CA2218044C - Hydrodynamic air thrust bearing with offset bump foils - Google Patents
Hydrodynamic air thrust bearing with offset bump foils Download PDFInfo
- Publication number
- CA2218044C CA2218044C CA002218044A CA2218044A CA2218044C CA 2218044 C CA2218044 C CA 2218044C CA 002218044 A CA002218044 A CA 002218044A CA 2218044 A CA2218044 A CA 2218044A CA 2218044 C CA2218044 C CA 2218044C
- Authority
- CA
- Canada
- Prior art keywords
- bump foil
- resilient bump
- thrust bearing
- segments
- foil segments
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/04—Sliding-contact bearings for exclusively rotary movement for axial load only
- F16C17/042—Sliding-contact bearings for exclusively rotary movement for axial load only with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings
Abstract
The leading edges (40, 50) of the segmented corrugated springs of each of the two bump foils (16, 24) of a hydrodynamic thrust bearing (10) an offset such that the leading edge (40) in the upper segmented corrugated springs (16) are circumferentially spaced relative to the leading edge (50) of the lower segmented corrugated springs (24) that is underlying each respective segment of the bump foils. In some embodiments, the leading edge of the bump foil is attached and the trailing edge is free to move axially and in other embodiments, the reverse occurs where the trailing edge of the bump foil is attached and the leading edge is free to move axially.
Description
> CA 02218044 1997-10-10 WO 96/33350 Yf'TIUS96~03079 , , ' ;
Description HYDRODYNAMIC AIR THRUST BEARING WITH OFFSET BUI~ FOILS
Technical Field This invention relates to hydrodynamic air thrust bearings and particularly to the relative orientation of the thrust bearing bump foils with respect to the backing spring bump foils.
Background Art As one skilled in this art appreciates, air foil bearings are extremely sophisticated and highly technical devices and alterations, changes and additions to the composition and configuration of these types of bearings are very critical and can materially affect the operation thereof. An example of a hydrodynamic fluid film thrust bearing is disclosed in U.S. Patent No. 4,462,700 granted to G. L. Agrawal on July 31, 1984 entitled "Hydrodynamic Fluid Film Thrust Bearing" and commonly assigned to United Technologies Corporation. This invention constitutes an improvement over the thrust bearing disclosed in this patent.
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WO 96133350 PCTfUS96103079 Typically, the thrust bearing includes a stationary thrust plate, a rotating thrust runner axially spaced therefrom, and one or two foils disposed therebetween. Each of the foils include backing members having different relative spring rates. In the thrust bearing that includes two foil corrugated backing members, the foil member adjacent to the rotating thrust runner typically is a corrugated metallic member with a relatively high spring rate which has a higher spring constant than the foil member adjacent the stationary thrust plate. This serves to establish and maintain an optimum fluid film geometry under all loading, speed and other operating conditions. The other backing member which has the lower relative spring constant provides the bearing with compliance for adequate load capacity and damping characteristics. It is to be understood that for certain applications it is beneficial to design both backing members to have equal spring rates to achieve particular performance parameters.
As is well known in this technology the surface of the washer shaped thrust bearing foil plate is fitted with a plurality of wedge shaped corrugated thrust bearing bump foils (segments) spaced about the circumference. The leading edge of the corrugated thrust bearing bump foils are welded to the face of the thrust bearing foil plate and the opposite end is unattached and free to move axially.
The top foil which is similarly shaped to the corrugated thrust plate is likewise welded at the leading edge to the thrust bearing foil plate. The leading edge of the top foils is spaced just upstream of the leading edge of the corrugated thrust bearing bump foils. Depending on the particular application, the thrust bearing will consist of several of such segments and the number of segments utilized will principally depend on the optimized performance of such application.
To obtain damping the thrust bearing includes a second washer shaped backing spring foil plate and a plurality of corrugated backing spring bumper foils.
Each of the corrugated backing spring bumper foils are identical in shape and size to each of the corrugated thrust bearing bump foils and their leading or trailing edges are welded to the face of the backing spring foil plate and the opposite end is unattached. The thrust bearing pump foil is attached to the upper face of the foil plate and the backing spring bump is attached to the lower face of its foil plate.
