|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 60/2263 ; 137/151|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 23 인용 특허 : 0|
A nacelle for a gas turbine engine (10) defines an air intake which is capable of meeting all the engine airflow requirements. The nacelle comprises a cowling (22), fixed upstream and in spaced apart relationship from an engine cowling (16), to define an annular passage (30) therebetween. Each of the cowlings, (22) and (16), have an air intake, (24) and (20) respectively, through which the mainstream flow of air passes into the engine (10). Depending upon the amount of airflow the engine (10) demands at different operating flight conditions air can flow ...
A nacelle comprising a first cowling for a gas turbine engine, said first cowling having an air intake forward of said gas turbine engine for directing a flow of air to the gas turbine engine, and a second cowling upstream of said first cowling also having an air intake forward of the gas turbine engine, the first and second cowlings being arranged so that the air intakes in each of the cowlings are in series flow relationship with one another to allow the passage of flow of air to said gas turbine engine, the second cowling being in a spaced apart relat...