|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||415/145; 415/220; 415/914|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 20|
A gas turbine engine is provided with a nacelle having a hollow inner space. The inner space is utilized as a plenum for directing air from an inlet to an outlet at the upstream end of the nacelle to allow control of an effective lip width of the nacelle under certain flight conditions.
1. A gas turbine engine comprising: a nacelle defining an interior space;a fan section, a compressor section and a turbine section positioned within said nacelle, an inner cowl surrounding said compressor section and said turbine section, and said fan section delivering air to said compressor section, and bypass air between said cowl and an interior surface of said nacelle;an air inlet for capturing air and communicating the air into the interior space of said nacelle, said interior space defining a plenum, the air leaving said air inlet, flowing through...