SBIR/STTR Research Award

SMART SNUBBER/DAMPER FOR FIVE FOLD INCREASE IN DAMPING OF BEARINGLESS MAIN ROTOR BLADES

Award identifier 575a5872969fd475a4353e454aac01f778de189643b9adf2f4f1f0c814ba8b48Awarding agency Department of Defense · Army

Award amount

$120,000

Program and phase

SBIR · Phase I

Award year

2004

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
Materials Technologies Corporation
Proposal award date
2003-12-11
Contract end date
2004-06-10
UEI
MC9CPJ8DFPE3
Solicitation number
2003.2
Topic code
A03-073

Research abstract

Snubber/damper damping performance is severely limited by component size and load constraints yielding insufficient RLM damping. Solutions using existing technology lead to excessive snubber damper size and weight to accommodate all operating conditions. Also, current snubber/damper designs are not sufficiently reliable and have limited life. High damping is required for stabilizing ground and air-resonance (rotating frequency of interest typically 0.3-0.7P). However, simply increasing the damping of snubber/dampers designs will also increases the 1P lead-lag associated loads and reduce related component lives One solution to the above problem would be to design a ¡smart¡" snubber-damper that takes advantage of the superimposed 1P motions by producing damping forces that oppose ƒçlag motions but produce zero or low force when the net damper loads are not favorable for suppressing ƒçlag motions. This is not possible using conventional passive dampers because passive elements like relief valves, orifices, produce forces that oppose the net velocity even if the resulting force excites the regressive lag mode! The new active concept arises from the recognition that the net damper force, i.e. from the combined ƒçlag and 1P motions, often produces forces that can be advantageously used to suppress ƒçlag response, thus converting a chronic difficulty in damper technology, unwanted 1P motions, into a benefit. The proposed concept relies upon two actions: 1) Minimizing the net damper force when it is in the same direction as the ƒçlag velocity. This avoids adding energy to the ƒçlag mode. This would be done by selectively opening a controlled valve to equalize the pressure in the damper chambers thus not allowing pressures to build. 2) Maximizing the net damper force when it opposes the ƒçlag velocity. This would extract energy from the ƒçlag mode. This would be done by selectively closing a controlled valve to maximize the damper load.

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

48 SBIR/STTR records share this UEI (1988–2022). Reported award amounts total $11,941,405. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

Department of Defense

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