Non symmetrical bi-directional thrust bearing with two active faces

Patent metadata

Field	Value
Publication number	US-10458466-B2
Application number	US-201415034946-A
Country	US
Kind code	B2
Filing date	Oct 27, 2014
Priority date	Nov 13, 2013
Publication date	Oct 29, 2019
Grant date	Oct 29, 2019

Abstract

A bearing device supports a shaft of a gas turbine engine. A first support disk is mounted to the bearing housing element. First tilting pads are tiltably arranged one after another along a circumferential direction at the first support disk. A second support disk is mounted to the bearing housing element spaced apart from the first support disk along an axial direction. Second tilting pads are tiltably arranged one after another along the circumferential direction at the second support disk. A first number of the first tilting pads is greater than the half of a second number of the second tilting pads but smaller than the second number of the second tilting pads.

First claim

The invention claimed is:

1. A bearing device for supporting a shaft of a gas turbine engine, the bearing device comprising
a bearing housing element,
a first support disk which is mounted to the bearing housing element,
first tilting pads, which are tiltably arranged one after another along a circumferential direction and secured to the first support disk in a manner that prevents movement of the first tilting pads in an axial direction,
a second support disk which is mounted to the bearing housing element spaced apart from the first support disk along the axial direction,
second tilting pads, which are tiltably arranged one after another along the circumferential direction and secured to the second support disk in a manner that prevents movement of the second tilting pads in the axial direction,
wherein the first tilting pads are arranged with respect to a first thrust collar mounted to the shaft such that a first axial thrust is transferrable from the first thrust collar to the first tilting pads, and
wherein the second tilting pads are arranged with respect to a second thrust collar mounted to the shaft such that a second axial thrust which is orientated in opposite direction with respect to the first axial thrust is transferrable from the second thrust collar to the second tilting pads,
wherein a first number of the first tilting pads is greater than the half of a second number of the second tilting pads but smaller than the second number of the second tilting pads,
wherein the first tilting pads define a first axial thrust capacity and the second tilting pads define a second axial thrust capacity that is different than the first axial thrust capacity,
wherein the first tilting pads are unequally distributed onto a first support surface of the first support disk along the circumferential direction, and
wherein the second tilting pads are equally distributed onto a second support surface of the second support disk along the circumferential direction.

2. The bearing device according to claim 1 , further comprising
at least three journal pads which are mounted to the first support disk and the second support disk spaced apart from each other along the circumferential direction,
wherein the at least three journal pads are arranged between the first support disk and the second support disk such that a radial force is transferrable between the at least three journal pads and the shaft and such that the shaft is rotatable with respect to the at least three journal pads.

3. The bearing device according to claim 1 ,
wherein the first support disk comprises at least one spacer element which protrudes from the first support surface along the axial direction, and
wherein each spacer element of the at least one spacer element is arranged between two adjacent first tilting pads of the first tilting pads for preventing a contact of the two adjacent first tilting pads.

4. The bearing device according to claim 3 ,
wherein the at least one spacer element is a blanked nozzle.

5. The bearing device of claim 4 , further comprising:
plural gaps between the first tilting pads, wherein a first gap of the plural gaps is larger than a second gap of the plural gaps, wherein the at least one spacer element is disposed at a leading edge of the first gap with respect to a direction of rotation of the first thrust collar.

6. The bearing device according to claim 3 ,
wherein the at least one spacer element is an oil lubrication nozzle for injecting oil such that a lubrication oil film between the first tilting pads and the first thrust collar is generatable.

7. The bearing device according to claim 1 ,
wherein more than ⅔ of the first tilting pads are arranged onto a first half of the first support disk and less than ⅓ of the first tilting pads are arranged onto a second half of the first support disk.

8. The bearing device according to claim 1 ,
wherein the first number of the first tilting pads is 6 to 11 and the second number of the second tilting pads is 12 to 21.

9. The bearing device of claim 1 , further comprising:
plural gaps between the first tilting pads, wherein a first gap of the plural gaps is larger than a second gap of the plural gaps,
wherein the bearing housing element protrudes into the first support disk at a location that is circumferentially aligned with the first gap and the first tilting pads.

10. A gas turbine engine, comprising the bearing device according to claim 1 ,
a gas turbine housing,
a shaft,
the first thrust collar which is mounted to the shaft,
the second thrust collar which is mounted to the shaft,
wherein the first thrust collar is arranged spaced apart from the second thrust collar along the axial direction, and
wherein the bearing housing element is mounted to the gas turbine housing.

Assignees

• Siemens Ag

Inventors

• Hird James

Classifications

• F01D25/16

  Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title

• F16C17/107

  with at least one surface for radial load and at least one surface for axial load · CPC title

• F05D2240/52

  Axial thrust bearings · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F16C2360/23

  Gas turbine engines · CPC title