发明名称 Turbojet engine
摘要 The present invention deals with a turboreactor comprising at least a precombustion chamber, a combustion chamber, means for directing combustion gases from the precombustion chamber into the combustion chamber, an air compressor, and means for dividing the air flow from the air compressor while guiding it in the combustion chamber. The turboreactor comprises advantageously a contrarotating stator. The invention relates also to a process in which the blades are heated and pushed in a thermoplastic layer of the body of the rotor and/or stator.
申请公布号 US6553765(B2) 申请公布日期 2003.04.29
申请号 US20010871207 申请日期 2001.05.31
申请人 BREGENTZER DANIEL 发明人 BREGENTZER DANIEL
分类号 F01D1/24;F02C3/14;F23R3/34;F23R3/40;F23R3/54;(IPC1-7):F02C3/14 主分类号 F01D1/24
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