|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/214 ; 244/113|
|발명자 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 0|
An aircraft spoiler system consisting of semi-circular rods disposed within the leading edge of an aircraft wing and rotatably carried thereby so that in the inactive position the substantially flat surfaces are flush with the wing surface and in its most active position the flat surfaces are at right angles to the wing surface with approximately half of the rods extending above the wing surface, acting in a manner to eliminate the lift of the wing, i.e., as spoilers. The rods are controlled by a pair of magnetic clutches which connect the spoiler rods t...
An aircraft spoiler system comprising: a retro-fit mounting having a geometry of a predetermined aircraft wing leading edge, said retro-fit mounting being fixedly attached to the leading edge of an aircraft wing providing an extension thereof; at least one spoiLer rod having one substantially flat surface portion, said at least one spoiler rod disposed within said retro-fit mounting and rotatably carried thereby, said spoiler rod having a geometry for being flush with the surface of said retro-fit mounting in one extreme rotative position; and a control ...