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공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
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| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
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예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Aerospace vehicle yaw generating systems and associated methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-001/12   
미국특허분류(USC) 244/184; 244/195; 244/099.1; 244/099.11
출원번호 US-0158198 (2005-06-21)
등록번호 US-7367530 (2008-05-06)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 7  인용 특허 : 157

Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system can further include a movable control surface coupled to the fuselage and extending generally in a horizontal plane. The control surface can be movable to a deflected position in which the control surface can be positioned to create a flow pattern proximate to the fuselage when the aerospace ...


We claim: 1. A yaw generating system, comprising: an aerospace vehicle having a fuselage with a first portion and a second portion; a wing section coupled to the fuselage; and a movable control surface attached directly to the wing section and extending generally in a horizontal plane, the control surface being movable to a deflected position in which the control surface is positioned to create a flow pattern proximate to the fuselage when the aerospace vehicle is located in a flow field, the flow pattern being positioned to create a pressure differenti...

이 특허에 인용된 특허 (157)

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