发明名称 INTERMEDIATE HOUSING HUB FOR AN AIRCRAFT TURBOFAN, INCLUDING AIR GUIDE DEFLECTORS
摘要 <p>The invention relates to an intermediate housing hub for an aircraft turbofan, including an inner ferrule for defining a first flow space for a main gas flow in a turbofan and moreover at least one intermediate space. The inner ferrule is provided with at least one main opening and at least one movable door forming a main air passage duct. Said door is capable of taking, from the main opening, air flowing into the main gas space and, of sending the air thus taken, back to the intermediate space toward a secondary air passage duct. The secondary duct is moreover extended, from the inlet thereof, by means of a deflector extending upstream into the intermediate space. Said hub is characterized in that the deflector forms an air-guiding duct having an inner surface extending from said inlet to a guide opening arranged downstream from the outlet of the door.</p>
申请公布号 WO2015011392(A1) 申请公布日期 2015.01.29
申请号 WO2014FR51879 申请日期 2014.07.21
申请人 SNECMA 发明人 LUKOWSKI, BENJAMIN;FESSOU, PHILIPPE;LAPORTE, ARNAUD
分类号 F01D17/10;F02C6/08;F02C7/052;F02K3/075 主分类号 F01D17/10
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