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Developmental Considerations on the Free-Piston Stirling Power Convertor for Use in Space by Jeffrey Schreiber presented at the 2006 IECEC Abstract Free-piston Stirling power conversion has been considered a candidate for radioisotope power systems for space for more than a decade. Prior to the free-piston Stirling architecture, systems were designed with kinematic Stirling engines with rotary alternators to convert heat to electricity. These systems were proposed with lightly loaded linkages to achieve the necessary life. When the free-piston configuration was initially proposed, it was thought to be attractive due to the relatively high conversion efficiency, acceptable mass, and the potential for long life and high reliability. These features have consistently been recognized by teams that have studied technology options for radioisotope power systems. Since free-piston Stirling power conversion was first considered for space power applications, there have been major advances in three general areas of development: demonstration of life and reliability, the success achieved by Stirling cryocoolers in flight, and the overall developmental maturity of the technology for both flight and terrestrial applications. Based on these advances, free-piston Stirling convertors are currently being developed for a number of terrestrial applications. They commonly operate with the power, efficiency, life, and reliability as intended, and much of the development now centers on system integration. This paper will summarize the accomplishments of free-piston Stirling power conversion technology over the past decade, review the status, and discuss the challenges that remain. https://ntrs.nasa.gov/search.jsp?R=20070017910 2020-04-29T21:10:50+00:00Z

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Developmental Considerations on the Free-Piston Stirling Power Convertor for Use in Space

by

Jeffrey Schreiber presented at the 2006 IECEC

Abstract Free-piston Stirling power conversion has been considered a candidate for radioisotope power systems for space for more than a decade. Prior to the free-piston Stirling architecture, systems were designed with kinematic Stirling engines with rotary alternators to convert heat to electricity. These systems were proposed with lightly loaded linkages to achieve the necessary life. When the free-piston configuration was initially proposed, it was thought to be attractive due to the relatively high conversion efficiency, acceptable mass, and the potential for long life and high reliability. These features have consistently been recognized by teams that have studied technology options for radioisotope power systems. Since free-piston Stirling power conversion was first considered for space power applications, there have been major advances in three general areas of development: demonstration of life and reliability, the success achieved by Stirling cryocoolers in flight, and the overall developmental maturity of the technology for both flight and terrestrial applications. Based on these advances, free-piston Stirling convertors are currently being developed for a number of terrestrial applications. They commonly operate with the power, efficiency, life, and reliability as intended, and much of the development now centers on system integration. This paper will summarize the accomplishments of free-piston Stirling power conversion technology over the past decade, review the status, and discuss the challenges that remain.

https://ntrs.nasa.gov/search.jsp?R=20070017910 2020-04-29T21:10:50+00:00Z

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Dev

elop

men

tal C

onsi

dera

tions

on

the

Free

-P

isto

n S

tirlin

g P

ower

Con

verto

r for

Use

in

Spa

ce

pres

ente

d at

the

2006

Inte

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l Ene

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Engi

neer

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go, C

A

byJe

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chre

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as e

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Dev

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•S

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chno

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dev

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be

view

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s ha

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gon

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roug

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gene

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hase

s–

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ly a

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artic

ular

em

phas

is is

pla

ced

on th

e ad

vanc

es b

etw

een

1999

and

200

5, y

ears

of r

adio

isot

ope

gene

rato

r de

velo

pmen

t

3

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•S

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m 1

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abo

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prim

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afet

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otor

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pha

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deve

lopm

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ame

to a

n en

d

4

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Dev

elop

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tirlin

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Dev

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itial

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flow

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–H

ighe

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cien

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lips

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impr

oved

und

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th

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Reg

ener

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ycle

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licat

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plic

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5

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ww

w.n

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Dev

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men

t of S

tirlin

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Dev

elop

men

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app

licat

ions

incl

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PU

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r milit

ary,

qui

et p

orta

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pow

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lips

4-21

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appl

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nite

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war

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otiv

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pum

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ter

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radi

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tem

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cros

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side

load

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ntly

life

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otop

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Sys

tem

(SIP

S) w

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by

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lect

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Bas

ed o

n rh

ombi

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with

two

rota

ry a

ltern

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s•

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d ve

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vie

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as

the

seco

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ener

al p

hase

of S

tirlin

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velo

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6

Nat

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ww

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Dev

elop

men

t of S

tirlin

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The

third

pha

se o

f dev

elop

men

t beg

an w

ith th

e in

vent

ion

of th

e fre

e-pi

ston

Stir

ling

in th

e 19

60’s

•E

limin

ated

:–

Lubr

icat

ion

syst

em–

Gas

com

pres

sor a

nd g

as m

anag

emen

t sys

tem

–Li

fe li

miti

ng w

ear o

f slid

ing

seal

s•

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ld b

e de

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to h

ave:

