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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|