Exhaust-gas turbocharger
09726081 · 2017-08-08
Assignee
Inventors
Cpc classification
F02C6/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2220/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/186
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C9/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02B33/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C9/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An exhaust-gas turbocharger having a compressor with a compressor wheel, a turbine with a turbine wheel, a shaft on which the compressor wheel and the turbine wheel are arranged, a control rod for actuating an adjustment apparatus of the exhaust-gas turbocharger, and an actuator for moving the control rod. A damping apparatus with an elastic element is fixedly connected to the control rod and projects in two opposite directions from the control rod.
Claims
1. An exhaust-gas turbocharger (1) comprising: a compressor (2) with a compressor wheel (3), a turbine (5) with a turbine wheel (6), a control rod (10) for actuating an adjustment apparatus (9) of the exhaust-gas turbocharger (1), and an actuator (11) for moving the control rod (10), wherein a damping apparatus (15) comprising an elastic wire cable having a first end and a second end is fixedly connected to the control rod (10) and projects in two opposite directions from the control rod (10) and wherein a first weight is arranged on the first end of the elastic wire cable, a second weight is arranged on the second end of the elastic wire cable, and the first and second weights (19) are at equal distances from the control rod (10).
2. The exhaust-gas turbocharger as claimed in claim 1, wherein the wire cable has a thickness of 1 mm to 10 mm.
3. The exhaust-gas turbocharger as claimed in claim 1, wherein the adjustment apparatus (9) is a charge pressure regulating device which has a shut-off element (25) which opens or closes a flow opening.
4. The exhaust-gas turbocharger as claimed in claim 3, wherein the shut-off element (25) is a flap or a slide.
5. The exhaust-gas turbocharger as claimed in claim 1, wherein the turbine has an inflow region, and wherein the adjustment apparatus is a variable turbine geometry device in which multiple vanes in the inflow region of the turbine (5) are adjustable.
6. The exhaust-gas turbocharger as claimed in claim 1, wherein the two opposite ends of the elastic wire cable extend away from the control rod (10) at an angle less than 90°.
7. The exhaust-gas turbocharger as claimed in claim 1, wherein the wire cable has a thickness of 2 mm to 7 mm.
8. An exhaust-gas turbocharger (1) comprising: a compressor (2) with a compressor wheel (3), a turbine (5) with a turbine wheel (6), a control rod (10) for actuating an adjustment apparatus (9) of the exhaust-gas turbocharger (1), and an actuator (11) for moving the control rod (10), wherein a damping apparatus (15) with an elastic element (18) having a first end and a second end is fixedly connected to the control rod (10) and projects in two opposite directions from the control rod (10), and wherein a first weight is arranged on the first end of the elastic element (18), a second weight is arranged on the second end of the elastic element (18), and the first and second weights (19) are at different distances from the control rod (10).
9. The exhaust-gas turbocharger as claimed in claim 8, wherein the elastic element (18) is a wire cable, and wherein the wire cable has a thickness of 1 mm to 10 mm.
10. The exhaust-gas turbocharger as claimed in claim 8, wherein the elastic element (18) is a wire cable, and wherein the wire cable has a thickness of 2 mm to 7 mm.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
(1) Further details, advantages and features of the invention can be found in the following description of exemplary embodiments with reference to the drawing, in which:
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION OF THE INVENTION
(7) Identical or functionally identical components are denoted by the same reference numerals in all of the exemplary embodiments.
(8)
(9) As a result of the turbine wheel 6 being impinged on by a flow of exhaust gas, the shaft 8 is set in rotation and, as a result, charge air is compressed by means of the compressor 2.
(10) The illustration in
(11) The exhaust-gas turbocharger 1 comprises an actuator 11 which, in the exemplary embodiment illustrated, is controlled by means of compressed air. Electrically driven actuators may likewise be used, as shown in
(12)
(13)
(14) In each case one weight 19 is provided on the ends of the elastic element 18.
(15)
(16) The first profile 20 was recorded without a damping apparatus 15. The second profile 21 was determined using a thin elastic element 18 with two weights 19. The third profile 22 was determined using a damping apparatus 15 with a thin elastic element 18 without weights 19. The fourth profile 23 shows the result using a thick elastic element 18 with two weights 19. The fifth profile 24 was determined using a thick elastic element 18 without weights 19.
(17) From the profiles 23 and 21, it can be seen very clearly that a considerable reduction of a vibration amplitude in natural frequency ranges can be realized using a damping apparatus 15 with elastic element 18 and with weights 19.
(18) However, the profile 22 also shows that, with a corresponding design of the elastic element 18, a positive effect can be achieved even without the use of weights 19.
(19)
(20)
(21) In addition to the above written disclosure of the invention, reference is hereby explicitly made, for additional disclosure thereof, to the diagrammatic illustration of the invention in
LIST OF REFERENCE SIGNS
(22) 1 Exhaust-gas turbocharger 2 Compressor 3 Compressor wheel 4 Compressor housing 5 Turbine 6 Turbine wheel 7 Turbine housing 8 Shaft 9 Adjustment apparatus 10 Control rod 11 Actuator 12 First lever 13 Journal 14 Second lever 15 Damping apparatus 16 Movement 17 Fastening element 18 Elastic element 19 Weights 20 to 24 Profiles 25 Shut-off element