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erm

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con

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men

t of w

orki

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uid

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on-c

onta

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g op

erat

ion

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ough

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load

of a

n ex

tern

al c

ontro

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–19

70’s

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ign

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llow

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sign

ifica

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opm

ent

–19

80’s

desi

gn p

erfo

rman

ce fo

llow

ing

limite

d de

velo

pmen

t–

1990

’sde

sign

per

form

ance

follo

win

g m

inim

al

deve

lopm

ent

•S

till m

inim

al c

onsi

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tion

of s

yste

m in

tegr

atio

n

7

Nat

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tics

and

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min

istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g•

Free

-pis

ton

Stir

ling

conv

erto

r tec

hnol

ogy

for

radi

oiso

tope

app

licat

ions

was

bei

ng d

evel

oped

by

NA

SA

& D

OE

at l

ow le

vels

dur

ing

the

1990

’s•

1997

stu

dy le

d by

DO

E c

oncl

uded

that

Stir

ling

tech

nolo

gy e

xist

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nd w

as a

vaila

ble

for f

light

de

velo

pmen

t•

1999

Tec

hnol

ogy

Rea

dine

ss A

sses

smen

t was

co

mm

issi

oned

to d

eter

min

ed if

Stir

ling

was

su

ffici

ently

mat

ure

for t

rans

ition

to fl

ight

de

velo

pmen

t•

Team

mem

bers

DO

E, G

RC

, JP

L, L

M, O

SC

•R

eadi

ness

Ass

essm

ent c

onsi

dere

d –

Per

form

ance

map

ping

–E

MI/E

MC

cha

ract

eriz

atio

n–

Laun

ch lo

ad v

ibra

tion

test

–Fa

ult t

oler

ant g

ener

ator

con

figur

atio

n–

Flig

ht w

orth

y co

ntro

ller d

esig

n–

Rad

iatio

n to

lera

nce

–FM

EC

A

8

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

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istra

tion

ww

w.n

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gov

Dev

elop

men

t of S

tirlin

g•

The

1999

stu

dy fo

und

that

:–

EM

I mea

sure

men

t sho

wed

that

a S

tirlin

g ge

nera

tor

coul

d m

eet t

he re

quire

men

ts o

f mos

t sci

ence

mis

sion

s,

but n

ot th

e m

ost d

eman

ding

–S

tirlin

g co

nver

tor T

DC

#1

surv

ived

12.

3 gr

ms

rand

om

vibr

atio

n te

st–

Gen

erat

or c

once

ptua

l des

igns

exi

sted

from

LM

, OS

C,

and

GR

C, w

ith v

ario

us d

egre

es o

f det

ail a

nd d

iffer

ent

conc

epts

for f

ault

tole

ranc

e–

A fl

ight

con

trolle

r con

cept

ual d

esig

n w

as d

evel

oped

, but

no

t bui

lt or

test

ed–

Ther

e ap

pear

ed to

be

no b

arrie

rs fo

r im

plem

entin

g a

suite

of o

rgan

ics

that

cou

ld s

urvi

ve th

e no

min

al ra

diat

ion

leve

ls–

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FME

CA

sho

wed

no

show

-sto

pper

s•

1999

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hnol

ogy

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dine

ss A

sses

smen

t det

erm

ined

th

at S

tirlin

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as s

uffic

ient

ly m

atur

e fo

r tra

nsiti

on to

fli

ght d

evel

opm

ent

9

Nat

iona

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and

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min

istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g

•LM

was

sel

ecte

d by

DO

E a

s th

e S

yste

m In

tegr

atio

n C

ontra

ctor

for t

he S

RG

110

gene

rato

r•

Flig

ht d

evel

opm

ent c

ontin

ued

at L

M, I

nfin

ia, a

nd G

RC

w

orki

ng in

par

tner

ship

thro

ugh

2005

•G

RC

als

o co

nduc

ted

an a

dvan

ced

tech

nolo

gy e

ffort

to

incr

ease

effi

cien

cy, r

educ

e m

ass,

enh

ance

robu

stne

ss•

Hig

hlig

hts

incl

ude:

