FIELD: machine building.
SUBSTANCE: invention relates to a device for transferring oil between two coordinate systems rotating relative to each other and in particular, but not exclusively, between a static housing and a speed reducing device or gearbox of a gas turbine engine with twin reverse rotation propellers. Invention also relates to a gas turbine engine comprising said oil transfer device. Device (20) comprises two concentric rings, outer ring (22) and inner ring (23), one of which is connected to an oil supply from one of the coordinate systems, and the other ring being connected to the other coordinate, the oil flowing between said rings, and bearings between the rings in order to change coordinate systems between the two rings. According to the invention, device (20) further comprises flexible means (31) forming a shock absorber, provided between a first of said rings and intermediate ring (41) that is separated from a second of said rings by said bearings (25), said flexible means (31) defining deformable sealed chamber (32) in which oil travels between the two coordinate systems.
EFFECT: invention compensates for displacements, in particular radial and angular displacements, which allows to maintain the alignment between the two coordinate systems.
10 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
OIL-PRESSURE COVER FOR GAS TURBINE ENGINE UNIT | 2015 |
|
RU2690900C2 |
REDUCTION GEAR WITH EPICYCLOID TRANSMISSION FOR GAS TURBINE ENGINE | 2016 |
|
RU2704516C2 |
EPICYCLIC REDUCTION GEAR WITH FLUID TRANSFER PIPES, AND PROPELLER TURBOMACHINE FOR AIRCRAFT WITH SUCH REDUCTION GEAR | 2014 |
|
RU2653671C2 |
GAS TURBINE ENGINE MODULE COMPRISING CRANKCASE AROUND UNIT WITH CASING FOR LUBING OIL RECUPERATION | 2015 |
|
RU2688048C2 |
SEALED FRONT CHAMBER DURING MODULAR DISMANTLING OF TURBOJET WITH REDUCTION GEAR | 2014 |
|
RU2674837C1 |
FAN MODULE WITH VARIABLE ANGLE BLADES | 2019 |
|
RU2794134C2 |
REDUCTION GEAR WITH TWO INTERMEDIATE TRANSMISSION LINES | 2015 |
|
RU2688494C2 |
PORTABLE CONTRA-PROPS SYSTEM | 2010 |
|
RU2526130C2 |
CYCLOIDAL REDUCER, FAN MODULE OF DUAL-FLOW TURBOJET ENGINE AND DUAL-FLOW TURBOJET ENGINE | 2013 |
|
RU2627990C2 |
MODULAR ENGINE, SUCH AS JET ENGINE, WITH SPEED REDUCTION GEAR | 2014 |
|
RU2674098C1 |
Authors
Dates
2018-08-28—Published
2014-10-01—Filed