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"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

System for aerodynamic flows and associated method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-021/04    B64C-021/00   
미국특허분류(USC) 244/207; 244/208
출원번호 UP-0200515 (2005-08-09)
등록번호 US-7635107 (2010-01-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Alston & Bird LLP
인용정보 피인용 횟수 : 3  인용 특허 : 37
초록

A system and method for controlling boundary layer flow over an aircraft wing are provided. The system includes at least one wing element, and a plurality of ports defined in the wing element and in fluid communication with one another. The system also includes at least one fluidic device operable to continuously ingest the fluid through at least one of the ports and eject the fluid out of at least one other port to control boundary layer flow of the fluid over the wing element.

대표
청구항

That which is claimed: 1. A system for controlling boundary layer flow over an aircraft wing comprising: a plurality of wing elements, wherein the plurality of wing elements comprise a slat and a flap interconnected to a main wing element; a plurality of ports defined in the slat, flap, and main wing element, at least a pair of ports in the slat, flap, and main wing element in fluid communication with one another; and at least one fluidic device operable to continuously ingest the fluid through at least one of the ports and eject the fluid out of at lea...

이 특허에 인용된 특허 (37)

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