SBIR/STTR Research Award
Development Technology for a Stepped Diameter TMC Shaft
Award amount
$749,890Program and phase
SBIR · Phase IIAward year
2005Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- WOODBINE LABS, INC.
- Proposal award date
- 2005-05-09
- Contract end date
- 2007-09-09
- UEI
- Not reported
- Solicitation number
- 2004.1
- Topic code
- AF04-188
Research abstract
This proposal is to develop and demonstrate technologies for a JSF TMC shaft. Two possible JSF TMC shaft configurations are possible. One is a large diameter, thick wall, very high torque, bottle shaped LP shaft that transmits torque from the LP turbine to both the engine’s fan and an in-line lift-fan-shaft. The other is a stepped configuration inner shaft of a counter rotating engine-system. The first is for use in a lighter weight design of the current JSF engine and the second for use in a redesigned, significantly lighter weight, counter rotating JSF engine. A Phase I SBIR is studying design and manufacturing approaches applicable to the forward and aft ends of a TMC stepped shaft for the JSF engine and the GE/VAATE counter-rotating engine. Issues associated with using TMCs for a very high torque, thick walled, application are being successfully addressed under a Phase II SBIR program titled “Thick-Wall Oriented-Fiber TMC Shaft Development”. This proposal is for a Phase II follow-on to the above Phase I TMC Stepped Shaft Program. It will provide detailed analytical derivations, scale-up-development and prototypical device demonstrations, as well as develop a technology transition plan for future systems and commercial ventures.
Technology keywords
Not reported
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