SBIR/STTR Research Award

Restoration of Dimensional Tolerances

Award identifier 27b1fd630bb4d35cb5e6318c32ccd2fdccf1a5d7175e50d86b238bcde33cbee9Awarding agency Department of Defense · Air Force

Award amount

$99,968

Program and phase

SBIR · Phase I

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ENGINEERING AND SOFTWARE SYSTEM SOLUTIONS, INC.
Proposal award date
2008-04-30
Contract end date
2009-01-30
UEI
X13SUGQE8VG6
Solicitation number
2007.3
Topic code
AF073-115

Research abstract

When the inner diameter (ID) of aluminum landing gear outer cylinders is worn or damaged there is very little that can be done to repair the damage consequently the outer cylinder has to be condemned and taken out of service. The aircraft industry condemns many aluminum strut outer cylinders at a high cost. The cost to the USAF alone is of approximately $3M per years. The main cause for condemnations is that the ID of the cylinders is over sized due to wear or a deep scratch cause by failure of an internal component. Chrome plating and various thermal sprays can be used to repair steel outer cylinders when they are damaged, unfortunately there is very little that can be done to repair a hard anodized surface. A coating repair which builds up thickness and can be machined /ground to size, like chrome plating, for aluminum cylinder IDs would be a great value to the aircraft industry. The coating would have to be able to seal hydraulic fluid and high pressure nitrogen. It would also have to be able to handle high loads without spalling off. If a repair method could be developed then a considerable savings could be realized by the aircraft as well as improved supportability to the fleet. Physical Vapor Deposition (PVD) or magnetron sputtering technology has the potential to apply the same series of aluminum onto worn aluminum outer cylinders and possibly other aluminum parts. Magnetron sputtering process is currently used to apply thin coatings (0.001 inches) of aluminum on steel landing gear parts for corrosion. This process can be modified to be able to apply thick coatings (0.008-0.010 inches) of same series aluminum onto the ID of aluminum outer cylinders. This coating then can be machine, anodized and honed to bring the outer cylinder back to serviceable condition.

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

110 SBIR/STTR records share this UEI (2007–2025). Reported award amounts total $101,039,446. Reported amounts are not federal obligations.

Phases: Phase II, Phase I, Phase II – Direct to Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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