Exhaust gas turbocharger with vibration-insulating mounting of a rotor
09689425 ยท 2017-06-27
Assignee
Inventors
Cpc classification
F01D25/164
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/4206
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F1/324
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/96
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/077
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/668
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/059
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/54
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/527
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F1/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2250/314
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2360/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/184
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16C27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/059
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F1/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16F1/34
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/52
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C35/077
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C19/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An exhaust gas turbocharger may include a rotor mounted in a bearing housing via a rolling bearing. The rolling bearing may include an outer shell, an inner shell and rolling bodies running therebetween. At least one annular and vibrational noise absorbing diaphragm spring element may be arranged between the outer shell of the rolling bearing and the bearing housing. The diaphragm spring element may mount the rotor in radial direction and axial direction in a vibration-insulating manner with respect to the bearing housing.
Claims
1. An exhaust gas turbocharger, comprising: a rotor mounted in a bearing housing via a rolling bearing, wherein the rolling bearing includes an outer shell, an inner shell and rolling bodies running therebetween, at least one annular and vibrational noise absorbing diaphragm spring element arranged between the outer shell of the rolling bearing and the bearing housing, the diaphragm spring element mounting the rotor in radial direction and axial directions in a vibration-insulating manner with respect to the bearing housing, and a retaining ring arranged axially between a radial surface of the bearing housing and a radial surface of the diaphragm spring element.
2. The exhaust gas turbocharger according to claim 1, wherein the diaphragm spring element is formed of metal.
3. The exhaust gas turbocharger according to claim 1, wherein the diaphragm spring element includes an outer ring and an inner ring connected therewith via ribs.
4. The exhaust gas turbocharger according to claim 3, wherein the ribs are arranged at an angle relative to the radial direction.
5. The exhaust gas turbocharger according to claim 3, wherein the ribs connect to the inner ring at a first connection point radially in the direction of the outer ring, the ribs connect to the outer ring at a second connection point radially in the direction of the inner ring, and the first and the second connection points are not located on a common radial ray.
6. The exhaust gas turbocharger according to claim 1, wherein the diaphragm spring element is formed as a punched part.
7. The exhaust gas turbocharger according to claim 1, wherein the diaphragm spring element is at least one of fixed to the outer shell of the rolling bearing and fixed to the bearing housing.
8. The exhaust gas turbocharger according to claim 7, wherein the diaphragm spring element is one of welded in, clamped in, or flanged on to the outer shell of the rolling bearing.
9. The exhaust gas turbocharger according to claim 1, wherein the retaining ring includes a plastic contact region via which the retaining ring is in contact with the diaphragm spring element.
10. A diaphragm spring element for an exhaust gas turbocharger, comprising: an annular outer ring connected to an annular inner ring via a plurality of circumferentially spaced ribs, wherein the respective ribs are arranged between the outer ring and the inner ring at an angle with respect to a radial direction and are formed at least one of straight and wavy; wherein the inner ring and the outer ring are solid circumferentially.
11. The diaphragm spring element according to claim 10, wherein the ribs connect to the inner ring at a first connection point radially in the direction of the outer ring, the ribs connect to the outer ring at a second connection point radially in the direction of the inner ring, and the first and the second connection point are not located on a common radial ray.
12. The diaphragm spring element according to claim 11, wherein the respective ribs are arranged obliquely to the radial direction.
13. The exhaust gas turbocharger according to claim 4, wherein the ribs connect to the inner ring at a first connection point radially in the direction of the outer ring; the ribs connect to the outer ring at a second connection point radially in the direction of the inner ring; and the first and second connection points are offset in circumferential direction relative to one another.
14. The exhaust gas turbocharger according to claim 7, wherein the diaphragm spring element is fixed to the bearing housing via the retaining ring.
15. The exhaust gas turbocharger according to claim 1, wherein the retaining ring includes an elastomer contact region, the contact region being connected to an outer ring of the diaphragm spring element.
16. An exhaust gas turbocharger, comprising: a rotor mounted in a bearing housing via a rolling bearing, the rolling bearing including an outer shell, an inner shell and rolling bodies running therebetween; at least one annular diaphragm spring element disposed between the outer shell of the rolling bearing and the bearing housing, the diaphragm spring element including an annular outer ring connected to an annular inner ring via a plurality of circumferential spaced ribs, the ribs being arranged between the outer ring and the inner ring at an angle with respect to a radial direction; and a retaining ring arranged axially between a radial surface of the bearing housing and a radial surface of the diaphragm spring element; wherein the diaphragm spring element is connected to the outer shell of the rolling bearing via the inner ring and is connected to the bearing housing via the outer ring, and wherein the diaphragm spring element mounts the rotor in the radial and axial directions in a vibration-insulating manner with respect to the bearing housing.
17. The exhaust gas turbocharger according to claim 16, wherein the retaining ring includes an elastomer contact region connected to the outer ring of the diaphragm spring element, wherein the outer ring of the diaphragm spring element is fixed to the bearing housing via the retaining ring.
18. The exhaust gas turbocharger according to claim 16, wherein the outer shell of the rolling bearing includes at least one groove into which the inner ring of the diaphragm spring element engages.
19. The exhaust gas turbocharger according to claim 16, wherein the ribs connect to the inner ring at a first connection point radially in the direction of the outer ring; the ribs connect to the outer ring at a second connection point radially in the direction of the inner ring; and the first and second connection points are offset in circumferential direction relative to one another.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Here it shows, in each case schematically:
(2)
(3)
(4)
DETAILED DESCRIPTION
(5) According to the
(6) With previous mountings of the rotor 2 there was frequently the problem that said rotor was mounted in the bearing housing in a structure-borne noise vibration-reducing manner in radial direction, but not in axial direction, so that when a rotor ran up against the bearing housing in axial direction structure-borne noise transmission which, under certain conditions, was direct, would occur. With the exhaust gas turbocharger 1 according to the invention this is no longer possible since the diaphragm spring element 7 is fixed, in particular welded in, clamped in or flanged on to the outer shell 8 of the rolling bearing 3 and directly or indirectly to the bearing housing 4 via a retaining ring 11. By fixing the diaphragm spring element 7 on the one hand on the rolling bearing 3 and on the other hand directly or indirectly on the bearing housing 4, the rotor 2 can only move in axial direction 12 to a limited degree and do so additionally merely in a cushioned manner. Connecting the diaphragm spring element 7 to the outer shell 8 of the rolling bearing 3 can for example be brought about by a suitable groove 12 on the outer shell 8, in which the diaphragm spring element 7 engages with an inner ring 13. Generally, the diaphragm spring element 7 is constructed of the inner ring 13, an outer ring 14 as well as ribs 15 connecting the two rings 13, 14 (see
(7) Generally, the diaphragm spring element 7 can be formed of metal, in particular produced as punched part in a cost-effective and economical manner. Considering the diaphragm spring element 7 according to
(8) The embodiment of the diaphragm spring element 7 according to the invention shown according to
(9) Looking at the retaining ring 11 according to
(10) By way of the material selection for the diaphragm spring element 7 and in particular also the geometrical arrangement or orientation of the individual ribs 15 and their number, the axial or radial spring stiffness of the diaphragm spring element 7 can be individually adjusted. By forming the diaphragm spring element 7 as a cost-effective sheet metal punched part it is not only resistant and can be employed over the entire lifespan of the exhaust gas turbocharger 1, but can also be additionally produced cost-effectively.