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특허 상세정보

Synthetic jet actuators

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B05B-003/04   
미국특허분류(USC) 239/102.2; 239/509; 239/102.1; 239/510; 239/521; 239/524
출원번호 US-0003540 (2001-10-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Atwood, Pierce
인용정보 피인용 횟수 : 67  인용 특허 : 9
초록

A first embodiment of the present invention provides a vortex generator in the form of a flexible piezoelectric actuator blade disposed in a wall of a flowpath, such as an airfoil. Another embodiment provides a synthetic jet actuator in which a pair of bimorph piezoelectric plates are connected by a flexible hinge.

대표
청구항

A first embodiment of the present invention provides a vortex generator in the form of a flexible piezoelectric actuator blade disposed in a wall of a flowpath, such as an airfoil. Another embodiment provides a synthetic jet actuator in which a pair of bimorph piezoelectric plates are connected by a flexible hinge. an indication of said fuel level in said fuel cell.15. The system of claim 14 wherein the tool includes a fuel metering valve and said control unit is connected to said fuel metering valve, and further including a temperature sensor configure...

이 특허를 인용한 특허 피인용횟수: 67

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