Invention Grant
- Patent Title: Method of testing the integrity of a fluid flow regulator system for a turbine engine
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Application No.: US16310648Application Date: 2017-06-08
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Publication No.: US10760439B2Publication Date: 2020-09-01
- Inventor: Clementine Morisot , Benoit Michel Pontallier
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@33571966
- International Application: PCT/FR2017/051449 WO 20170608
- International Announcement: WO2017/220881 WO 20171228
- Main IPC: F01D17/12
- IPC: F01D17/12 ; F01D9/06 ; F01D17/10

Abstract:
A method of testing the integrity of a fluid flow regulator system for a turbine engine, the system including a fluid-passing duct associated with a movable flap; an actuator having a movable drive element suitable for delivering a movement force between a first position corresponding to the closed position of the movable flap and a second position corresponding to the open position of the movable flap; a push-pull cable interconnecting the drive element and the movable flap; and return device exerting a return force for moving the flap; the method of testing the integrity of the system including in succession: a step of supplying power to the actuator in order to place the drive element in the second position; a step of interrupting the supply of power; and a step of measuring the position of the drive element.
Public/Granted literature
- US20190323369A1 METHOD OF TESTING THE INTEGRITY OF A FLUID FLOW REGULATOR SYSTEM FOR A TURBINE ENGINE Public/Granted day:2019-10-24
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