发明名称 Ring structure and compressor blow-off arrangement comprising said ring
摘要 A ring of an annular valve assembly is movable in the direction of its longitudinal axis and is intended for an axial compressor blow-off arrangement. The ring takes the form of an axially orientated channel-section member having a first annular skin of concave section nested in a second annular skin also of concave section. A cavity filled with a synthetic resin filler is defined by the two skins. The blow-off arrangement for an axial-flow compressor of a turbo-jet engine, which incorporates this ring, comprises an annular opening with which the ring cooperates to re-form the wall of the air flow when the blow-off arrangement is inoperative.
申请公布号 US4674951(A) 申请公布日期 1987.06.23
申请号 US19850770247 申请日期 1985.08.28
申请人 SNECMA 发明人 JOURDAIN, GERARD E. A.;SOLIGNY, MARCEL R.
分类号 F04D27/02;(IPC1-7):F04D27/02 主分类号 F04D27/02
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