发明名称 |
COMPACT ACTUATION SYSTEM FOR A GAS TURBINE ENGINE EXHAUST NOZZLE |
摘要 |
An exemplary nozzle having a variable internal exhaust area for a gas turbine engine can have a plurality of flap trains extending around a periphery of the gas turbine engine. Each flap train can include a convergent flap pivotally attached to an engine body and a divergent flap pivotally attached to the engine body downstream of the convergent flap. The nozzle can further have a fluid circuit in communication with the convergent and divergent flaps and configured to pivot the convergent and divergent flaps between a radially inward position and a radially outward position. |
申请公布号 |
EP2971724(A1) |
申请公布日期 |
2016.01.20 |
申请号 |
EP20140719966 |
申请日期 |
2014.03.13 |
申请人 |
ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. |
发明人 |
PESYNA, KENNETH, M. |
分类号 |
F02K1/12;F02K1/15 |
主分类号 |
F02K1/12 |
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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