waam mechanical properties · cast ti-6al-4v (mmpds) 14 all data is property of cranfielduniversity...
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www.cranfield.ac.uk
Mechanical properties
waammat.com
Updated 15th November 2017
®
WAAM is a registered trademark of Cranfield University
2All data is property of Cranfield University unless specified differently
The deposition strategies
Single pass
Parallel passes
Oscillation
Single pass
Parallel passes
Oscillation
Single pass
Parallel passes
Oscillation
3All data is property of Cranfield University unless specified differently
Ti64 // Cutting plan for static properties
a)
85
8 22
600
500
150
substrate
deposit
Z
XY
Z
YX
b)
locations of coupons
4All data is property of Cranfield University unless specified differently
Ti64 // Static properties
Directionality
750 800 850 900 950 1000Proof strength (MPa)
850
900
950
1000
1050
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Wrought AMS 4928
Vertical Additive AMS 4999
Horizontal Additive AMS 4999
Single Vert.Single Horiz.Par. Vert.Par. Horiz.Oscill. Vert.Oscill. Horiz.Plate
750 800 850 900 950 1000Proof strength (MPa)
6
8
10
12
14
16
18
20
22
24
26
Elon
gatio
n (%
)
Wrought AMS 4928
Vertical Horizontal Additive AMS 4999
Single Vert.Single Horiz.Par. Vert.Par. Horiz.Oscill. Vert.Oscill. Horiz.Plate
5All data is property of Cranfield University unless specified differently
Ti64 // Static properties
Average values
750 800 850 900 950 1000Proof strength (MPa)
860
880
900
920
940
960
980
1000
1020
1040
1060
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
SinglePar.Oscill.Plate
750 800 850 900 950 1000Proof strength (MPa)
6
8
10
12
14
16
18
20
22
Elon
gatio
n (%
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
SinglePar.Oscill.Plate
6All data is property of Cranfield University unless specified differently
Ti64 // Static properties with in-process cold work
Directionality
750 800 850 900 950 1000 1050Proof strength (MPa)
850
900
950
1000
1050
1100
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Cast ASTM F1108
Wrought AMS 4928Additive AMS 4999
Unrolled Vert.Unrolled Horiz.50 kN Vert.50 kN Horiz.75 kN Vert.75 kN Horiz.75 kN plasma Vert.75 kN plasma Horiz.Plate
750 800 850 900 950 1000 1050Proof strength (MPa)
6
8
10
12
14
16
18
20
22
24
26
Elon
gatio
n (%
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
Unrolled Vert.Unrolled Horiz.50 kN Vert.50 kN Horiz.75 kN Vert.75 kN Horiz.75 kN plasma Vert.75 kN plasma Horiz.Plate
7All data is property of Cranfield University unless specified differently
Ti64 // Static properties with in-process cold work
Average values
750 800 850 900 950 1000 1050Proof strength (MPa)
850
900
950
1000
1050
1100
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Cast ASTM F1108
Wrought AMS 4928Additive AMS 4999
Unrolled50 kN75 kN75 kN plasmaPlate
750 800 850 900 950 1000 1050Proof strength (MPa)
6
8
10
12
14
16
18
20
22
Elon
gatio
n (%
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
Unrolled50 kN75 kN75 kN plasmaPlate
8All data is property of Cranfield University unless specified differently
Ti64 // Comparison against other processes
Directionality
750 800 850 900 950 1000Proof strength (MPa)
850
900
950
1000
1050
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Wrought AMS 4928
Vertical Additive AMS 4999
Horizontal Additive AMS 4999
750 800 850 900 950 1000Proof strength (MPa)
5
10
15
20
25
30
35
Elon
gatio
n (%
)
Wrought AMS 4928
Vertical Horizontal Additive AMS 4999
