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Abstract for submission to Fall MS&T06 Symposium ”Phase Stability, Diffusion and Their Applications” Phase Stability of a Powder Metallurgy Disk Superalloy T. P. Gabb, J. Gayda, P. Kantzos, J. Telesman Advanced powder metallurgy superalloy disks in aerospace turbine engines now entering service can be exposed to temperatures approaching 700°C, higher than those previously encountered. They also have higher levels of refractory elements, which can increase mechanical properties at these temperatures but can also encourage phase instabilities during service. Microstructural changes including precipitation of topological close pack phase precipitation and coarsening of existing γ precipitates can be slow at these temperatures, yet potentially significant for anticipated disk service times exceeding 1,000 h. The ability to quantify and predict such potential phase instabilities and degradation of capabilities is needed to insure structural integrity and air worthiness of propulsion systems over the full life cycle. A prototypical advanced disk superalloy was subjected to high temperature exposures, and then evaluated. Microstructural changes and corresponding changes in mechanical properties were quantified. The results will be compared to predictions of microstructure modeling software.

Abstract for submission to Fall MS&T06 Symposium ”Phase

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Abstract for submission to Fall MS&T06 Symposium ”Phase Stability, Diffusion and Their Applications”

Phase Stability of a Powder Metallurgy Disk Superalloy

T. P. Gabb, J. Gayda, P. Kantzos, J. Telesman Advanced powder metallurgy superalloy disks in aerospace turbine engines now entering service can be exposed to temperatures approaching 700°C, higher than those previously encountered. They also have higher levels of refractory elements, which can increase mechanical properties at these temperatures but can also encourage phase instabilities during service. Microstructural changes including precipitation of topological close pack phase precipitation and coarsening of existing γ ′ precipitates can be slow at these temperatures, yet potentially significant for anticipated disk service times exceeding 1,000 h. The ability to quantify and predict such potential phase instabilities and degradation of capabilities is needed to insure structural integrity and air worthiness of propulsion systems over the full life cycle. A prototypical advanced disk superalloy was subjected to high temperature exposures, and then evaluated. Microstructural changes and corresponding changes in mechanical properties were quantified. The results will be compared to predictions of microstructure modeling software.

1

Nat

iona

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Gle

nn R

esea

rch

Cen

ter

Phas

e St

abili

ty o

f a P

owde

r Met

allu

rgy

Dis

k Su

pera

lloy

Tim

Gab

b, J

. Gay

da, J

. Tel

esm

an, A

. Gar

g, P

. Kan

tzos

Phas

e St

abili

ty, D

iffus

ion

and

Thei

r App

licat

ions

Mat

eria

ls S

cien

ce &

Tec

hnol

ogy

2006

O

ctob

er 1

8, 2

006

2

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nn R

esea

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Cen

ter

Bac

kgro

und

-Pow

der m

etal

lurg

y pr

oces

sing

of d

isk

supe

rallo

ysal

low

s hi

gher

le

vels

of s

tren

gthe

ning

ele

men

ts fo

r inc

reas

ed te

mpe

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re

capa

bilit

ies

-Adv

ance

d du

al m

icro

stru

ctur

e he

at tr

eatm

ents

(DM

HT)

can

als

o be

app

lied

to p

rodu

ce o

ptim

al g

rain

siz

e vs

. loc

atio

n an

d as

soci

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tem

pera

ture

/str

ess

1)Fi

ne g

rain

siz

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bor

e an

d w

eb s

ectio

ns fo

r hig

h st

reng

th

and

fatig

ue re

sist

ance

up

to 5

00°C

2)C

oars

e gr

ain

size

in th

e rim

for h

igh

cree

p an

d cr

ack

grow

th re

sist

ance

at 7

00°C

+

DM

HT

Dis

k10

mm

Gra

in S

ize

= 4

.5 μ

mG

rain

Siz

e =

34 μ

m

Supe

rsol

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Rim

Subs

olvu

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10 μ

m10

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Stat

emen

t of P

robl

em

The

long

term

sta

bilit

y of

a D

MH

T ri

m’s

mic

rost

ruct

ure

at70

0°C

+ is

a c

once

rn-

Com

mer

cial

sof

twar

e pr

edic

ts p

reci

pita

tion

of h

arm

ful p

hase

s fo

rDM

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allo

y (L

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nges

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cipi

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Thes

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ight

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rain

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How

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ld th

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pert

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d lim

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e at

thes

e te

mpe

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res

-G

rain

bou

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ies

are

ofte

n fa

ilure

site

s he

re :

enha

nced

effe

cts?

