IP Library Granted Patent US 10,385,864
Granted Patent B2
US 10,385,864 · App. 15/227,943 · Granted Aug 20, 2019

Compressor wheel of a charging device

Inventor: Kinh Toai Pham (Ludwigsburg, DE)
Assignee: BMTS Technology GmbH & Co. KG
F04D29/26F01D5/021F01D5/043F01D5/048F02B33/00F02B37/00F02C6/12F04D25/04F04D29/284F05B2220/40F05B2240/30F05D2220/40F05D2250/611Y02T10/144
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Quick Facts
Patent No.
US 10,385,864
App. No.
15/227,943
Granted
Aug 20, 2019
Kind
B2
Abstract

A compressor wheel of a charging device may include a hub, a plurality of blades and a wheel back. The wheel back may have an undulating profile which extends from the hub in a radial direction. The undulating profile may include a plurality of regions. The plurality of regions may adjoin one another and may include a first concave region, a second convex region, a third concave region, and a fourth convex region. The second convex region may adjoin the first concave region. The third concave region may adjoin the second convex region. The fourth convex region may adjoin the third concave region.

Claims (45)

1. A compressor wheel of a charging device, comprising: a hub, a plurality of blades and a wheel back, wherein the wheel back has an undulating profile which extends from the hub in a radial direction, the undulating profile including a plurality of regions which emerge from the hub in the radial direction and adjoin one another, wherein the plurality of regions of the undulating profile include:

a first concave region;

a second convex region adjoining the first concave region;

a third concave region adjoining the second convex region; and

a fourth convex region adjoining the third concave region; and

wherein at least one of the first concave region has a radial extent of approx. 7% of a radius of the compressor wheel, and the fourth convex region has a radial extent of approx. 20% of a radius of the compressor wheel.

2. The compressor wheel according to claim 1 , wherein the fourth convex region includes a bulge that has an axial height of approx. 0.15 mm.

3. The compressor wheel according to claim 1 , wherein the hub extends from an axis of rotation to the first concave region and the hub includes a flat end surface.

4. The compressor wheel according to claim 3 , wherein the flat end surface has a radial extent of approx. 15% of the radius of the compressor wheel.

5. The compressor wheel according to claim 1 , wherein the first concave region has a radial extent of approx. 7% of the radius of the compressor wheel.

6. The compressor wheel according to claim 1 , wherein the second convex region has the radial extent of approx. 25% of the radius of the compressor wheel, and the fourth convex region has the radial extent of approx. 20% of the radius of the compressor wheel.

7. The compressor wheel according to claim 1 , wherein the third concave region has a radial extent of approx. 30% of the radius of the compressor wheel.

8. An exhaust gas turbocharger, comprising: a compressor wheel, the compressor wheel including:

a hub;

a plurality of blades; and

a wheel back, the wheel back having an undulating profile that extends from the hub in a radial direction;

the undulating profile including a plurality of regions extending from the hub in the radial direction, wherein the plurality of regions of the undulating profile include a first concave region, a second convex region, a third concave region, and a fourth convex region;

wherein the second convex region is disposed between the first concave region and the third concave region, and the third concave region is disposed between the second convex region and the fourth convex region; and

wherein at least one of:

the first concave region has a radial extent of approx. 7% of a radius of the compressor wheel;

the second convex region has a radial extent of approx. 25% of a radius of the compressor wheel;

wherein the third concave region has a radial extent of approx. 30% of a radius of the compressor wheel; and

wherein the fourth convex region has a radial extent of approx. 20% of a radius of the compressor wheel.

9. The exhaust gas turbocharger according to claim 8 , wherein the plurality of regions adjoin one another such that the second convex region adjoins the first concave region, the third concave region adjoins the second convex region, and the fourth convex region adjoins the third concave region.

10. The exhaust gas turbocharger according to claim 8 , wherein the fourth convex region includes a bulge that has an axial height of approx. 0.15 mm.

11. The exhaust gas turbocharger according to claim 8 , wherein the hub extends from an axis of rotation to the first concave region.

12. The exhaust gas turbocharger according to claim 11 , wherein the hub has a flat axial end surface.

13. The exhaust gas turbocharger according to claim 12 , wherein the flat axial end surface has a radial extent of approx. 15% of the radius of the compressor wheel.

14. The exhaust gas turbocharger according to claim 8 , wherein the first concave region has the radial extent of approx. 7% of the radius of the compressor wheel.

15. The exhaust gas turbocharger according to claim 8 , wherein the second convex region has the radial extent of approx. 25% of the radius of the compressor wheel.

16. The exhaust gas turbocharger according to claim 8 , wherein the third concave region has the radial extent of approx. 30% of the radius of the compressor wheel.

17. The exhaust gas turbocharger according to claim 8 , wherein the fourth convex region has the radial extent of approx. 20% of the radius of the compressor wheel.

18. The exhaust gas turbocharger according to claim 8 , wherein the first concave region has the radial extent of approx. 7% of the radius of the compressor wheel, the second convex region has the radial extent of approx. 25% of the radius of the compressor wheel, the third concave region has the radial extent of approx. 30% of the radius of the compressor wheel, and the fourth convex region has the radial extent of approx. 20% of the radius of the compressor wheel.

19. A compressor wheel for a charging device, comprising:

a hub, a plurality of blades, and a wheel back;

the wheel back having an undulating profile extending from the hub in a radial direction, the undulating profile including a plurality of regions that emerge from the hub in the radial direction and adjoin one another, and wherein the plurality of regions of the undulating profile include:

a first concave region;

a second convex region adjoining the first concave region;

a third concave region adjoining the second convex region; and

a fourth convex region adjoining the third concave region, wherein the fourth convex region includes a bulge that has an axial height of approx. 0.15 mm.

20. The compressor wheel according to claim 19 , wherein at least one of:

the first concave region has a radial extent of approx. 7% of a radius of the compressor wheel;

the second convex region has a radial extent of approx. 25% of a radius of the compressor wheel;

the third concave region has a radial extent of approx. 30% of a radius of the compressor wheel; and

the fourth convex region has a radial extent of approx. 20% of a radius of the compressor wheel.

Assignments (2)
CHANGE OF NAME Recorded Jan 22, 2019
From: BOSCH MAHLE TURBO SYSTEMS GMBH & CO. KG
To: BMTS TECHNOLOGY GMBH & CO. KG
Reel/Frame 048108/0265 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 19, 2018
From: PHAM, KINH T.
To: BOSCH MAHLE TURBO SYSTEMS GMBH & CO. KG
Reel/Frame 047872/0810 →
Priority Claims (1)
DE 10 2015 214864 · Aug 4, 2015 · national
Continuity (1)
Related Publication 20170037864A1 · Feb 9, 2017
Cited By (2)
US 12,392,347 US 12,584,492