WAAM Single V.WAAM Single H.WAAM Par. V.WAAM Par. H.WAAM Oscill. V.WAAM Oscill. H.Norsk Ti V.Norsk Ti H.Sciaky V.Sciaky H.Blown powder V.Blown powder H.Laser + wire V.Laser + wire H.Plate
• Norsk Ti from norsktitanium.com; Sciaky from Structure-property correlations for additively manufactured Ti-6Al-4V components produced using directed energy deposition processes, 2016 Proceedings of the 13th World Conference on Titanium
• Blown-powder from IREPA lasers
• Laser + Wire from “Additive Manufacturing of Ti-6Al-4V: Relationship between Microstructure, Defects and Mechanical Properties”, Pia Akerfeldt, PhD Thesis, Lulea
9All data is property of Cranfield University unless specified differently
Ti64 // Comparison against other processes
Average values
• Norsk Ti from norsktitanium.com; Sciaky from Structure-property correlations for additively manufactured Ti-6Al-4V components produced using directed energy deposition processes, 2016 Proceedings of the 13th World Conference on Titanium
• Blown-powder from IREPA lasers
• Laser + Wire from “Additive Manufacturing of Ti-6Al-4V: Relationship between Microstructure, Defects and Mechanical Properties”, Pia Akerfeldt, PhD Thesis, Lulea
800 850 900 950 1000Proof strength (MPa)
860
880
900
920
940
960
980
1000
1020
1040
1060
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
WAAM SingleWAAM Par.WAAM Oscill.Norsk TiSciakyBlown powderLaser + wirePlate
800 850 900 950 1000Proof strength (MPa)
6
8
10
12
14
16
18
20
22
24
26
28
Elon
gatio
n (%
)
Cast ASTM F1108
Wrought AMS 4928
Additive AMS 4999
WAAM SingleWAAM Par.WAAM Oscill.Norsk TiSciakyBlown powderLaser + wirePlate
10All data is property of Cranfield University unless specified differently
Ti64 // Fatigue durability
High cycle fatigue, Kt = 1 and Kt = 2.3
103 104 105 106 107 108
Cycles to failure
0
100
200
300
400
500
600
700
800
900
1000
Max
stre
ss (M
Pa)
R = 0.1, Kt = 1
As-dep Vert.As-dep Vert. (run-off)As-dep Horiz.As-dep Horiz. (run-off)Wrought measured by PetersWrought measured by Peters (trendline)Lamellar by Peters Property of Airbus
11All data is property of Cranfield University unless specified differently
Ti64 // Damage tolerance
Fatigue crack growth rate (single bead, without and with cold-work)
10 100"K (MPa m1=2)
10-8
10-7
10-6
10-5
da/d
N(m
/cy
cle)
R = 0.1
No in-process cold-work
WAAM: crack across layersWAAM: crack along layersWrought Ti-6Al-4V (L-T measured)Wrought Ti-6Al-4V (T-L measured)Wrought Ti-6Al-4V (L-T MMPDS)Cast Ti-6Al-4V (MMPDS)
10 100"K (MPa m1=2)
10-9
10-8
10-7
10-6
10-5
10-4
da/
dN
(m/c
ycle) In-process cold-worked at 75 kN
WAAM: crack across layers 1 (R = 0.5)WAAM: crack across layers 2 (R = 0.5)WAAM: crack along layers 1 (R = 0.5)WAAM: crack along layers 2 (R = 0.5)Wrought NASA CR2319 (R = 0.5)
12All data is property of Cranfield University unless specified differently
Ti64 // Damage tolerance
Fatigue crack growth rate (parallel and oscillated)
10 100"K (MPa m1=2)
10-9
10-8
10-7
10-6
10-5
10-4
da/d
N(m
/cy
cle)
R = 0.1
No in-process cold-work
Parallel dep. strategy
WAAM: crack across layers Test 1WAAM: crack across layers Test 2WAAM: crack along layers Test 1WAAM: crack along layers Test 2Wrought Ti-6Al-4V (L-T MMPDS)Cast Ti-6Al-4V (MMPDS)
10 100"K (MPa m1=2)
10-9
10-8
10-7
10-6
10-5
10-4
da/d
N(m
/cycle)
R = 0.1
No in-process cold-work
Oscillation dep. strategy
WAAM: crack across layers Test 1WAAM: crack across layers Test 2WAAM: crack along layers Test 1WAAM: crack along layers Test 2Wrought Ti-6Al-4V (L-T MMPDS)Cast Ti-6Al-4V (MMPDS)
13All data is property of Cranfield University unless specified differently
Ti64 // Damage tolerance
Recap FCGR
10 100"K (MPa m1=2)
10-9
