| 发明名称 |
Gas turbine engine for subsonic flight |
| 摘要 |
A gas turbine engine for use on an aircraft which flies entirely within a subsonic velocity range is provided with a fixed area convergent-divergent nozzle to provide better overall engine performance.
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| 申请公布号 |
US3896615(A) |
申请公布日期 |
1975.07.29 |
| 申请号 |
US19740512286 |
申请日期 |
1974.10.04 |
| 申请人 |
UNITED AIRCRAFT CORPORATION |
发明人 |
SLATKIN, MARTIN S.;MOTYCKA, DAVID L.;DISABATO, VINCENT J. |
| 分类号 |
F02K1/00;(IPC1-7):F02K3/06;F02K1/24 |
主分类号 |
F02K1/00 |
| 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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