|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/54 ; 60/226R ; 248/554|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 58 인용 특허 : 2|
A gas turbine powerplant has an inner casing (4A) containing a gas turbine engine, an outer casing (5) surrounding the inner casing, a fan driven by the engine and driving air through an annular duct defined between the casings. The powerplant is connected to an aircraft fuselage (1) by a front mounting (9,9A,9B,9C) and by a rear mounting (8,10,17,18). The front and rear mountings react lateral forces on the powerplant. The powerplant includes a thrust reverser (11) situated rearwards of the rear mounting and supported by a ring (18) lying in the annulus...
A mounting for a gas turbine powerplant which comprises an inner annular casing containing a gas turbine engine, an outer annular casing surrounding the inner casing, a compressor connected to be driven by the engine and adapted to drive air through an annular duct defined between the casings, and a thrust reverser means at the outer casing for reversing the flow therethrough; the mounting comprising front and rear structural means arranged respectively at a front and rear location of the powerplant for supporting the powerplant laterally on a support si...