Invention Grant
US08256708B2 Device for attaching an aircraft engine comprising a thrust force take-up device with a compact design
有权
用于附接具有紧凑设计的推力牵引装置的飞机发动机的装置
- Patent Title: Device for attaching an aircraft engine comprising a thrust force take-up device with a compact design
- Patent Title (中): 用于附接具有紧凑设计的推力牵引装置的飞机发动机的装置
-
Application No.: US12674555Application Date: 2008-08-22
-
Publication No.: US08256708B2Publication Date: 2012-09-04
- Inventor: Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
- Applicant: Emmanuel Guillet , Jean-Marc Martinou , Pascal Gardes
- Applicant Address: FR Toulouse
- Assignee: Airbus Operations SAS
- Current Assignee: Airbus Operations SAS
- Current Assignee Address: FR Toulouse
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0757166 20070824
- International Application: PCT/EP2008/061010 WO 20080822
- International Announcement: WO2009/027333 WO 20090305
- Main IPC: B64D27/00
- IPC: B64D27/00

Abstract:
An aircraft engine attachment device including a rigid structure and a mechanism attaching the engine on the rigid structure, the attachment mechanism including a rear engine attachment and a device for taking-up thrust forces generated by the engine. The rear engine attachment is attached to the rigid structure by two lateral fittings attached to the rigid structure. The force take-up device includes two connecting rods mechanically connected to a spreader beam by a mechanical connection, a connection fitting attached to the rear engine attachment and mechanically connected to the rigid structure by a thrust pin, the lateral fittings including a stop mechanism to limit pivoting of the spreader beam if a connecting rod breaks and ensuring transmission of thrust forces to the rigid structure.
Public/Granted literature
- US20110114786A1 DEVICE FOR ATTACHING AN AIRCRAFT ENGINE COMPRISING A THRUST FORCE TAKE-UP DEVICE WITH A COMPACT DESIGN Public/Granted day:2011-05-19
Information query