Advanced high performance vertical hybrid synthetic jet...

Fluid sprinkling – spraying – and diffusing – With means to vibrate or jiggle discharge

Reexamination Certificate

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C239S102200

Reexamination Certificate

active

08052069

ABSTRACT:
The present invention comprises a high performance, vertical, zero-net mass-flux, synthetic jet actuator for active control of viscous, separated flow on subsonic and supersonic vehicles. The present invention is a vertical piezoelectric hybrid zero-net mass-flux actuator, in which all the walls of the chamber are electrically controlled synergistically to reduce or enlarge the volume of the synthetic jet actuator chamber in three dimensions simultaneously and to reduce or enlarge the diameter of orifice of the synthetic jet actuator simultaneously with the reduction or enlargement of the volume of the chamber. The jet velocity and mass flow rate for the present invention will be several times higher than conventional piezoelectric synthetic jet actuators.

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patent: 6394363 (2002-05-01), Arnott et al.
patent: 6722581 (2004-04-01), Saddoughi
Tian-Bing Xu et al., “Advanced High Performance Synthetic Jet Actuators (HIZMASS) for Active Flow Control in Supersonic Internal and External Viscous Flow”, Technical Proposal, National Institute of Aerospace ROA 2006, Hampton Jul. 7, 2006.
Tian-Bing Xu et al., “High Performance, Zero-Net Mass-Flux Actuators (HIZMASS) for Active Control of Viscous Separated Flow on Rotorcraft Vehicles”, Technical Proposal, National Institute of Aerospace ROA 2006, Hampton Jul. 7, 2006.

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