|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 12|
An air intake system of a propeller-turbine engine with a propeller gearbox 1 in in-line arrangement, includes one or more intake units 3 arranged essentially below a nacelle fairing 2 of the propeller-turbine engine with each intake unit 3 being related to a elbow diffuser 19 , a shock diffuser 4 , and a rotationally symmetric attenuation chamber 5 into which the respective shock diffuser 4 issues and which is connected to the compressor inlet 6 of the propeller-turbine engine.
1. An air intake system of a propeller-turbine engine having a propeller gearbox in in-line arrangement, comprising:at least one intake unit arranged essentially below a nacelle fairing of the propeller-turbine engine,a diffuser flowingly connected to each intake unit, anda rotationally symmetric attenuation chamber that is rotationally symmetric with the engine and into which each respective diffuser issues and which is flowingly connected to a compressor inlet of the propeller-turbine engine. 2. An air intake system in accordance with claim 1, wherein ...