As is well known in this technology, the practice is to axially align the leading edges of the thrust bearing bump foil with the leading edges of the backing spring bump foil. Thus the leading edges and their respective weld joints of all the segments are in axial alignment with each other.
I have found that I can increase thrust bearing load capacity while at the same time reduce running torque by a significant amount by substantially offsetting the leading edge of the thrust bearing bump foil relative to the leading edge of the backing spring bump foil. This improvement in the thrust bearing makes the difference in certain applications of meeting the thrust bearing requirements of certain rotating machinery.
Summary of the Invention An object of this invention is to provide an improved W'O 96/33350 PC~/LIS96103379 hydrodynamic air thrust bearing.
A feature of this invention is to provide for a hydrodynamic air thrust bearing a pair of bump foils that are substantially offset relative to each other.
The foregoing and other features of the present invention will become more apparent from the following description and accompanying drawings.
Brief Description of Drawings Fig. 1 is an exploded view in perspective illustrating the thrust bearing of this invention;
Fig. 2 is a partial sectional view taken through a segment of the overlying top foil, thrust bearing bump foil, thrust bearing foil plate and backing spring foil plate of Fig. 1; and Fig. 3 is a partial sectional view depicting another embodiment of the invention which is substantially the same as Fig. 2 except the weldment for attaching the bump foil to the lower plate is on the trailing edge rather than on the leading edge.
Detailed Description of the Preferred Embodiment This invention is best understood by referring to Figs. 1 and 2 wherein the thrust bearing generally illustrated by reference numeral 10 includes the top plate 12 consisting of foil plate 14, bump foils I6, and top foils 18 and the lower plate 20 consists of foil plate 22, and bump foils 24. As noted in Fig. 1, the foil plates 14 and 22 are annular similar to a washer and include circumferentially spaced tangs 26 and 28 respectively, that include the central recess 32 and 30, ~~r,~~_pluLfl ~'t-~~
WO 96!33350 PCT/IIS96/03079 respectively for attachment to the bearing support (not shown). A plurality of bump foils 16 and an equal number of the top foils 18 of the thrust bearing top plate 12 are circumferentially spaced and attached to the upper face 36 of foil plate 14. As noted in Figs. 2 and 3, each of the bump foils 16 are fabricated from a metallic spring material and are corrugated with the corrugation oriented from the inner to outer diameter, i.e., radially, of the foil plate 14. The leading edge 40 of each of the bump foils are welded to support each of the truncated pie shaped wedge segments of the bump foils 16. The top foils 18 are similarly configured and likewise are fabricated from a high spring rate metallic material although they are not corrugated. The leading edge 42 of each of the top .foils is also attached to the upper face of the top plate 14. The aft ends or trailing edges 44 and 46 of each of the bump foils 16 and top foils 18 are unattached and hence are free to move in the axial direction . As noted in Fig . 2 , the leading edges 42 of the top foils 18 protrude beyond the leading edges 40 of the bump foils 16 in the circumferential direction.
The bump foils 24 are fabricated into a corrugated segment and are made from a spring metallic material whose spring rate is lower than or equal to the spring rate of the bump foils 16 and are likewise corrugated whose corrugations are similarly oriented. In Fig. 2 each of the leading edges 50 are welded to the under face of the lower plate 22. The welding is typically a spot weld process and the weldment are represented by reference numeral 53. As is the case of the bump foils 16 only the leading edge is secured and the aft or trailing edge 54 is free to move axially. For some applications, the design may be optimized (as noted in Fig. 3) by securing the trailing edge 57 of the bump foil 55 by weldment 53 and the leading edge 56 is free to move axially. As is well known the bump foils provide the compliancy, bearing preload, load deflection and spring rate and the use of dual bump foils, as shown, provide the damping. For further details of the operation of this type of bearing reference should be made to U.S. Patent No. 4,672,700, supra.
