| 发明名称 |
Gas turbine engine with dual compression rotor |
| 摘要 |
The present invention provides a gas turbine engine including a first combustion chamber, a dual compression rotor positioned behind the combustion chamber, and a centrifugal compression rotor positioned behind the dual compression rotor.
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| 申请公布号 |
US8356469(B1) |
申请公布日期 |
2013.01.22 |
| 申请号 |
US20080156809 |
申请日期 |
2008.04.07 |
| 申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE;DALE MARK R. |
发明人 |
DALE MARK R. |
| 分类号 |
F02K3/00;F02C3/00;F02C3/04;F02C5/00 |
主分类号 |
F02K3/00 |
| 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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