Invention Grant
- Patent Title: Pylon for supporting an aircraft turbomachine
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Application No.: US16534864Application Date: 2019-08-07
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Publication No.: US11435263B2Publication Date: 2022-09-06
- Inventor: Jacky Raphael Michel Derenes , Michael Daniel Joel Bertin , Etienne Romain Pascal Grenier
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1857409 20180809
- Main IPC: F16M11/00
- IPC: F16M11/00 ; G01M15/14 ; G01M15/02

Abstract:
A pylon for supporting an aircraft turbomachine, in particular for a test bench, the pylon having a generally elongated shape along an axis and including, at a first longitudinal end, first members for fixing to a turbomachine and, at a second longitudinal end, second members for fixing to a base plate, the pylon being traversed by at least one fluid pipe including a first end for connecting to the turbomachine and a second end for connecting to a fluid supply circuit, wherein the at least one pipe includes a movable portion movable in translation along the axis so as to be able to adjust the position along the axis of the first connecting end relative to the first longitudinal end. It also concerns a method of mounting an aircraft turbomachine on such a pylon.
Public/Granted literature
- US20200049591A1 PYLON FOR SUPPORTING AN AIRCRAFT TURBOMACHINE Public/Granted day:2020-02-13
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