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etal

lics

•O

ptim

ized

hea

ter h

ead

mat

eria

ls fo

r lon

g lif

e, c

hara

cter

ized

the

mat

eria

ls•

Dev

elop

ed te

chni

ques

to re

pres

ent t

he m

ater

ials

on

a pr

obab

ilistic

bas

is, c

ondu

ct li

fe a

naly

sis

in p

roba

bilis

tic te

rms

•V

alid

ate

heat

er h

ead

life

anal

ysis

thro

ugh

benc

hmar

k te

sts

•O

ptim

ize

rege

nera

tor p

roce

ssin

g to

enh

ance

relia

bilit

y

10

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

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istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g–

Org

anic

s•

Cha

ract

eriz

e cu

re k

inet

ics

of c

ritic

al a

dhes

ives

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opt

imiz

e pr

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sing

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ondu

ct a

ging

test

s of

the

orga

nics

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itial

ass

essm

ent o

f rad

iatio

n to

lera

nce

–M

agne

ts a

nd li

near

alte

rnat

ors

•C

hara

cter

ize

cand

idat

e m

agne

ts•

Dev

elop

sho

rt te

rm a

nd lo

ng te

rm m

agne

t agi

ng te

sts

•D

evel

op te

chni

que

to c

hara

cter

ize

curv

ed m

agne

ts•

Cre

ate

tech

niqu

e fo

r 3-D

line

ar a

ltern

ator

mag

neto

stat

ican

alys

is

•P

redi

ct c

ondi

tions

for d

emag

netiz

atio

n in

a li

near

alte

rnat

or a

nd

valid

ate

with

test

dat

a–

Stru

ctur

al d

ynam

ics

•D

emon

stra

te fu

ll op

erat

ion

of c

onve

rtor u

p to

12.

