TURBINE ENGINE WITH AN OIL GUIDING DEVICE AND METHOD FOR DISASSEMBLING THE TURBINE ENGINE

You are here: Homepage > Search

TURBINE ENGINE WITH AN OIL GUIDING DEVICE AND METHOD FOR DISASSEMBLING THE TURBINE ENGINE

Free access

COTTET CLEMENT / CRETIN FABRICE MICHEL FRANÇOIS RENE / JACQUEMARD CHRISTOPHE PAUL / PERDRIGEON CHRISTOPHE MARCEL LUCIEN / TORIBIO LENY

Abstract

A turbine engine is provided with a longitudinal rotation axis having at least one shaft with a radial axis, in particular a pitch change system for the blades of a propeller, said shaft traversing a radial passage of a substantially cylindrical case around the longitudinal axis. The turbine engine includes an annular oil guiding device around the radial shaft. The device has first and second annular parts nested in one another and secured to one another by hooping. The first part is secured by hooping to the radial shaft, and the second part is configured so as to be separated from the first part under the action of a force oriented along the radial axis and exerted on the second part by a member of the turbine engine forming a stop during a radial movement of the radial shaft.

Access

Download

Export, share and cite

Document information

Title :

TURBINE ENGINE WITH AN OIL GUIDING DEVICE AND METHOD FOR DISASSEMBLING THE TURBINE ENGINE

Contributors:

COTTET CLEMENT (author) / CRETIN FABRICE MICHEL FRANÇOIS RENE (author) / JACQUEMARD CHRISTOPHE PAUL (author) / PERDRIGEON CHRISTOPHE MARCEL LUCIEN (author) / TORIBIO LENY (author)

Publication date :

2018-03-01

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT