Invention Grant
US08522529B2 Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow
有权
具有热交换器的飞机推进装置具有用于冷却空气流和热空气流的前入口面
- Patent Title: Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow
- Patent Title (中): 具有热交换器的飞机推进装置具有用于冷却空气流和热空气流的前入口面
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Application No.: US11996019Application Date: 2006-07-07
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Publication No.: US08522529B2Publication Date: 2013-09-03
- Inventor: Jean-Marc Martinou , Herve Marche
- Applicant: Jean-Marc Martinou , Herve Marche
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Perman & Green, LLP
- Priority: FR0552352 20050728
- International Application: PCT/FR2006/001695 WO 20060707
- International Announcement: WO2007/012722 WO 20070201
- Main IPC: F02K99/00
- IPC: F02K99/00 ; F02C6/08 ; F02C6/04 ; B64D33/10
Abstract:
An aircraft propulsion unit including a turbojet and a heat exchanger located above the turbojet and drawing a cooling air stream and a hot air stream in the turbojet. Wherein the cooling air intake and hot air intake surfaces in the housing are directed forward of the turbojet and have normal lines inclined relative to the axis of the turbojet. The embodiment also concerns an aircraft equipped with at least one such propulsion unit.
Public/Granted literature
- US20090025366A1 PROPULSION UNIT FOR AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION UNIT Public/Granted day:2009-01-29
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