3 gr

ms,

0.2

g2 /

Hz

•Fu

lly c

hara

cter

ize

mod

al re

spon

se o

f the

Stir

ling

conv

erto

r•

Dev

elop

con

cept

for s

truct

ural

inte

grat

ion

of S

tirlin

g co

nver

tors

into

th

e ge

nera

tor t

o re

duce

laun

ch lo

ads

•D

evel

op s

pace

craf

t ada

pter

that

cou

ld b

e us

ed to

redu

ce la

unch

lo

ads

if ne

eded

•V

alid

ate

stru

ctur

al m

odel

thro

ugh

gene

rato

r sim

ulat

or te

st•

Sho

w a

naly

tical

ly th

at S

RG

-like

gen

erat

or c

ould

sur

vive

up

to 1

5.1

grm

s, 0

.3g2 /H

z

11

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

min

istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g–

EM

I/EM

C•

Tota

l of t

hree

test

s co

nduc

ted

at G

RC

and

JP

L•

It re

mai

ns th

e fin

ding

that

Stir

ling

coul

d m

eet

gene

ral s

cien

ce re

quire

men

ts, b

ut w

ould

nee

d a

mis

sion

kit

for t

he m

ore

dem

andi

ng m

issi

ons

•E

MI r

emai

ns a

sys

tem

leve

l iss

ue, r

equi

ring

com

plet

e ge

nera

tor d

esig

n–

Rel

iabi

lity

•Te

chni

ques

for p

roba

bilis

tic a

naly

sis

have

bee

n ap

plie

d to

all

criti

cal c

ompo

nent

s–

Nee

d to

com

bine

indi

vidu

al a

naly

ses

into

a s

ingl

e S

tirlin

g co

nver

tor a

naly

sis

•D

iffic

ulty

rem

ains

in v

erify

ing

life

and

relia

bilit

y of

a

devi

ce w

ith n

o w

ear m

echa

nism

–Sa

me

prob

lem

face

d by

the

cryo

cool

er in

dust

ry•

Expe

rienc

e fro

m lo

ng li

fe S

tirlin

g co

nver

tors

and

cr

yoco

oler

s is

dire

ctly

app

licab

le•

Muc

h m

ore

oper

atio

nal d

ata

is n

ow a

vaila

ble

–O

ver 8

0,00

0 ho

urs

at G

RC

12

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

min

istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g–

Con

trolle

r dev

elop

men

t•

Flig

ht c

ontro

ller h

as b

een

parti

ally

des

igne

d•

Har

dwar

e ha

s no

t bee

n te

sted

, con

verto

rs

rem

ain

on te

st w

ith re

sear

ch c

ontro

llers

•N

ew d

irect

ion

is b

eing

pur

sued

in A

ctiv

e P

ower

Fa

ctor

Cor

rect

ion

cont

rolle

rs•

Con

trolle

r rem

ains

unp

rove

n–

Stir

ling

cryo

cool

ers

have

bee

n pl

aced

in fl

ight

•D

ata

is b

eing

acc

umul

ated

on

life

and

relia

bilit

y•

Less

ons

lear

ned

are

bein

g ap

plie

s w

here

ap

prop

riate

•C

riter

ion

for v

alid

atio

n of

life

and

relia

bilit

y ar

e be

ing

stud

ied

for p

ossi

ble

use

in p

ower

co

nver

sion

•Te

rrest

rial d

esig

ns h

ave

been

dep

loye

d,

accu

mul

ated

ove

r 44

milli

on h

ours

, dat

a is

sh

owin

g M

TBF

of o

ver 5

00,0

00 h

ours

–S

yste

m in

tegr

atio

n ha

s ad

vanc

ed to

a m

uch

high

er le

vel o

f det

ail

13

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

min

istra

tion

ww

w.n

asa.

gov

Dev

elop

men

t of S

tirlin

g•

Adv

ance

d te

chno

logy

–Th

is e

ffort

has

resu

lted

in a

6-fo

ld in

crea

se in

spe

cific

po

wer

of t

he S

tirlin

g co

nver

tor

–Tw

o fo

reru

nner

s of

the

Adv

ance

d te

chno

logy

co

nver

tor w

ere

able

to o

pera

te s

ucce

ssfu

lly a

t vi

brat

ion

leve

ls u

p to

24

grm

s, 0

.8 g

2 /Hz

–Th

e ad

vanc

ed te

chno

logy

cou

ld in

crea

se g

ener

ator

sp

ecifi

c po

wer

from

~4

W/k

g to

~8

W/k

g–

AP

FC c

ontro

llers

cou

ld re

duce

con

trolle

r mas

s an

d vo

lum

e•

Hav

e be

en s

ucce

ssfu

lly u

sed

in la

bora

tory

, nee

d to

be

mad

e fu

lly a

uton

omou

s, fl

ight

wor

thy

–M

odel

ing

now

has

tool

s to

redu

ce ti

me

and

risk

of

deve

lopm

ent

•C

FD to

inve

stig

ate

deta

ils o

f ope

ratio

n, a

ppea

rs v

alid

•SD

M to

inve

stig

ate

com

plet

e sy

stem

dyn

amic

in

tera

ctio

n, in

clud

ing

ther

mal

con

ditio

n, c

ontro

ller a

nd

end

user

load

14

Nat

iona

l Aer

onau

tics

and

Spac

e Ad

min

istra

tion

ww

w.n

asa.

gov

Con

clus

ion

•Th

e st

atus

of S

tirlin

g de

velo

pmen

t has

cha

nged

fund

amen

tally

si

nce

1999

with

dat

a at

han

d–

Ove

r 80,

000

hour

s of

ope

ratio

n of

pro

toty

pica

l har

dwar

e–

QA

sys

tem

und

erst

ood

incl

udin

g le

sson

s le

arne

d fro

m lo

ng li

fe

cyro

cool

erin

dust

ry–

Mat

eria

ls w

ell c

hara

cter

ized

for l

ong

life

and

high

relia

bilit

y (m

etal

lics

and

orga

nics

)–

Stru

ctur

al d

ynam

ics

test

s sh

ow s

ucce

ssfu

l ope

ratio

n at

hig

h le

vels

of

vibr

atio

n–

Crit

ical

com

pone

nt a

ging

has

bee

n m

odel

ed a

nd is

bei

ng v

alid

ated

–S

ucce

ss o

f Stir

ling

fligh

t cry

ocoo

lers

(and

long

-life

terr

estri

al u

nits

) pr

ovid

es s

uppo

rting

dat

a in

pow

er c

onve

rtor t

rans

ition

to fl

ight

–G

ener

ator

inte

grat

ion

succ

essf

ul fo

r lau

nch

load

s

•S

ome

area

s re

mai

n to

be

com

plet

ed, s

yste

m in

tegr

atio

n, fl

ight

co

ntro

ller,

exte

nded

ope

ratio

n of

inte

grat

ed g

ener

ator

, etc

•Th

ird g

ener

al p

hase

will

be

conc

lude

d w

ith s

ucce

ssfu

l sys

tem

in

tegr

atio

n of

free

-pis

ton

Stir

ling

into

a s

yste

m