10-8
10-7
10-6
10-5
10-4
da/dN
(m/cycle) No in-process cold-work
R = 0.1
All dep. strategies
Single, crack across layers Test 1Single, crack along layers Test 1Parallel, crack across layers Test 1Parallel, crack along layers Test 1Oscill., crack across layers Test 1Oscill., crack along layers Test 1Wrought Ti-6Al-4V (L-T MMPDS)Cast Ti-6Al-4V (MMPDS)
14All data is property of Cranfield University unless specified differently
Ti64 // Damage tolerance
Fracture toughness
0
10
20
30
40
50
60
70
80
90
100
K Q o
r KIC
(MPa
m1/
2 )
Across the layersAlong the layers
Grade 5parallel
Grade 5oscillated
Grade 23parallel
WroughtRef: MMPDS
thickness > 25 mmplane strain cond.
Wroughtthis research
15All data is property of Cranfield University unless specified differently
Ti64 // Properties at the interface
• Case 3: symmetric structure
• Case 2: plate at the bottom
• Case 1: fully sacrificial
16All data is property of Cranfield University unless specified differently
Ti64 // Crack growth trajectory at the interface
AM
SubstrateCrack trajectory
maintains almost a straight line
AM
Substrate
Crack trajectory maintains almost a
straight line
substrate
buildingdirection40
87.5 84
60
120
445
40
33
WAAM material
interface
A B CD
E
17All data is property of Cranfield University unless specified differently
Ti64 // Crack growth trajectory at the interface
substrate
buildingdirection40
87.5 84
60
120
445
40
33
WAAM material
interface
A B CD
E
10 100"K (MPa m1=2)
10-8
10-7
10-6
10-5
da/
dN
(m/cy
cle)
Type AType BType CType DType EWrought Ti-6Al-4V (L-T)Cast Ti-6Al-4V
10 100"K (MPa m1=2)
10-8
10-7
10-6
10-5
da/dN
(m/c
ycle)
Type AType BType CType DType EWAAM: crack across layersWAAM: crack along layers
18All data is property of Cranfield University unless specified differently
“Other” titanium alloys (tensile test in progress)
• Ti-5Al-5Mo-5V-3Cr (5553)• à UTS up to 1300 MPa
• Ti64 with 2000ppm O2• à + 500ppm O2 = + 70 Mpa
• Ti64 coated with TiB2• à grain refinement
• Timetal 407• à medium strength, high ductility• à energy absorption = 1.6 x Ti64• à machinability = 2 x Ti64
352.1 367.3 353.0
416.22
270.09
Vickers HardnessTi 64 Ti 64 high O2 TiB2 coated Ti 5553 Ti 407
20All data is property of Cranfield University unless specified differently
Aluminium 2024
All values measured in the horizontal direction
150 200 250 300 350 400 450Proof strength (MPa)
250
300
350
400
450
500
Ultim
ate
tens
ile st
reng
th (M
Pa)
Unroll.Unroll. T615 kN30 kN45 kN45 kN T6Wrought T6
150 200 250 300 350 400 450Proof strength (MPa)
7
8
9
10
11
12
13
Elon
gatio
n (%
)
Unroll.Unroll. T615 kN30 kN45 kN45 kN T6Wrought T6
21All data is property of Cranfield University unless specified differently
Aluminium 2319
Average values
120 140 160 180 200 220 240 260 280 300 320Proof strength (MPa)
260
280
300
320
340
360
380
400
420
440
460
Ultim
ate
tens
ile st
reng
th (M
Pa)
Unroll.Unroll. T615 kN30 kN45 kN45 kN T6Wrought T6
120 140 160 180 200 220 240 260 280 300 320Proof strength (MPa)
7
8
9
10
11
12
13
14
15
16
17
Elon
gatio
n (%
)
Unroll.Unroll. T615 kN30 kN45 kN45 kN T6Wrought T6
22All data is property of Cranfield University unless specified differently
Aluminium Safra 66 / ZL205A
Thin walls (single beads)
100 150 200 250 300 350 400 450Proof strength (MPa)
200
250
300
350
400
450
500
550
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Desirable
Safra 66 Vert.Safra 66 Horiz.Safra 66 Rolled Vert.Safra 66 Rolled Horiz.ZL205A Vert.ZL205A Horiz.ZL205A Rolled Vert.ZL205A Rolled Horiz.ZL205A + T6 Vert.ZL205A + T6 Horiz.ZL205A Rolled + T6 Vert.ZL205A Rolled + T6 Horiz.