In accordance with this invention, the bump foils 16 and 24 are circumferentially offset such that the leading edges 40 of bump foils 16 and the leading edges 50 of bump foils 24 are circumferentially spaced with respect to each other. This orientation of the leading edges of the bump foils serves to improve the compliancy characteristics of the thrust bearing and enhance the air wedge to improve air flow over the top foil.
It has been found that by actual tests, this offset bump foil arrangement provides assistance and compliance to the top foil leading edge 42 to form an improved air film to increase load capacity and reduce running torque.
Although this invention has been shown and described with respect to the detailed embodiments thereof, it will be appreciated and understood by those skilled in the art that various changes in form and detail thereof may be made without departing from the scope of the claims.
Description HYDRODYNAMIC AIR THRUST BEARING WITH OFFSET BUI~ FOILS
Technical Field This invention relates to hydrodynamic air thrust bearings and particularly to the relative orientation of the thrust bearing bump foils with respect to the backing spring bump foils.
Background Art As one skilled in this art appreciates, air foil bearings are extremely sophisticated and highly technical devices and alterations, changes and additions to the composition and configuration of these types of bearings are very critical and can materially affect the operation thereof. An example of a hydrodynamic fluid film thrust bearing is disclosed in U.S. Patent No. 4,462,700 granted to G. L. Agrawal on July 31, 1984 entitled "Hydrodynamic Fluid Film Thrust Bearing" and commonly assigned to United Technologies Corporation. This invention constitutes an improvement over the thrust bearing disclosed in this patent.
A~~~vC~~ ~;-i~~T
WO 96133350 PCTfUS96103079 Typically, the thrust bearing includes a stationary thrust plate, a rotating thrust runner axially spaced therefrom, and one or two foils disposed therebetween. Each of the foils include backing members having different relative spring rates. In the thrust bearing that includes two foil corrugated backing members, the foil member adjacent to the rotating thrust runner typically is a corrugated metallic member with a relatively high spring rate which has a higher spring constant than the foil member adjacent the stationary thrust plate. This serves to establish and maintain an optimum fluid film geometry under all loading, speed and other operating conditions. The other backing member which has the lower relative spring constant provides the bearing with compliance for adequate load capacity and damping characteristics. It is to be understood that for certain applications it is beneficial to design both backing members to have equal spring rates to achieve particular performance parameters.
As is well known in this technology the surface of the washer shaped thrust bearing foil plate is fitted with a plurality of wedge shaped corrugated thrust bearing bump foils (segments) spaced about the circumference. The leading edge of the corrugated thrust bearing bump foils are welded to the face of the thrust bearing foil plate and the opposite end is unattached and free to move axially.
The top foil which is similarly shaped to the corrugated thrust plate is likewise welded at the leading edge to the thrust bearing foil plate. The leading edge of the top foils is spaced just upstream of the leading edge of the corrugated thrust bearing bump foils. Depending on the particular application, the thrust bearing will consist of several of such segments and the number of segments utilized will principally depend on the optimized performance of such application.
To obtain damping the thrust bearing includes a second washer shaped backing spring foil plate and a plurality of corrugated backing spring bumper foils.
Each of the corrugated backing spring bumper foils are identical in shape and size to each of the corrugated thrust bearing bump foils and their leading or trailing edges are welded to the face of the backing spring foil plate and the opposite end is unattached. The thrust bearing pump foil is attached to the upper face of the foil plate and the backing spring bump is attached to the lower face of its foil plate.
As is well known in this technology, the practice is to axially align the leading edges of the thrust bearing bump foil with the leading edges of the backing spring bump foil. Thus the leading edges and their respective weld joints of all the segments are in axial alignment with each other.
I have found that I can increase thrust bearing load capacity while at the same time reduce running torque by a significant amount by substantially offsetting the leading edge of the thrust bearing bump foil relative to the leading edge of the backing spring bump foil. This improvement in the thrust bearing makes the difference in certain applications of meeting the thrust bearing requirements of certain rotating machinery.
Summary of the Invention An object of this invention is to provide an improved W'O 96/33350 PC~/LIS96103379 hydrodynamic air thrust bearing.
A feature of this invention is to provide for a hydrodynamic air thrust bearing a pair of bump foils that are substantially offset relative to each other.
