发明名称 |
Variable cycle propulsion device for supersonic airplanes using diverted exhaust gas |
摘要 |
The variable cycle propulsion mechanism has a propulsor (1) carrying gas products escaping through a tube creating a thrust, and an auxiliary propulsion unit (14) separate from the propulsor. The auxiliary propulsion unit operate for subsonic flights, landings and take offs and has a gas mechanism passing gas from the main propulsion unit when operating, or switched off for supersonic flights. |
申请公布号 |
EP1267064(A1) |
申请公布日期 |
2002.12.18 |
申请号 |
EP20020291409 |
申请日期 |
2002.06.07 |
申请人 |
SNECMA MOTEURS |
发明人 |
FRANCHET, MICHEL;LAUGIER, YANN;LOISY, JEAN |
分类号 |
B64C30/00;F02C3/10;F02C7/36;F02K1/12;F02K3/02;F02K3/075;F02K3/12 |
主分类号 |
B64C30/00 |
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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