Invention Grant
US08850824B2 Aircraft gas turbine with variable bypass nozzle by deforming element
有权
具有可变旁路喷嘴的飞机燃气轮机通过变形元件
- Patent Title: Aircraft gas turbine with variable bypass nozzle by deforming element
- Patent Title (中): 具有可变旁路喷嘴的飞机燃气轮机通过变形元件
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Application No.: US13541260Application Date: 2012-07-03
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Publication No.: US08850824B2Publication Date: 2014-10-07
- Inventor: Predrag Todorovic , Miles Trumper
- Applicant: Predrag Todorovic , Miles Trumper
- Applicant Address: DE
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy J. Klima
- Priority: DE102011106959 20110708
- Main IPC: F02K1/08
- IPC: F02K1/08 ; F02K3/02 ; F02K1/82
Abstract:
The present invention relates to an aircraft gas turbine with a core engine which is surrounded by a bypass duct enclosed radially outwards by a bypass wall, with a radially inner wall of the bypass duct forming with the radially outer bypass wall a bypass nozzle, and with the radially inner wall including an adjusting element extending along the circumference of the inner wall and being deformable radially outwards.
Public/Granted literature
- US20130008147A1 Aircraft gas turbine with variable bypass nozzle Public/Granted day:2013-01-10
Information query
