发明公开
- 专利标题： AIRCRAFT PNEUMATIC SYSTEM
- 专利标题（中）： 气体流体力学
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申请号： EP16178641.3申请日： 2016-07-08
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公开(公告)号： EP3127812A1公开(公告)日： 2017-02-08
- 发明人: Stieger, Rory , Popovic, Ivan
- 申请人： Rolls-Royce plc
- 申请人地址： 62 Buckingham Gate London SW1E 6AT GB
- 专利权人： Rolls-Royce plc
- 当前专利权人： Rolls-Royce plc
- 当前专利权人地址： 62 Buckingham Gate London SW1E 6AT GB
- 代理机构： Rolls-Royce plc
- 优先权： GB201513952 20150807
- 主分类号： B64D13/06
- IPC分类号： B64D13/06 ; F02C6/08
摘要：
An aircraft pneumatic system comprises a main gas turbine engine (10) comprising a main compressor (14, 16), a recuperated auxiliary gas turbine engine (40) comprising a core compressor (42) having an inlet in fluid communication with a main compressor bleed (32) of the main gas turbine engine(10) and an environmental control system inlet in fluid communication with the main compressor bleed (32) of the main gas turbine engine (10). The environmental control system comprises a compressor (68) driveable by power provided by the auxiliary gas turbine engine (40).
公开/授权文献
- EP3127812B1 AIRCRAFT PNEUMATIC SYSTEM 公开/授权日：2019-06-19
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