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특허 상세정보

Hierarchical closed-loop flow control system for aircraft, missiles and munitions

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01    B64C-005/12    F42B-010/14    F42B-010/62    F42B-015/00    F42B-010/00   
출원번호 US-0057211 (2016-03-01)
등록번호 US-10139209 (2018-11-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kolkowski, Brian
인용정보 피인용 횟수 : 0  인용 특허 : 31
초록

The present invention relates to a missile or aircraft with a hierarchical, modular, closed-loop flow control system and more particularly to aircraft or missile with a flow control system for enhanced aerodynamic control, maneuverability and stabilization and methods of operating the flow control system. Various embodiments of the flow control system of the present invention involve flow sensors, active flow control device or activatable flow effectors and/or logic devices with closed loop control architecture. The sensors are used to estimate or determ...

대표
청구항

1. A munition comprising: an aerodynamic surface or surfaces, and a forebody and an afterbody;at least two air flow control zones each comprising a discrete area or region and at least one adjustable control surface on the aerodynamic surface or surfaces of the munition, at least one air flow control zone being on the forebody and at least one air flow control zone being on the afterbody, the at least one adjustable control surface being activatable flow effectors adapted to be activated, and controlled once activated; andone or more digital logic device...

이 특허에 인용된 특허 (31)

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