100 150 200 250 300 350 400 450Proof strength (MPa)
0
5
10
15
20
25
30
Elon
gatio
n (%
)
DesirableSafra 66 Vert.Safra 66 Horiz.Safra 66 Rolled Vert.Safra 66 Rolled Horiz.ZL205A Vert.ZL205A Horiz.ZL205A Rolled Vert.ZL205A Rolled Horiz.ZL205A + T6 Vert.ZL205A + T6 Horiz.ZL205A Rolled + T6 Vert.ZL205A Rolled + T6 Horiz.
23All data is property of Cranfield University unless specified differently
Aluminium Safra 66 / ZL205A
Thick walls
50 100 150 200 250 300 350 400 450Proof strength (MPa)
150
200
250
300
350
400
450
500
550
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Desirable
Safra 66 Oscill. Vert.Safra 66 Oscill. Horiz.Safra 66 Parallel Vert.Safra 66 Parallel Horiz.ZL205A Oscill. Vert.ZL205A Oscill. Horiz.ZL205A Oscill. + T4 Vert.ZL205A Oscill. + T4 Horiz.ZL205A Oscill. + T6 Vert.ZL205A Oscill. + T6 Horiz.ZL205A Parallel Vert.ZL205A Parallel Horiz.ZL205A Parallel + T4 Vert.ZL205A Parallel + T4 Horiz.ZL205A Parallel + T6 Vert.ZL205A Parallel + T6 Horiz.
50 100 150 200 250 300 350 400 450Proof strength (MPa)
0
5
10
15
20
25
30
35
40
Elon
gatio
n (%
)
Desirable
Safra 66 Oscill. Vert.Safra 66 Oscill. Horiz.Safra 66 Parallel Vert.Safra 66 Parallel Horiz.ZL205A Oscill. Vert.ZL205A Oscill. Horiz.ZL205A Oscill. + T4 Vert.ZL205A Oscill. + T4 Horiz.ZL205A Oscill. + T6 Vert.ZL205A Oscill. + T6 Horiz.ZL205A Parallel Vert.ZL205A Parallel Horiz.ZL205A Parallel + T4 Vert.ZL205A Parallel + T4 Horiz.ZL205A Parallel + T6 Vert.ZL205A Parallel + T6 Horiz.
