发明名称 |
Changeover valve for a combi jet engine having two operational configurations. |
摘要 |
This jet engine is composed of a central turbojet stream (2) and of a peripheral ramjet stream (3) which deployable flaps located on the inlet cone (5) and on the inlet (8) of the peripheral stream (3) can obstruct or free in turn depending on the desired operating mode. Very good guidance of the gases may be obtained. <IMAGE>
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申请公布号 |
EP0576355(A1) |
申请公布日期 |
1993.12.29 |
申请号 |
EP19930401611 |
申请日期 |
1993.06.23 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." |
发明人 |
BROSSIER, PASCAL NOEL;MAZEAUD, GEORGES;WURNIESKY, PASCAL CLAUDE |
分类号 |
F02C7/042;F02K7/16;(IPC1-7):F02C7/042 |
主分类号 |
F02C7/042 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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