SBIR/STTR Research Award

Robust Solid Lubricant Coating for Gears of Cryogenic Fuel Turbopumps

Award identifier d294de82b44b8e931ec4a63fffab3bea25bd20e84f7e304a210c1b7790fe26c1Awarding agency Department of Defense · Air Force

Award amount

$906,161

Program and phase

SBIR · Phase II

Award year

2006

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Tribologix Inc
Proposal award date
2006-04-24
Contract end date
2009-04-24
UEI
DB6LEDJJVKS6
Solicitation number
2005.1
Topic code
AF05-131

Research abstract

Our advanced surface engineering technologies provide new and broader operating windows for moving mechanical parts in extreme environments. Several of our advanced solid film lubricant coating technologies have been successfully evaluated as viable candidates for RL-10 rocket engine turbopumps. The turbomachinery used for rocketry operate under extreme conditions with a zero fault tolerance. Gears and bearings operate at high speeds and high contact pressures at cryogenic temperatures. Based on our Phase I results a significant improvement in turbopump operation is possible. Improvements in coating uniformity, structure, wear life with a reduction in friction and vibrations yield improved turbopump operations. This study details specific cryogenic testing and laboratory characterization at appropriate loads and speeds similar to that of rocket fuel pump. Cryogenic WAM testing is used to provide the proper tribological test conditions. Coating compatibility with liquid propelent is investigated. Advanced coatings include PVD, Spray, Burnish and Smart Surface Laser Textured solid film lubes and Soft Metallic coatings by PVD and Hybrid PVD. We deliver a reference database of our advanced surface engineering treatments as well as surface treatment of the RL-10 bearing sleeve and turbopump gear based on our results with deliberate concern for economic industrial viability. We provide a compiled matrix of tribological solutions to choose from based on operational level requirements. By working closely with Pratt & Whitney during our Phase I effort and as well as during this research project on technical issues and risk analysis we shall do our first engine test third quarter of 2006 on a bearing sleeve, followed by further engine testing with our new technology on turbopump gears. An incremental approach for insertion of our technology in to full production requires a well executed project flow from Research to Development to PWA Certified Production. We shall also work with Pratt Whitney for process certification.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

8 SBIR/STTR records share this UEI (2005–2016). Reported award amounts total $3,595,836. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: Department of Defense

Agency intelligence

Department of Defense

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