Invention Grant
- Patent Title: Aircraft propelling assembly including a duct forming a thermal barrier integrated in the caisson of the rigid structure of the engine mounting system
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Application No.: US14707240Application Date: 2015-05-08
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Publication No.: US09975641B2Publication Date: 2018-05-22
- Inventor: Wolfgang Brochard , Misael Hernandez-Perez , Yves Belloc
- Applicant: Airbus Operations (SAS)
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS SAS
- Current Assignee: AIRBUS OPERATIONS SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1454183 20140509
- Main IPC: B64D27/26
- IPC: B64D27/26 ; F28F3/02
Abstract:
Housing a conduit of a thermal protection system of a rigid structure of an attachment pylon in an aircraft propulsion assembly within a box of the rigid structure, so as to take advantage of the volume within the rigid structure. The elements forming the conduits thus form an integral part of the rigid structure and can thus play a structural role.
Public/Granted literature
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