Bearing assembly, in particular for a turbomachine, and turbomachine having such a bearing assembly
10329952 ยท 2019-06-25
Assignee
Inventors
- Michael Flouros (Munich, DE)
- Peter Gloeckner (Schweinfurt, DE)
- Patrick Mirring (Schwebheim, DE)
- Matthias Martin (Wuerzburg, DE)
Cpc classification
F16C33/303
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/6651
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/76
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/077
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/125
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/186
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2360/23
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C37/007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/583
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C27/045
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/6659
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16C33/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/66
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/76
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/077
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A bearing assembly (2) is provided, in particular for a turbomachine, including: an inner bearing race (3); an outer bearing race (4) having at least one cooling channel (15) formed within it or in its outer surface; rolling elements (7) made of ceramic and disposed between the inner bearing race (3) and the outer bearing race (4); and a surrounding bearing ring (9) connected to the outer bearing race (4) and configured to form a squeeze film (10) of oil between its outer surface and an opposite inner surface of a housing (1) in which the bearing assembly can be mounted.
Claims
1. A bearing assembly comprising: an inner bearing race; an outer bearing race disposed opposite the inner bearing race and having at least one cooling channel; rolling elements made of ceramic and disposed between the inner bearing race and the outer bearing race; and a surrounding bearing ring connected to the outer bearing race and configured to form a squeeze film of oil between an outer surface of the bearing ring and an opposite inner surface of a housing in which the bearing assembly can be mounted.
2. The bearing assembly as recited in claim 1 wherein the inner bearing race or the outer bearing race is provided with residual compressive stress, the residual compressive stress being induced in the inner bearing race or the outer bearing race.
3. The bearing assembly as recited in claim 2 wherein the residual compressive stress is induced by a nitriding process.
4. The bearing assembly as recited in claim 3 wherein the residual compressive stress is further induced by an additional heat treatment.
5. The bearing assembly as recited in claim 1 wherein the at least one cooling channel is formed within the outer bearing race or in a bearing race outer surface of the outer bearing race.
6. The bearing assembly as recited in claim 5 wherein the at least one cooling channel in the bearing race outer surface of the outer bearing race is formed using a mechanical machining process, or the at least one cooling channel within the outer bearing race is formed using an additive manufacturing process.
7. The bearing assembly as recited in claim 6 wherein the at least one cooling channel is formed within the outer bearing race using laser melting or laser sintering.
8. The bearing assembly as recited in claim 1 wherein the cooling channel is circular, triangular, semicircular, slot-shaped, oval or polygonal in cross section; the dimensions or shape of the cross section of the cooling channel is constant or varying along the length of the cooling channel.
9. The bearing assembly as recited in claim 1 wherein the bearing ring has at least one oil distribution groove in the outer surface.
10. The bearing assembly as recited in claim 1 wherein a seal is provided on the outer surface of the bearing ring in order to seal the two ends of the squeeze film; the bearing ring being provided on the outer surface with a receiving recess and a sealing element received therein.
11. The bearing assembly as recited in claim 10 wherein the sealing element is located at both ends of the squeeze film in order to seal the squeeze film.
12. The bearing assembly as recited in claim 1 wherein the bearing ring is provided at one side with a coolant feed duct coupled to the at least one cooling channel of the outer bearing race for supplying coolant.
13. The bearing assembly as recited in claim 1 wherein the coolant feed duct supplies the coolant through a coolant distribution groove; with oil being used as the coolant.
14. The bearing assembly as recited in claim 1 wherein the bearing ring has a coolant supply passage for supplying oil of the squeeze film to the cooling channel; the coolant supply passage extending from the outer surface of the bearing ring to the at least one cooling channel of the outer bearing race, or to a connecting channel of the outer bearing race to the at least one cooling channel.
15. The bearing assembly as recited in claim 1 wherein the outer bearing race has a coolant drain duct connected to the at least one cooling channel for draining coolant from the cooling channel to the exterior.
16. The bearing assembly as recited in claim 1 wherein the inner bearing race has at least one coolant supply duct.
17. The bearing assembly as recited in claim 16 wherein the inner bearing race is made in one piece or in two pieces.
18. The bearing assembly as recited in claim 1 wherein the inner bearing race or the outer bearing race has at least one receptacle for receiving a sensor.
19. The bearing assembly as recited in claim 18 wherein the sensor is a thermocouple.
20. The bearing assembly as recited in claim 1 wherein the bearing ring and outer bearing race are joined by an interlocking or frictional connection.
21. The bearing assembly as recited in claim 1 wherein the bearing ring and outer bearing race are joined by an interference fit, a threaded connection, a welded connection, interlocking teeth or a keyed connection.
