SBIR/STTR Research Award

Fiber Optic Fabry Perot Vector Sensor Arrays

Award identifier e09208c3662bdeb7cb3cc8de709074a0258073e35b2dfd8967fa1f79c49df990Awarding agency Department of Defense · Navy

Award amount

$99,795

Program and phase

SBIR · Phase I

Award year

2008

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
Vibration, Impact and Pressure Sensors, Inc.
Proposal award date
2008-03-17
Contract end date
2009-02-10
UEI
X1S3PK2UPCU3
Solicitation number
2007.3
Topic code
N07-215

Research abstract

Conventional accelerometers are non-optimal for many submarine sensor applications, especially for hydrophone towed arrays. Limitations include size and weight, need for heavy copper conductors, susceptibility to electromagnetic interference and electrical cross talk, and limited cable drive capability. VIP Sensors proposes to develop a sensor measuring system consisting of optical MEMS vector sensors distributed on a single optic fiber, each working at different frequency ranges. A broadband high intensity LED is used as a light source for the serially connected accelerometers. Each optical sensor, tuned to work at a unique frequency of the spectrum, shifts (modulates) its corresponding input signal frequency proportional to the measured pressure and lets pass all other frequency signals. The light at the end of the optic fiber contains the information for all sensors at different preset frequency slots, in a scheme similar to Wave Division Multiplexing. An optical demultiplexer located at the fiber end separates the signal spectrum. A photodiode array converts the photons to electrons and specialized circuitry quantifies the frequency shift corresponding to each sensor. The sensor is sculptured on silicon wafer using MEMS processes. It consists of a mass hanging on a flexure hinge. A strand of optical fiber is attached on the surface of the sensor chip with an intrinsic Fabry Perot cavity laid between the mass and the rigid frame. The inertia force rotates the hanging mass about the flexure hinge. The mass displacement stretches or compresses the fiber. The strain in the fiber changes the length of the Perot cavity, which causes the shift of the incoming light wavelength. The shift of wavelength is thus proportional the inertia force or acceleration.

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

14 SBIR/STTR records share this UEI (2004–2017). Reported award amounts total $6,843,712. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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