Invention Grant
- Patent Title: Uncoupling system for an aircraft turbojet engine rotary shaft
- Patent Title (中): 用于飞机涡轮喷气发动机旋转轴的解耦系统
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Application No.: US13575218Application Date: 2011-01-12
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Publication No.: US08646978B2Publication Date: 2014-02-11
- Inventor: Edouard Joseph Jadczak , Cedric Magret , Pierrick Ollivier , Arnaud Fabrice Quenardel
- Applicant: Edouard Joseph Jadczak , Cedric Magret , Pierrick Ollivier , Arnaud Fabrice Quenardel
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1050573 20100128
- International Application: PCT/FR2011/050056 WO 20110112
- International Announcement: WO2011/092411 WO 20110804
- Main IPC: F16C27/00
- IPC: F16C27/00 ; F16C43/00

Abstract:
A decoupling system for a rotary shaft of an aircraft turbojet, the decoupling system including: a rolling bearing including rolling elements inserted between a first ring fastened to a stationary bearing support and a second ring mounted in a mounting chamber fastened to a rotary shaft; a transmission mechanism transmitting rotary torque from the rotary shaft to the second ring; a mechanism allowing the second ring to move radially relative to the mounting chamber when a static force associated with an unbalance affecting the rotary shaft exceeds a predetermined threshold; and a plurality of leaktight flexible bags interposed between the second ring and the mounting chamber and each including a heterogeneous structure including a porous capillary solid matrix and an associated liquid relative to which the matrix is lyophobic.
Public/Granted literature
- US20130022448A1 UNCOUPLING SYSTEM FOR AN AIRCRAFT TURBOJET ENGINE ROTARY SHAFT Public/Granted day:2013-01-24
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