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|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-009/00 B64C-003/00 B64C-005/00 F42B-010/00 F42B-015/01|
|미국특허분류(USC)||244/201 ; 244/198 ; 244/003.26|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 3|
A configurable aerial vehicle aerosurface is disclosed, The configurable aerial vehicle aerosurface includes first and second airfoil surfaces in sliding engagement. A plurality of apertures pass transversely through the airfoil surfaces and are disposed in such a relationship so as to define a first position wherein the apertures are in substantial alignment and a second position wherein the apertures are in substantial non-alignment. In this way, the configurable aerial vehicle aerosurface of the present invention can be configured from a first, low dr...
[ I claim:] [1.]1. An aerial vehicle aerosurface, comprising:a first airfoil surface having at least one aperture passing transversely therethrough; and,a second airfoil surface slidably received within said first airfoil surface, said second airfoil surface having at least one aperture of like kind passing transversely therethrough, said second airfoil surface being positionable with respect to said first airfoil surface to define a first position wherein said apertures in said airfoil surfaces are in substantial alignment and a second position wherein ...