22. A turbomachine comprising the bearing assembly as recited in claim 1.
23. The turbomachine as recited in claim 22 further comprising a housing, the bearing assembly disposable in the housing for supporting a shaft of the turbomachine.
24. An aircraft engine or a gas turbine comprising the turbomachine as recited in claim 23.
25. A stationary gas turbine comprising the turbomachine as recited in claim 23.
26. The bearing assembly as recited in claim 1 wherein the squeeze film is sealed laterally between the housing and the bearing ring to prevent the oil from escaping laterally.
27. The bearing assembly as recited in claim 1 further comprising lateral seals between the bearing ring and the housing and sealing the squeeze film of oil laterally.
28. The bearing assembly as recited in claim 1 wherein the inner bearing race has a coolant supply duct.
29. The bearing assembly as recited in claim 1 further comprising a cage between the inner race and the outer race.
30. The bearing assembly as recited in claim 1 wherein the inner race has a groove, the rolling elements running in the groove.
Description
BRIEF DESCRIPTION OF THE DRAWING
(1) Other features and advantages of the present invention are described below with reference to the FIGURE.
(2)
DETAILED DESCRIPTION
(3)
(4) In the inventive bearing assembly 2, which will be described in detail below with reference to
(5) Thus, the inventive bearing assembly 2 makes it possible to reduce power losses and temperatures, to increase the service life and resistance to rolling wear, and to reduce the required quantity of oil and the bearing and system weight while at the same time enabling increased speed or RPM.
(6) The bearing assembly 2 embodied according to the present invention and shown in
(7) The rolling elements 7 of the bearing assembly are received between inner bearing race 3 and outer bearing race 4 and may additionally be guided, for example within an optional cage 8.
(8) Rolling elements 7 are in this case made of ceramic, in particular of a high-performance ceramic material, such as, for example, Si.sub.3N.sub.4. The rolling elements 7 made of ceramic have the advantage over conventional steel rolling elements that they dissipate less power.
(9) In the exemplary embodiment shown in
(10) Bearing assembly 2 further has a surrounding bearing ring 9, which is connected to outer bearing race 4. The connection between surrounding bearing ring 9 and outer bearing race 4 is created by an interlocking and/or frictional connection, such as, for example, an interference fit, a threaded connection, a welded connection, interlocking teeth and/or a keyed connection, etc. However, the present invention is not limited to the mentioned examples of interlocking and/or frictional connections. The inventive bearing assembly 2 has the advantage that outer bearing race 4 does not necessarily have to be flange-mounted to an associated housing in centered relationship thereto via additional, so-called spring bars, as in the prior art, but rather can be connected freely; i.e., without being centered, to the surrounding bearing ring 9 required for squeeze film damping, as illustrated in the exemplary embodiment in
(11) In this connection, a squeeze film 10 of oil or lubricating oil for damping bearing assembly 2 is formed between the outer surface of surrounding bearing ring 9 and the opposite inner surface of housing 1. In the exemplary embodiment shown in
(12) Oil distribution groove 11 may be coupled or connected, for example, to an oil supply duct 12 of housing 1, as shown in the exemplary embodiment in
(13) In this connection, as shown in
(14) Due to the self-centering action of the inventive bearing assembly 2, the squeeze film damper or squeeze film damping of bearing assembly 2 has no static stiffness. The dynamic stiffness does not develop until a shaft supported by bearing assembly 2 reaches a certain rotational speed. Thus, the bearing assembly 2 according to the present invention provides a reduction in weight, axial space, and assembly effort as compared to a conventional, centered design.
(15) Outer bearing race 4 has at least one cooling channel 15. In the exemplary embodiment shown in
(16) Cooling channel 15 may, for example, be formed as a recess, such as a groove, in the outer surface of outer bearing race 4, as illustrated in
(17) In the exemplary embodiment of the inventive bearing assembly shown in
(18) Similarly, in the case of a cooling channel 15 provided within outer bearing race 4, a corresponding coolant feed duct may be provided for supplying the coolant to cooling channel 15. Such coolant feed ducts may be formed by drilling or, like the respective cooling channel 15 within outer bearing race 4, using an additive manufacturing process, such as laser sintering or laser melting, etc. Optionally additionally, an additional coolant drain duct 21 may be provided in outer bearing race 4, such as, for example, a bore for removing the coolant from cooling channel 15 after cooling of cooling channel 15. Such bores may be formed, for example, by drilling or using an additive manufacturing process such as, for example, laser melting or laser sintering, etc.
(19) The cooling of outer bearing race 4 by providing outer bearing race 4 with at least one cooling channel 15 allows the energy dissipated in the rolling contacts to be very effectively removed. Furthermore, the use of rolling elements 7 of ceramic makes it possible to reduce centrifugal loading as well as the power losses occurring in the rolling contact.
