Modelling the Effects of Surface Residual Stresses on Fatigue Behavior of PM Disk Alloys

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,943.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
NNX11CD72P
Award Id:
n/a
Agency Tracking Number:
104633
Solicitation Year:
2010
Solicitation Topic Code:
A1.01
Solicitation Number:
n/a
Small Business Information
OH, Parma Heights, OH, 44130-3821
Hubzone Owned:
N
Minority Owned:
Y
Woman Owned:
N
Duns:
123834959
Principal Investigator:
JohnGayda, Jr.
Principal Investigator
(440) 845-7020
johngaydajr@yahoo.com
Business Contact:
VinodNagpal
Business Official
(440) 845-7020
vnagpal@nrengineering.com
Research Institute:
n/a
Abstract
A finite element based model will be developed and validated to capture the evolution of residual stresses and cold work at machined features of compressor and turbine powder metallurgy superalloy disks. The focus will be to quantify, model and validate residual stress and cold work evolution at stress concentration features during simulated service in aerospace gas turbine engine disk materials. This will be accomplished by first utilizing existing NASA Test data. If the existing test data are insufficient, a minimum number of specimens will be tested if the resources permit. These specimens will have varied surface finish conditions to be determined in consultation with NASA personnel and will be tested using a thermal mechanical load history that will simulate the operating conditions of new generation of gas turbine engines and include the effect of superimposed dwell cycles. The deliverables will include effects of service history on residual stress and cold work depth profile evolutions within notches, and analytical modeling descriptions of the evolution of these parameters as a function of simulated service history. Also included will be models and algorithms extrapolating the predicted residual stresses and cold work to service conditions outside of those tested during the program.

* information listed above is at the time of submission.

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