Hydrodynamic bearing

Patent metadata

Field	Value
Publication number	US-10167895-B2
Application number	US-201615552975-A
Country	US
Kind code	B2
Filing date	Feb 23, 2016
Priority date	Feb 24, 2015
Publication date	Jan 1, 2019
Grant date	Jan 1, 2019

Abstract

To overcome defects in the supply of pressurized lubricant, a hydrodynamic bearing for guiding a shaft (14) includes a stationary outer annular wall, a rotatable inner annular wall (20), and a space (22) between the walls. The outer annular wall comprises an opening for supplying pressurized lubricant to the space so as to form a film of load-bearing fluid. The bearing includes a cavity (30) externally defined by the inner annular wall (20) and axially defined by two transverse annular walls (31A, 31B) secured to the shaft (14) and arranged on both sides of the cavity. The inner annular wall (20) comprises fluid connection orifices (32) connecting the cavity (30) to the space (22). The cavity (30) is divided into compartments (50, 52) by a partition wall (48) configured such that the cavity forms a lubricant supply for a transient operational phase.

First claim

What is claimed is:

1. Hydrodynamic bearing ( 16 ) intended to guide a shaft ( 14 ) in rotation about a longitudinal axis ( 17 ) defined relative to a support ( 12 ),
the hydrodynamic bearing comprising a stationary outer annular bearing wall ( 18 ) and a rotatable inner annular bearing wall ( 20 ) extending opposite the outer annular bearing wall ( 18 ) so as to provide an annular space ( 22 ) between the inner and outer annular bearing walls ( 18 , 20 ),
wherein the outer annular bearing wall ( 18 ) comprises at least one lubricant supply orifice ( 24 ) for supplying pressurised lubricant to said annular space ( 22 ) so as to form a load-bearing fluid film,
wherein the hydrodynamic bearing ( 16 ) comprises a cavity ( 30 ) externally defined by the inner annular bearing wall ( 20 ) and axially defined by two transverse annular walls ( 31 A, 31 B) secured to the inner annular bearing wall ( 20 ) and arranged on both sides of the cavity ( 30 ),
the inner annular bearing wall ( 20 ) comprising fluid connection means ( 32 ) that place the cavity ( 30 ) in fluid communication with said annular space ( 22 ),
wherein the hydrodynamic bearing ( 16 ) further comprises partitioning means ( 48 , 68 , 92 , 94 ) connected to the inner annular bearing wall ( 20 ) so as to divide the cavity ( 30 ) into a plurality of compartments ( 50 , 52 , 70 , 72 , 74 , 82 ), the partitioning means forming an obstacle to a flow of lubricant contained in at least one of the compartments under gravitational force (G), towards the fluid connection means ( 32 ), regardless of an angular position of the inner annular bearing wall ( 20 ) when the inner annular bearing wall is at a standstill, such that the cavity ( 30 ) forms a lubricant reserve for a transient operating phase.

2. Hydrodynamic bearing according to claim 1 , wherein the fluid connection means comprise a plurality of lubricant flow orifices ( 32 ) that pass through the inner annular bearing wall ( 20 ) and that are regularly distributed about the longitudinal axis ( 17 ).

3. Hydrodynamic bearing according to claim 1 , comprising a ring ( 40 ) intended to be mounted on the shaft ( 14 ) such that the ring can be removed therefrom, said ring ( 40 ) integrating said inner annular bearing wall ( 20 ) in addition to said two transverse annular walls ( 31 A, 31 B).

4. Hydrodynamic bearing according to claim 1 , wherein the partitioning means comprise a partition wall ( 48 ) of annular shape, dividing the cavity ( 30 ) into two compartments ( 50 , 52 ) arranged one behind the other along the longitudinal axis ( 17 ), said partition wall comprising at least one opening ( 54 ) defined by the inner annular bearing wall ( 20 ) and circumferentially offset relative to the fluid connection means ( 32 ).

5. Hydrodynamic bearing according to claim 1 , wherein the partitioning means comprise partition walls ( 68 ) extending longitudinally from one to the other of said transverse annular walls ( 31 A, 31 B), so as to divide the cavity ( 30 ) into a plurality of compartments ( 70 , 72 , 74 ) distributed about the longitudinal axis ( 17 ), the partition walls ( 68 ) being circumferentially offset relative to the fluid connection means ( 32 ).

6. Hydrodynamic bearing according to claim 1 , wherein the partitioning means divide the cavity ( 30 ) into a plurality of compartments ( 82 ) circumferentially offset relative to the fluid connection means ( 32 ) and regularly distributed about the longitudinal axis ( 17 ), and into a distribution channel ( 84 ) connecting each compartment ( 82 ) to the fluid connection means ( 32 ) and comprising a circumferential portion ( 86 ) that is axially offset on a same side relative to each compartment ( 82 ) and the fluid connection means ( 32 ), in addition to first connection portions ( 88 ) that respectively connect the compartments ( 82 ) of the cavity to the circumferential portion ( 86 ) of the distribution channel and which are angularly offset relative to circumferential ends ( 90 ) of each compartment.

7. Hydrodynamic bearing according to claim 6 , wherein the fluid connection means ( 32 ) are located axially on a same side of the circumferential portion ( 86 ) of the distribution channel ( 84 ) as the compartments ( 82 ) of the cavity ( 30 ).

8. Turbomachine ( 100 ), in particular for an aircraft, comprising a support ( 12 ), a shaft ( 14 ) and at least one hydrodynamic bearing ( 16 ) according to claim 1 , the outer annular bearing wall ( 18 ) of which is secured to the support ( 12 ) and the inner annular bearing wall ( 20 ) of which is secured to the shaft ( 14 ), such that the hydrodynamic bearing ( 16 ) contributes to the guiding of the shaft ( 14 ) in rotation.

9. Turbomachine according to claim 8 , wherein the shaft ( 14 ) forms a part of an accessory gear box ( 108 ) of the turbomachine.

10. Method for lubricating a hydrodynamic bearing ( 16 ) according claim 1 , comprising:
at least one transient operating phase wherein lubricant ( 60 ) previously stored in the cavity ( 30 ) is injected into said annular space ( 22 ) by passing through the fluid connection means ( 32 ) under centrifugal force, and
a steady-state operating phase, wherein pressurised lubricant is supplied to said annular space ( 22 ) through each lubricant supply orifice ( 24 ), and a part of the lubricant penetrates the cavity ( 30 ) through the fluid connection means ( 32 ).

Assignees

• Safran Trans Systems

Inventors

• Bauduin Lionel
• Guillemont Maxence
• Morelli Boris
• Viel Julien

Classifications

• F01D25/166 Primary

  Sliding contact bearing (gas bearings F01D25/22) · CPC title

• F16C33/106

  Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid · CPC title

• F16C33/107

  Grooves for generating pressure · CPC title

• F16C33/1045

  Details of supply of the liquid to the bearing · CPC title

• F01D25/186

  for sliding contact bearing · CPC title