|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/053.B; 244/117.R; 244/102.R|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 13 인용 특허 : 66|
Engine nacelles for use with aircraft. In one embodiment, an engine nacelle includes an inlet having an inlet aperture and an outlet having an outlet aperture. In one aspect of this embodiment, the engine nacelle further includes a first side portion, a second side portion, and a third side portion. The first side portion can extend at least generally between a first edge portion of the inlet aperture and a third edge portion of the outlet aperture. The second side portion can be offset from the first side portion and extend at least generally between a ...
1. An engine nacelle for use with an aircraft, the engine nacelle comprising:an air inlet configured to direct incoming air from an inlet aperture to an aircraft engine; a gear bay at least approximately laterally offset from the air inlet, wherein the gear bay is configured to house a landing gear assembly having a wheel truck, wherein the wheel truck is moveable between a stowed position within the gear bay and a deployed position offset from the gear bay, and wherein the wheel truck is configured to support at least a portion of the weight of the airc...