Invention Grant
- Patent Title: Turbomachine support pylon for aircraft
- Patent Title (中): 涡轮机支架用于飞机
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Application No.: US13094363Application Date: 2011-04-26
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Publication No.: US08714477B2Publication Date: 2014-05-06
- Inventor: Christelle Rinjonneau , Pierre Guillaume
- Applicant: Christelle Rinjonneau , Pierre Guillaume
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations S.A.S.
- Current Assignee: Airbus Operations S.A.S.
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1053200 20100427
- Main IPC: B64D27/00
- IPC: B64D27/00 ; B64D33/10

Abstract:
An aircraft support pylon designed to attach a turbomachine housed in a nacelle to an aircraft fuselage is disclosed. The pylon includes a cooler, located substantially in the vicinity of a leading edge of the pylon, and able to be heated by a hot fluid, the hot fluid intended to be cooled by heat exchange with cold air outside the cooler. The pylon also includes at least one air evacuation duct, at the exit from the cooler and extending longitudinally in an internal volume of the pylon to a trailing edge of the pylon.
Public/Granted literature
- US20110315813A1 TURBOMACHINE SUPPORT PYLON FOR AIRCRAFT Public/Granted day:2011-12-29
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