The foregoing and other features of the present invention will become more apparent from the following description and accompanying drawings.
Brief Description of Drawings Fig. 1 is an exploded view in perspective illustrating the thrust bearing of this invention;
Fig. 2 is a partial sectional view taken through a segment of the overlying top foil, thrust bearing bump foil, thrust bearing foil plate and backing spring foil plate of Fig. 1; and Fig. 3 is a partial sectional view depicting another embodiment of the invention which is substantially the same as Fig. 2 except the weldment for attaching the bump foil to the lower plate is on the trailing edge rather than on the leading edge.
Detailed Description of the Preferred Embodiment This invention is best understood by referring to Figs. 1 and 2 wherein the thrust bearing generally illustrated by reference numeral 10 includes the top plate 12 consisting of foil plate 14, bump foils I6, and top foils 18 and the lower plate 20 consists of foil plate 22, and bump foils 24. As noted in Fig. 1, the foil plates 14 and 22 are annular similar to a washer and include circumferentially spaced tangs 26 and 28 respectively, that include the central recess 32 and 30, ~~r,~~_pluLfl ~'t-~~
WO 96!33350 PCT/IIS96/03079 respectively for attachment to the bearing support (not shown). A plurality of bump foils 16 and an equal number of the top foils 18 of the thrust bearing top plate 12 are circumferentially spaced and attached to the upper face 36 of foil plate 14. As noted in Figs. 2 and 3, each of the bump foils 16 are fabricated from a metallic spring material and are corrugated with the corrugation oriented from the inner to outer diameter, i.e., radially, of the foil plate 14. The leading edge 40 of each of the bump foils are welded to support each of the truncated pie shaped wedge segments of the bump foils 16. The top foils 18 are similarly configured and likewise are fabricated from a high spring rate metallic material although they are not corrugated. The leading edge 42 of each of the top .foils is also attached to the upper face of the top plate 14. The aft ends or trailing edges 44 and 46 of each of the bump foils 16 and top foils 18 are unattached and hence are free to move in the axial direction . As noted in Fig . 2 , the leading edges 42 of the top foils 18 protrude beyond the leading edges 40 of the bump foils 16 in the circumferential direction.
The bump foils 24 are fabricated into a corrugated segment and are made from a spring metallic material whose spring rate is lower than or equal to the spring rate of the bump foils 16 and are likewise corrugated whose corrugations are similarly oriented. In Fig. 2 each of the leading edges 50 are welded to the under face of the lower plate 22. The welding is typically a spot weld process and the weldment are represented by reference numeral 53. As is the case of the bump foils 16 only the leading edge is secured and the aft or trailing edge 54 is free to move axially. For some applications, the design may be optimized (as noted in Fig. 3) by securing the trailing edge 57 of the bump foil 55 by weldment 53 and the leading edge 56 is free to move axially. As is well known the bump foils provide the compliancy, bearing preload, load deflection and spring rate and the use of dual bump foils, as shown, provide the damping. For further details of the operation of this type of bearing reference should be made to U.S. Patent No. 4,672,700, supra.
In accordance with this invention, the bump foils 16 and 24 are circumferentially offset such that the leading edges 40 of bump foils 16 and the leading edges 50 of bump foils 24 are circumferentially spaced with respect to each other. This orientation of the leading edges of the bump foils serves to improve the compliancy characteristics of the thrust bearing and enhance the air wedge to improve air flow over the top foil.
It has been found that by actual tests, this offset bump foil arrangement provides assistance and compliance to the top foil leading edge 42 to form an improved air film to increase load capacity and reduce running torque.
Although this invention has been shown and described with respect to the detailed embodiments thereof, it will be appreciated and understood by those skilled in the art that various changes in form and detail thereof may be made without departing from the scope of the claims.
