发明名称 Aircraft airconditioning energy recovery device
摘要 The aircraft air conditioning energy recovery device exploits the high level energy in relation to the exterior, in the air conditioning air flow required for renewal, and involves the placement of the aircraft outflow valve in a duct through which all the air flows said duct being arranged from the pressurized cabin to the inside of the engine inlet diffuser, through the pylon and in some cases through the wing, with said air-conditioning flow being fed back to the input air flow through multiple openings on the inside wall of the inlet diffuser. Said openings or grooves run at a slight angle to the direction of flow to avoid turbulence.The air conditioning input may be introduced through hollow radial guide vanes attached at the front end to the vanes of the first stage of the low-pressure compressor and to the hollow vanes, open at the back, in the first stage or stages of the low-pressure compressor stator where the pressure is lower than that of the cabin air. <IMAGE>
申请公布号 EP0974515(A2) 申请公布日期 2000.01.26
申请号 EP19990500060 申请日期 1999.04.15
申请人 MUNOZ SAIZ, MANUEL 发明人 MUNOZ SAIZ, MANUEL
分类号 B64C23/00;B64D13/00;B64D33/02;F02C7/32;(IPC1-7):B64C21/04 主分类号 B64C23/00
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