SBIR/STTR Research Award

Smart Autonomous Miniaturized Contamination Condition Sensor with Embedded Prognostics

Award identifier e41e415b61c4afed07eb23ea3ed706a77b658f22ec7462de7c37fd74cc55d062Awarding agency Department of Defense · Army

Award amount

$69,831

Program and phase

SBIR · Phase I

Award year

2007

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
Benz Airborne Systems
Proposal award date
2007-10-11
Contract end date
2008-04-30
UEI
W8J7VHEVCJV9
Solicitation number
2007.2
Topic code
A07-008

Research abstract

The U.S. Army Aviation Engineering Directorate, Propulsion Drive Systems Branch, has identified the need to replace the antiquated, differential mechanical pressure switch/indicator currently being used in hydraulic system filter applications on all Army helicopters, in favor of newer technology, MEMS based, piezoresistive, solid-state differential pressure transducer with temperature sensing combination for the added benefit of performing self diagnostics and prognostics capabilities to increase aircraft maintainability. The current mechanical design dates back 40 years, does not have temperature sensing capabilities, is incapable of processing information, or from being used for diagnostics and prognostics purposes for condition based maintenance, and it’s inherent configuration makes it unreliable and problematic for users in the field, resulting in numerous false readings and premature component removals. In support of this effort, based on discussions with the U.S. Army’s Aviation Engineering Directorate, Benz Airborne is proposing to develop a multi-platform concept for a diagnostic and prognostic measurement system (DPMS) that, if successful, could be used on all Army helicopters. The Propulsions Drive Systems Branch envisions this pressure transducer with temperature sensor capability, to be a drop in, stand alone replacement for the current mechanical switch. In addition, the pressure sensor shall have provisions for recording data through either a remotely located black box, or electronics incorporated into the head of the transducer, for performing diagnostics and prognostics capabilities. The DPMS will be completely autonomous with no electrical connectors to the vehicle. The DPMS will provide both visual presentation of hydraulic system health (e.g. lights) and recording of the pressure/temperature history. Recorded data shall be retrieved by maintenance personnel using either wireless or wired data link as desired. It is important to note that this pressure sensing device is to be used as a maintenance tool only, and that, it is not intended for pilot usage.

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

3 SBIR/STTR records share this UEI (2007–2013). Reported award amounts total $248,605. Reported amounts are not federal obligations.

Phases: Phase I

Agencies: Department of Defense, Department of Energy

Agency intelligence

Department of Defense

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