|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-033/02 B64D-033/00 B64D-027/00|
|§371/§102 date||20070413 (20070413)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 3|
A vertical tail unit for an aircraft and an aircraft equipped with the vertical tail unit. The vertical tail unit is provided with an engine. The engine extends cantilevered beyond a fin of the vertical tail unit and is secured to the fin by a mount. The mount is at least partly attached to the fin. The mount comprises for example half-hoops arranged on either side of the fin.
The invention claimed is: 1. A vertical tail unit for aircraft, the vertical tail unit comprising a fin presenting a first face and a second opposing face, and a flight control surface, said vertical tail unit being equipped with an engine extending in a plane containing the vertical tail unit, the engine being supported by the vertical tail unit, wherein the engine extends cantilevered beyond at least one of the first face and the second face of the fin and is integral with said fin by a mount operably coupled to the fin such that the fin passes throug...