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Metal Rubber Sensor Appliqués for Rotor Blade Air, Phase I

Completed TRL 4 (started at 5, targeting 4)

Description

The objective of this NASA SBIR program is to develop conformal Metal RubberTM sensor skins for the distributed measurement of wall shear or skin friction on rotorcraft rotor blades. The sensor skin arrays would allow the direct two-dimensional mapping of both orthogonal components of tangential skin friction on rotor blade surfaces without requiring large recessed cavities within the blade structure. Metal RubberTM skin friction sensor element prototypes have been demonstrated on small laboratory flow test articles. Wall shear measurement data are important to 1) establishing boundary conditions for computational fluid dynamics (CFD) analysis of air vehicle boundary layer flow and turbulence, and 2) active flight control of air platforms. During Phase I, NanoSonic would design, fabricate and test new, large-area Metal RubberTM sensor skin materials and arrays capable of surviving the thermal, mechanical, UV and chemical environment of operational aircraft, and work with NASA and industrial partners to transition the use of such sensor skins to use on rotor blade wind tunnel models. The new high performance Metal RubberTM materials, sensor skin arrays, and data acquisition and signal processing electronics would be evaluated using multiple air and water flow systems at NanoSonic and in wind tunnel facilities at a partner institution.

Benefits

Potential NASA Commercial Applications: Non-NASA applications of similar conformal Metal RubberTM 'sensor skin' arrays include 1) measurement of skin friction and pressure on operational hydrocraft, 2) tactile sensor skin arrays that can flex in addition to bend, 3) 2D strain and pressure sensor arrays for biomedical instrumentation, and 3) sensors for high performance military aircraft, especially UAVs and Morphing Aircraft that require active air data sensing and flow control to optimize performance.

Details

Technology areaFlight Vehicle Systems > Flight Mechanics > Flight Mechanics Testing and Flight Operations
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationLangley Research Center, Hampton, VA
Start date2009-01-22
End date2009-07-22

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This is early/mid-stage (TRL 4) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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