(20) In a further embodiment of the present invention, as indicated by a dotted line in
(21) In the case of a cooling channel 15 present within outer bearing race 4, outer bearing race 4 is provided with a corresponding feed duct (not shown) connecting coolant supply passage 22 of surrounding bearing ring 9 to cooling channel 15 of outer bearing race 4.
(22) Moreover, outer bearing race 4 is provided with a coolant drain duct 21 (also indicated by a dotted line in
(23) This embodiment of bearing assembly 2 has the advantage that the damper oil of squeeze film 10 can be used for direct cooling of the outer bearing race. To this end, as previously described, outer bearing race 4 merely has provided therein a coolant supply passage 22 from squeeze film 10, which functions as damper oil film, to cooling channel 15 of outer bearing race 4, as well as a removing of this oil from outer bearing race 4 via a coolant drain duct 21. In this embodiment of the inventive bearing assembly 2, the previously described coolant feed duct 20 in outer bearing race 4 can be dispensed with because the oil for squeeze film 10 is additionally used as the coolant for cooling channel 15.
(24) As shown in the exemplary embodiment in
(25) In another embodiment of the inventive bearing assembly 2, a receptacle 25, or, as in the exemplary embodiment in
(26) In the bearing assembly 2 according to the present invention, in addition and preferably, residual compressive stresses are selectively introduced in outer bearing race 4 and/or inner bearing race 3, which, for example, are made of steel. Such residual compressive stresses in the outer and/or inner bearing races have the advantage of making it possible to counteract progressive damage, for example, which may be caused, for example, by cracks in the component. Such residual compressive stresses may be introduced into outer bearing race 4 and/or inner bearing race 3, for example, by a nitriding process and optionally additionally by a heat treatment. This increases the hardness and strength of outer bearing race 4 and/or inner bearing race 3.
(27) In the inventive bearing assembly 2, both the squeeze film damping at the outer diameter of surrounding bearing ring 9, cooling channel 15 on outer bearing race 4, as well as the lubricating cooling supply can be supplied via a shaft supported by bearing assembly 2 with in each case one oil supply passage 20, 22 intended for this purpose. In this connection, the oil can serve as a coolant and lubricant.
(28) As previously described, it is generally possible that the oil used for squeeze film damping can, at the same time, be also used for cooling the outer bearing race. By directly cooling outer bearing race 4, the temperature of the outer bearing race decreased significantly and the loading in the rolling contact is reduced. At the same time, a reduced material temperature of outer bearing race 4 means increased resistance to classic rolling-contact fatigue and surface fatigue. In contrast to the so-called under-race cooling via the small lateral surfaces of inner bearing race, a separation between lubrication and cooling is achieved for outer bearing race 4. The quantity of oil supplied for lubrication and cooling via the additional coolant supply duct 24 in inner bearing race 3 can thus be significantly reduced. As a result, the churning and splashing losses of bearing assembly 2 are reduced. The lower bearing temperature and the smaller quantity of oil required also mean a reduced oil weight, which not only allows for a smaller oil reservoir, but also for a smaller dimensioned oil/air and oil/fuel cooler. Moreover, in cases where smaller oil quantities are required, it is possible to use smaller, more efficient oil pumps. That is, the entire oil system architecture benefits from the use of the inventive bearing assembly 2 with regard to power and weight savings and increases in efficiency.
(29) The inventive bearing assembly described hereinbefore by way of example can be used as a rolling-element bearing assembly in particular in thermally and mechanically highly loaded applications, such as in aircraft engines and stationary gas turbines, for example as main shaft bearings of aircraft engines or stationary gas turbines. However, the present invention is not limited to the applications mentioned.
(30) Although the present invention has been completely described above with reference to preferred exemplary embodiments, it is not limited thereto, but may be modified in many ways. In particular, the exemplary embodiments described above with reference to
LIST OF REFERENCE NUMERALS
(31) 1 housing 2 bearing assembly 3 inner bearing race 4 outer bearing race 5 first inner bearing race half 6 second inner bearing race half 7 rolling element 8 cage 9 surrounding bearing ring 10 squeeze film 11 oil distribution groove 12 oil supply duct (housing) 13 receiving recess 14 sealing element 15 cooling channel 16 circular cross section 17 triangular cross section 18 polygonal cross section 19 cross section in the shape of a slot 20 coolant feed duct (outer bearing race) 21 coolant drain duct (outer bearing race) 22 coolant supply passage 24 coolant supply duct (inner bearing race) 25 receptacle for thermocouple 26 coolant distribution groove