|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/055; 244/054; 244/060; 244/069|
|우선권정보||DE-10 2008 062 813 (2008-12-23)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 14|
An aircraft propeller-engine layout includes at least one engine (10) arranged in a tail (2) of a fuselage (1) of an aircraft and has at least one propeller arrangement, with a shaft of the propeller (6, 7) being connected to a shaft (21) of the engine (10) via at least one transfer shaft (12).
1. An aircraft propeller-engine layout, comprising: an aircraft having a fuselage, the fuselage having a tail;first and second engines, each having a driving shaft, each engine being positionable in a tail of a fuselage of an aircraft;first and second propeller shafts;one propeller arrangement attached to each propeller shaft;first and second transfer shafts connecting the first and second propeller shafts respectively to the driving shafts of the first and second engines;wherein each propeller arrangement is disposed in a nacelle, connected to the fusel...