发明名称 MACHINE THERMIQUE A HAUT RENDEMENT
摘要 <p>The machine has main and secondary combustion chambers (19, 20) situated in a cylindrical central volume delimited at base by low pressure and high pressure rotors (3, 4) and at lateral surface by inner, intermediate and outer walls (22, 23, 24). The walls (23, 24) define an annular outer gas circulation conduit (25) connecting an outlet of a low pressure compressor (15) to an inlet of a high pressure compressor (16). The walls (22, 23) define an annular inner gas circulation conduit (26) connecting an outlet of the compressor (16) to an inlet of the chamber (19).</p>
申请公布号 FR2893086(B1) 申请公布日期 2008.01.25
申请号 FR20050011426 申请日期 2005.11.09
申请人 ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES) ETABLISSEMENT PUBLIC 发明人 RIBAUD YVES;GUIDEZ JOEL;BRETEAU JEAN PAUL;COURVOISIER THIERRY;DESSORNES OLIVIER;DUMAND CLEMENT
分类号 F02C6/00;F02C6/06;F02C7/00 主分类号 F02C6/00
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