SBIR/STTR Research Award

Composite Bearing Damper for Advanced Gas Turbine Engines

Award identifier d7c2736e2eda974638e431c490c1a6fc4f94bbe3ea1f5187d01039c75778e243Awarding agency Department of Defense · Army

Award amount

$69,669

Program and phase

SBIR · Phase I

Award year

1996

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Award details

Awarding agency
Department of Defense
Branch
Army
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 high temperature passive damping system is proposed for application to gas turbine engines. This dry-type damper eliminiates the need for lubricant to provide squeeze film damping. THE VENAM (tm) damper consists of a high temperature, high stiffness, composite material with vitreous enamel interlayers, which will dissipate vibrational energy viscoelastically. The effort proposed herein will concentrate on design and fabrication of a prototype damper for a typical gas turbine application and component testing to prove the feasibility of the concept. Elimination of oil lubricated systems from gas turbine engines.

Technology keywords

Not reported

Agency intelligence

Department of Defense

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