length ratio is 60.

The transistor was mounted in a microwave transistor package and tested with a Hewlett-Packard Network Analyzer. The transistor was tested first with one gate connection, then with both. The S-parameter readings are listed in Table 111.

Table I11 Experimentally Measured S-Parameters at 100 MHz

H21 s2 1 G1 G U K lMX

1 gate connection 2.1 -21.5 19.1 5.8 3.4 0.28 2.44

2 gate connection 4.3 -14.3 13.5 6.3 5.5 0.36 1.58 From the above dimensional information and the previous processing con-

stants, the RC time constant of the silicon gate is 2.7 nsec. The radian fre- quency (w = 1/RC) is 3.5 x 10 radians/sec. According to figures 10, 11 and 12 the gate series resistance effect on amplitude response should become pronounced at 100 MHz, as indeed it is.

8

It can be seen from this data that the forward current gain, H21, is doubled for the case of two gate contacts. The two gate contacts divide the

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I "

Figure 35. Transistor V-I Characteristic of DMOS Inverter

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Effect of Substrate Bias on Load Figure 36. Device Characteristics

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Zero Bia 8

'in

0.5V/Division

(b) 1V Bias

Figure 37. DMOS Inverter Characteristics in 5V Operation

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'in

0.5V /Division

Figure 38. DMOS Inverter Characteristics in 317 Operation

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Figure 3% Photomicrograph of DMOS T r a n s i s t o r Showing 2 Gate Contacts

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current into two halves and the voltage drop along each part of the distributed

gate is then reduced. This effectively higher gate voltage over more of the gate length increases the output drain current, hence H21 .

The naximum available power gain, is directly proportional to the Gmax, transconductance and inversely proportional to the input resistance. With two gate contacts, the input resistances, of which the silicon gate resistance con- tributes substantially, are effectively halved. Meanwhile, the transconductance is effectively increased because of reduced voltage drop along the silicon gate.

Hence, the maximum available gain is increased for two gate contacts. These measurements are therefore indicative of the degrading effect on frequency response by the silicon gate.

Ring Oscillator Performance

A number of DMOS inverters can be connected in cascade as a ring oscil- lator to test the propagation delay and the speed-power product. The one we

tested was a seven-inverter ring oscillator and a buffer as shwn in figure 40. The ring oscillator works satisfactorily from 1.3 to 8.5V. The test results are tabulated in Table IV. The oscillation waveforms are shown in figure 41 for supply voltages of 1.3, 3 , and 8.5V.

Table N Ring Oscillator Performance

- %D - 1.3V

1.5

2

3

4

5

6 -

v* = ov

tpd ’o tpdPo

ns mW PJ

7.57 .32 2.42

7.57 .35 2.68

7.57 1.09 8.23

7.29 1.7 12.38

6.93 2.38 16.45

6.64 3.34 22.17

vs “1V

11.43 .37 4.22

9.29 .51 4.76

8.64 1.01 8.75

8.0 1.6 12.8

7.5 2.3 17.25

7.14 3.3 23.57

The propagation delay, tpd i

VB = -2v

tpd ‘0 tpdPo

ns mW PJ

11.14 .889 9.90

9.14 1.44 13.16

8.36 2.12 17.72

7.71 2.93 22.59

calcui

vs = -3v

ns mW d

6.25 1.38 22.43

9.93 1.94 19.26

8.64 2.74 23.67

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Figure 40. Ring Oscillator

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Figure 41. Ring Oscillation

41a

VDD = 1.3V

41b

'DD =

41c

v = 8 . 3 DD

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where f is the frequency of oscillation and n is the number of inverters in the ring (n = 7 in our case). The power dissipation per stage Po is equal to the total power dissipation divided by the number of inverters used in the ring oscillator and the buffer (=8 in our case). The propagation delay-pawer dis- sipation product, t Po, is a figure of merit of a logic gate. Certain units have t as low as 4 nsec.

Pd Pd It should be noted that the propagation delay of 7 nsec is considerably

better than the conventional TTL gates. The propagation delay-paver dissipa- tion product at a supply of 1.3V is only 2 picojoules which is an order of magnitude lower than for TTL gates. The fact that the DMOS gates can operate as low as 1.3V is another advantage Over the TTL gates. It appears that the DMOS gates are better than the TTL gates in most important aspects. Figure 42 is a plot of propagation delay and power dissipation as a function of supply voltage .

SUMMARY AND CONCLUSIONS

The purpose of this work was to study the feasibility of using self- aligned silicon gate technology for DMOS integrated circuits. In the course of the experimental investigation, we have accomplished a number of tech- nological advances:

First, we developed a process for fabricating DMOS integrated circuits using silicon gate technology. Up to now, the DMOS transistor technology has been limited to aluminum gates, which are not self-aligned and therefore require overlap areas with resulting additional feedback capacitance. Our development makes it possible to combine the low parasitic capacitance and facilitated processing advantages of self-aligned gates with the short effective channel length of DMOS to produce a structure with much improved high-frequency performance.

Secondly, we developed a technique to optimize the design of the depletion- mode load device without the need for additional diffusion steps as is normally done in standard MOS processing. This was done by proper choice of the sub- strate orientation and resistivity. Moreover, our design approach resulted in a load device having the same length-to-width ratio as the DMOS transistor.

