SBIR/STTR Research Award

Useful Life Remaining Models for Turbine Engine Hot Section Components

Award identifier 97c24f2cbe4913f440f65f67f56c1544bce69ad3715b66d772aa33be979ead12Awarding agency Department of Defense · Navy

Award amount

$69,994

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
ROTORDYNAMICS-SEAL RESEARCH
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

A new advanced transient, nonlinear dynamic simulation technology is proposed for determining the operating characteristics of the gas turbine engine based on actual flight data and in-flight measurements. The analysis results are used to determine theuseful life remaining for each component in the engine. Improved engine maintenance procedures. Improved understanding of engine operating characteristics and events that lead to life limiting damage.

Technology keywords

Not reported

Agency intelligence

Department of Defense

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