Claims (10)
1. A hydrodynamic fluid film thrust bearing comprising an upper plate defining an upper surface, a plurality of resilient bump foil segments spaced circumferentially on said surface, each of said segments including a leading edge and means for attaching said leading edge to said upper plate, a plurality of top foils each having a leading edge circumferentially spaced on said surface and disposed in overlying relationship with said resilient bump foil segment, a lower plate defining a lower surface, said lower plate complementing and being spaced axially and disposed coaxially relative to said upper plate, a plurality of other resilient bump foil segments circumferentially spaced on said lower surface and each other resilient bump foil segment having a leading edge, means for attaching said leading edge to said lower plate, each of said resilient bump foil segments and each of said other resilient bump foil segments being in overlying relationship, characterized in that said upper and lower plates are annular plates and said leading edges of each of said resilient bump foil segments and the leading edges of each of said other bump foil segments in overlying relationship are substantially offset relative to each other.
2. A hydrodynamic fluid film thrust bearing according to claim 1, characterized in that each of said resilient bump foil segments and each of said other resilient bump foil segments are shaped to define corrugations.
3. A hydrodynamic fluid film thrust bearing according to claim 2, characterized in that the orientation of said corrugations is radial.
4. A hydrodynamic fluid film thrust bearing according to claim 3, characterized in that said leading edges of said resilient bump foil segments are spot welded to said upper surface and said leading edges of said other resilient bump foil segments are spot welded to said lower surface.
5. A hydrodynamic fluid film thrust bearing according to claim 4, characterized in that said segments of said resilient bump foil segments and said other resilient bump foil segments are truncated pie shaped wedges.
6. A hydrodynamic fluid film thrust bearing comprising an upper plate defining an upper surface, a plurality of resilient bump foil segments spaced circumferentially on said surface, each of said segments including a leading edge and means for attaching said leading edge to said upper plate, a plurality of top foils each having a leading edge circumferentially spaced on said surface and disposed in overlying relationship with said resilient bump foil segment, a lower plate defining a lower surface, said lower plate complementing and being spaced axially and disposed coaxially relative to said upper plate, a plurality of other resilient bump foil segments circumferentially spaced on said lower surface and each other resilient bump foil segment having a leading edge and a trailing edge, means for attaching one of said leading and trailing edges of said other resilient bump foil segments to said lower plate, each of said resilient bump foil segments and each of said other resilient bump foil segments being in overlying relationship, characterized in that said upper and lower plates are annular plates, that the means for attaching one of said leading and trailing edges is means for attaching said trailing edge of said other resilient bump foil segment to said lower plate and that said leading edges of each of said resilient bump foil segments and the leading edges of each of said other bump foil segments in overlying relationship are substantially offset relative to each other.
7. A hydrodynamic fluid film thrust bearing according to claim 6, characterized in that each of said resilient bump foil segments and each of said other resilient bump foil segments are shaped to define corrugations.
8. A hydrodynamic fluid film thrust bearing according to claim 7, characterized in that the orientation of said corrugations is radially.
9. A hydrodynamic fluid film thrust bearing according to claim 8, characterized in that said leading edges of said resilient bump foil segments are spot welded to said upper surface and said trailing edges of said other resilient bump foil segments are spot welded to said lower surface.
10. A hydrodynamic fluid film thrust bearing according to claim 9, characterized in that said segments of said resilient bump foil segments and said other resilient bump foil segments are truncated pie shaped wedges.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US08/424,030 US5547286A (en) | 1995-04-18 | 1995-04-18 | Hydrodynamic air thrust bearing with offset bump foils |
| US08/424,030 | 1995-04-18 | ||
| PCT/US1996/003079 WO1996033350A1 (en) | 1995-04-18 | 1996-03-05 | Hydrodynamic air thrust bearing with offset bump foils |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2218044A1 CA2218044A1 (en) | 1996-10-24 |
| CA2218044C true CA2218044C (en) | 2006-09-19 |
Family
ID=37056994
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002218044A Expired - Fee Related CA2218044C (en) | 1995-04-18 | 1996-03-05 | Hydrodynamic air thrust bearing with offset bump foils |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2218044C (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109764057A (en) * | 2019-02-01 | 2019-05-17 | 西安交通大学 | A kind of multi stage resilient supporting mechanism and kinetic pressure gas thrust bearing |
-
1996
- 1996-03-05 CA CA002218044A patent/CA2218044C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2218044A1 (en) | 1996-10-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20150305 |