发明名称 |
Aircraft gas turbine with thrust reverser with cascade elements and integrated rack and pinion type drive |
摘要 |
The present invention relates to an aircraft gas turbine comprising a thrust-reverser device that is arranged at the rear area of an engine cowling and that has multiple cascade elements which are distributed at the circumference and which divert a stream, characterized in that the cascade elements are mounted in a displaceable manner, in that on both sides of each cascade element at least one gear rack is formed that can be displaced via a respective cog wheel which is coupled to a driving device, and in that each cascade element is connected to a rear area of the engine cowling via a coupling element for the purpose of displacing the engine cowling in the axial direction. |
申请公布号 |
EP2886842(B1) |
申请公布日期 |
2016.05.18 |
申请号 |
EP20140194730 |
申请日期 |
2014.11.25 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG;LIEBHERR-AEROSPACE LINDENBERG GMBH |
发明人 |
TODOROVIC, PREDRAG;BÄR, JOSEF;MÜLLER, FRANK;SCHUMANN, UWE |
分类号 |
F02K1/56;F02K1/72;F02K1/76 |
主分类号 |
F02K1/56 |
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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