Invention Grant
US08366039B2 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft
有权
涡轮发动机从飞机的机翼悬挂通过该塔架进行整流
- Patent Title: Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft
- Patent Title (中): 涡轮发动机从飞机的机翼悬挂通过该塔架进行整流
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Application No.: US12305903Application Date: 2007-06-18
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Publication No.: US08366039B2Publication Date: 2013-02-05
- Inventor: Alain Porte
- Applicant: Alain Porte
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Dickinson Wright PLLC
- Priority: FR0605448 20060620
- International Application: PCT/FR2007/001009 WO 20070618
- International Announcement: WO2007/147965 WO 20071227
- Main IPC: B64D27/00
- IPC: B64D27/00
Abstract:
Disclosed is a pylon fairing for a turbine engine. The anterior portion of the pylon fair is attached to a turbine engine in a manner to absorb blows against the fan casing of the turbine engine in case of breakage of the fan blades of the turbine engine. The pylon fairing is configured with the turbine engine such that the anterior part of the pylon fairing is fastened to the engine's fan casing via a front fixing and a rear fixing. The rear fixing is affixed to the fan casing as relatively loose in order to absorb tolerances, and the front fixing is affixed to the fan casing and as flexible in at least approximately a radial direction with respect to the fan casing.
Public/Granted literature
- US20100176250A1 FAIRING FOR A PYLON VIA WHICH A TURBINE ENGINE IS SUSPENDED FROM A WING OF AN AIRCRAFT Public/Granted day:2010-07-15
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