|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/055; 244/001N; 244/087|
|우선권정보||FR-06 02405 (2006-03-20)|
|§371/§102 date||20080730 (20080730)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 6|
An aircraft having reduced environmental impact includes at least one engine with at least one propeller carried, at the rear, on the top of the aircraft with the propeller(s) located in vertical alignment with the rear part of a noise barrier cell and the rear face of a burst zone situated forward of the central part of an empennage box.
1. Aircraft of reduced environmental impact, having a longitudinal axis and comprising: at least one engine which comprises at least one propeller positioned behind said engine and able to exert thrust on said aircraft and which is mounted at the rear of said aircraft, on the back thereof, the axis of said engine being at least substantially parallel to said longitudinal axis of the aircraft, said engine and said propeller being such that, should they shatter, their debris would follow paths contained in a shatter region aligned with said axis of the eng...