TCP

Phas

esγ′C

oars

enin

g

4

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Cen

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Obj

ectiv

e

Ass

ess

the

long

term

sta

bilit

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rim

mec

hani

cal p

rope

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s an

d m

icro

stru

ctur

eat

704

°C

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Pres

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on

mic

rosc

opy

-In

itial

resu

lts fo

r exp

osur

es a

t 704

°C u

p to

5,0

00 h

will

be

pres

ente

d

5

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Mat

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Pro

cedu

reA

lloy:

NA

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Con

solid

atio

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rgon

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xtru

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reat

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Rat

es

Gra

in S

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10 m

m

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in S

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= 4

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m

BB

BB

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rsol

vus

Rim

Subs

olvu

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ore

10 μ

m10

μm

6

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Gle

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Cen

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Effe

cts

of E

xpos

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at 7

04°C

on

Tens

ile P

rope

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s

Incr

easi

ng e

xpos

ures

did

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sev

erel

y de

grad

e pr

oper

ties

Res

ults

7

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Effe

cts

of E

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at 7

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ss R

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e st

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rela

xatio

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704°

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t 1%

Str

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8

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Incr

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sist

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Effe

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on

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Dw

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rack

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wth

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nce

0 h

1,00

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terg

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wth

in a

ll ca

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0 se

c D

wel

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ter

Wha

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the

asso

ciat

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Cha

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wth

: m

odes

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prov

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t

10

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Min

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hase

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e D

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and

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Sig

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antly

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Expo

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b)C

11

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Seco

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y γ′P

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able

With

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γ′

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mic

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0 h

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Seco

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Tert

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Seco

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in b

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Tert

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γ′

mic

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mic

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mic

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mic

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mic

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0 h

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Seco

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yγ′

Tert

iary

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13

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Com

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γ′

Coa

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Thro

ugho

ut M

icro

stru

ctur

e A

ppea

rs M

ost

Clo

sely

Ass

ocia

ted

With

The

Obs

erve

d Pr

oper

ty C

hang

es

Tert

iary

coa

rsen

ing

appe

ars

near

t1/3

LSW

* dep

ende

nce

Tert

iary

γ′

*Lifs

hitz

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in

Bou

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fect

Gra

in

Bou

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fect

14

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Gle

nn R

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Cen

ter

Sum

mar

y an

d C

oncl

usio

ns

The

long

term

, hig

h te

mpe

ratu

re s

tabi

lity

of th

e D

MH

T rim

’s

mic

rost

ruct

ure

at70

0°C

+ ap

pear

s pr

omis

ing

so fa

r:M

echa

nica

l Pro

pert

ies

-Te

nsile

pro

pert

ies,

tim

e-de

pend

ent p

rope

rtie

s in

dica

te

expo

sure

s pr

oduc

ed a

slig

htly

mor

e fo

rgiv

ing

mat

eria

lM

icro

stru

ctur

e-

No

harm

ful p

hase

s fo

und

so fa

r, de

spite

mod

el p

redi

ctio

ns-

γ′p

hase

fairl

y st

able

, with

onl

y te

rtia

ry p

reci

pita

te c

oars

enin

g-

Gra

in b

ound

ary

mic

rost

ruct

ure

likew

ise

stab

le s

o fa

r M

icro

stru

ctur

e-Pr

oper

ties

-Ex

posu

re e

ffect

s on

mec

hani

cal p

rope

rtie

s ap

pear

ass

ocia

ted

with

coa

rsen

ing

of te

rtia

ry γ′t

hrou

ghou

t mic

rost

ruct

ure

-Se

cond

ary γ′s

ize

appe

ars

larg

ely

set t

hrou

gh s

olut

ion

heat

tr

eat c

oolin

g pa

th, n

ote

this

was

pre

viou

sly

show

n to

als

o ef

fect

thes

e pr

oper

ties

-A

pplic

atio

n of

diff

eren

t sta

rtin

g he

at tr

eatm

ents

and

oth

ersu

bseq

uent

exp

osur

es a

nd s

tres

s co

uld

alte

r the

se fi

ndin

gs

15

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nn R

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Cen

ter

Futu

re W

ork

-Tr

ansm

issi

on e

lect

ron

mic

rosc

opy

will

be

used

to m

ore

clos

ely

stud

y te

rtia

ry γ′c

hang

es-

Hig

her t

empe

ratu

res,

mor

e ex

posu

re ti

mes

will

be

expl

ored

-Ex

posu

res

unde

r str

ess

are

plan

ned,

to m

ore

clos

ely

sim

ulat

e st

ress

ed tu

rbin

e di

sk lo

catio

ns-

The

effe

cts

of d

iffer

ent h

eat t

reat

men

ts (c

oolin

g ra

tes

and

ages

) on

sub

sequ

ent e

xpos

ure

resp

onse

als

o ne

ed to

be

cons

ider

ed-

Mod

elin

g of

thes

e ef

fect

s is

als

o ge

tting

und

erw

ay