24All data is property of Cranfield University unless specified differently
Aluminium 4043 and 5087
Average values
60 80 100 120 140 160 180 200 220 240Proof strength (MPa)
160
180
200
220
240
260
280
300
320
340
360
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
404350875087 + rolling
60 80 100 120 140 160 180 200 220 240Proof strength (MPa)
19
19.5
20
20.5
21
21.5
22
Elon
gatio
n (%
)
404350875087 + rolling
25All data is property of Cranfield University unless specified differently
Picking the right alloy
Average values
100 150 200 250 300 350 400 450Proof strength (MPa)
200
250
300
350
400
450
500
550
600
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
100 150 200 250 300 350 400 450Proof strength (MPa)
6
8
10
12
14
16
18
20
22
Elon
gatio
n (%
)
2024 Single 2024 Single T6 2024 15 kN 2024 30 kN 2024 45 kN 2024 45 kN T6 2024 Wrought T6
2319 Single 2319 Single T6 2319 15 kN 2319 30 kN 2319 45 kN 2319 45 kN T6 2319 Wrought T6
5087 Single 5087 Rolled
27All data is property of Cranfield University unless specified differently
Steels (work in progress)
Average values
400 600 800 1000 1200 1400 1600 1800Proof strength (MPa)
500
1000
1500
2000
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
ER70S-6ER80S-Ni1ER90S-B3ER120Mar. steel 250Mar. steel 250 HTMar. steel 350Mar. steel 350 HT
400 600 800 1000 1200 1400 1600 1800Proof strength (MPa)
5
10
15
20
25
30
35
Elon
gatio
n (%
)
ER70S-6ER80S-Ni1ER90S-B3ER120Mar. steel 250Mar. steel 250 HTMar. steel 350Mar. steel 350 HT
28All data is property of Cranfield University unless specified differently
Stainless steels
Directionality
200 300 400 500 600 700 800 900Proof strength (MPa)
500
600
700
800
900
1000
1100
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
17-4 PH Vert.17-4 PH Horiz.316L Vert.316L Horiz.
200 300 400 500 600 700 800 900Proof strength (MPa)
10
15
20
25
30
35
40
45
Elon
gatio
n (%
)
17-4 PH Vert.17-4 PH Horiz.316L Vert.316L Horiz.
30All data is property of Cranfield University unless specified differently
Inconel® 718
CMT (brushed = mechanical cleaning of surface prior to successive layer)
300 400 500 600 700 800 900 1000 1100 1200Proof strength (MPa)
700
800
900
1000
1100
1200
1300
1400
1500
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
CMT
AMS 5662 and 5663 Bars, Forgings, & Rings
As-Dep Vert.As-Dep Horiz.As-Dep Vert. (diff. wire)As-Dep Horiz. (diff. wire)As-Dep (brushed) Vert. (diff. wire)As-Dep (brushed) Horiz. (diff. wire)Solutionised Vert.Solutionised Horiz.HT Vert.HT Horiz.
300 400 500 600 700 800 900 1000 1100 1200Proof strength (MPa)
10
15
20
25
30
35
40
45
50
Elon
gatio
n (%
)
CMT
AMS 5662 and 5663 Bars, Forgings, & Rings
As-Dep Vert.As-Dep Horiz.As-Dep Vert. (diff. wire)As-Dep Horiz. (diff. wire)As-Dep (brushed) Vert. (diff. wire)As-Dep (brushed) Horiz. (diff. wire)Solutionised Vert.Solutionised Horiz.HT Vert.HT Horiz.
31All data is property of Cranfield University unless specified differently
Inconel® 718
Plasma (including cold-work)
300 400 500 600 700 800 900 1000 1100 1200Proof strength (MPa)
600
700
800
900
1000
1100
1200
1300
1400
Ulti
mat
e te
nsile
stre
ngth
(MPa
)
Plasma
AMS 5662 and 5663 Bars, Forgings, & Rings
As-Dep Vert.As-Dep Horiz.Solutionised Vert.Solutionised Horiz.HT Vert.HT Horiz.Rolled @ 75 kN Vert.Rolled @ 75 kN Horiz.Rolled @ 75 kN + solut. Vert.Rolled @ 75 kN + solut. Horiz.Rolled @ 75 kN + HT Vert.Rolled @ 75 kN + HT Horiz.
300 400 500 600 700 800 900 1000 1100 1200Proof strength (MPa)
10
15
20
25
30
35
40
45
50
Elon
gatio
n (%
)
Plasma
AMS 5662 and 5663 Bars, Forgings, & Rings
As-Dep Vert.As-Dep Horiz.Solutionised Vert.Solutionised Horiz.HT Vert.HT Horiz.Rolled @ 75 kN Vert.Rolled @ 75 kN Horiz.Rolled @ 75 kN + solut. Vert.Rolled @ 75 kN + solut. Horiz.Rolled @ 75 kN + HT Vert.Rolled @ 75 kN + HT Horiz.