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1 2 3 4 5 6 "DD

Figure 42. Propagation Time and Power Dissipation of DMOS Inverters

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This ratioless geometry greatly reduces the size of an integrated circuit as

compared to other approaches where the size of the load device is relatively

larger than the MOS transistor. Thirdly, we developed a novel method of tapering the geometry of the out-

put stages for optimizing the propagation time and the chip area. This method

has general application to most clocked MOS LSI integrated circuits. This

design approach was incorporated in the design of the DMOS shift register under investigation.

Fourthly, we recognized the effect of the finite silicon gate resistance on the frequency response of an MOS transistor. The resistance creates a dis- trihted RC network along the gate and tends to slow dawn the transient

response. The effect is more pronounced for wider silicon gates (i.e., larger

devices). Care should be exercised to minimize this adverse effect on large

output devices.

Finally, we successfully fabricated an integrated DMOS ring oscillator

with a propagation time of 4 to 7 nanoseconds capable of operating as law as

1.3V and a speed-propagation-power dissipation product of 2 pJ. Such a per- formance is better than conventional TTL gates. The results are particularly

significant in that the ring oscillator transistors were test pattern devices

and not optimized for high-speed performance. Further improvement in perfor-

mance is to be expected by elimination of bonding pad capacitances and by optimizing the transistor geometry.

The results of our investigation have been published in four different

articles. The results of the DMOS process development and the tapered output

stage concept were presented in separate papers at the 1974 Government Micro-

electronic Applications Conference (GCIMAC) in Boulder, Colorado. An expanded

paper on the latter was also published in the IEEE Journal of Solid-state Circuits (April 1975). The effect of silicon gate resistance on the fre-

quency response of MOS transistors appeared in the IEEE Transactions on Electron Devices (May 1975). Publication of the experimental results and

design consideratims for the integrated llMOS ring oscillator is anticipated

for later this year.

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APPENDIX

Frequency Response of Distributed RC Line

Small Signal: Consider an incremental RC section as shown in figure 8.

The differential equations for such a section are:

c - = - dv di dt dx

ri = - dv dx

For steady-state sinusoidal voltages and currents,

2 d v

dx 2 - =

- = di dx

The solutions for these equations are

v = Ae Y X h

where A and B are arbitrary constants and

Y = (jwrcw 2 1/2

zo = (r/jwc> (A8

For an open ended line as shown in figure 1, the boundary conditions are

(ilxW = 0; (v)x=o - vi - (A91

Substituting into equations (AS) and (A6)

V ( X ) = COS hy (l-X/W)

vi cosh y

Transient Response

The Laplace transform of a step input voltage is V./s. From equation 1

(A10) the transform of any voltage x is,

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The inverse transform of this equation is

1 Viest cosh (1-x/W) W 6 v (x , t ) = - 6 2nJ . ds s cosh W K

The poles for cosh W rcs are given by the roots of the equation

where n is an integer. From Cauchy's integral theorem at any pole

where the residue R -

Thus the integral (A12) can be evaluated.

- , E M

D' (s)

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REFERJTNCES

1. Tarui, Y. ; Hayashi, Y; and Sekigawa, T: "Diffusion Self-Aligned MOST - A New Approach for High Speed Devices," in Proc. 1st Conf. Solid State Devices, Tokyo, 1969.

2. Cauge, T. P.; Kocsis, J.; Sigg, H. J.; and Vendelin, G. D.: "A Double Diffused MOS Transistor Achieves Microwave Gain," Electronics, Vol. 44, Feb. 1971, p. 99.

3. Lin, H. C.; and Jones, W. N.: "Computer Analysis of the Double-Diffused MOS Transistor for Integrated Circuits," IEEE Trans. Electron Devices, ED-20, Mar. 1973, pp. 275-283.

4. Lin, H. C.; and Halsor, J. L.: "Experimental Investigation of a Shielded Complementary Metal-Oxide Semiconductor (MOS) Structure ," NASA CR-132456, 1974.

5. Frohman-Bentchkowsky, D; and Vadasz, L.: "Computer-Aided Design and Characterization of Digital MOS Integrated Circuits," IEEE Journal of Solid State Circuits, SC-4, April 1969, pp. 57-64.

6. Lin, H. C.; and Varker, C. J.: "Normally-On Load Device for IGFET Switch- ing Circuits", 1969 NEREM Rec., Vol. 11, Nov. 1969, p. 125.

7. Lin, H. C. ; Arzoumanian, F. ; Halsor, J. L. ; Giuliano , M. N. ; and Benz , H.F. : "Effect of Silicon Gate Resistance on the Frequency Response of MOS Transistors," IEEE Trans. on Electron Devices, ED-22, May 1975, pp. 255- 265.

8 . Engeler, W. E.; and Brawn, D. M.: "Performance of Refractory Metal Multi- level Interconnection System", IEEE Transactions on Electron Devices, ED-19, Jan. 1972, pp. 54-61.

9. Lin, H. C. ; and Linholm, L. : "Optimized Output Stage for MOS Integrated Circuits", IEEE Journal of Solid-state Circuits, SC-10, April 1975, pp. 106-109.

10. NASA Tech Brief, "Polycrystalline Silicon Delineation with Application to a Double-Dif fused MOS Transistor", (LARS 11536. and 11598).

11. Ohta, K.; et al,: "A High-speed Logic LSI Using Diffusion Self-Alignment Depletion MOST", Digest of Solid-state Circuits Conference, XVIII, Feb. 1975, pp. 124-125.

74 NASA-Langley, 1976 CR-2620