IP Library Granted Patent US 10,487,726
Granted Patent B2
US 10,487,726 · App. 15/437,417 · Granted Nov 26, 2019

Turbocharger assembly

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Quick Facts
Patent No.
US 10,487,726
App. No.
15/437,417
Granted
Nov 26, 2019
Kind
B2
Abstract

A turbocharger can include a center housing; a compressor assembly operatively coupled to the center housing; and a turbine assembly operatively coupled to the center housing, where the center housing includes a bearing boss that includes a bore wall with opposing axial ends that define an axial through bore having opposing axial openings, an oil inlet, an oil outlet, an arcuate oil passage in fluid communication with the oil inlet, an oil passage in fluid communication with the arcuate oil passage and an opening in the bore wall, and an oil drainage passage in fluid communication with the opposing axial openings of the through bore and in fluid communication with the oil outlet.

Claims (55)

1. A turbocharger comprising:

an oil cooled center housing;

a compressor assembly operatively coupled to the oil cooled center housing; and

a turbine assembly operatively coupled to the oil cooled center housing,

wherein the oil cooled center housing comprises

a bearing boss that comprises a bore wall with opposing axial ends that define an axial through bore having a through bore axis and opposing axial openings wherein the opposing axial ends define an axial length of the axial through bore,

an oil inlet,

an oil outlet,

an arcuate oil passage in fluid communication with the oil inlet wherein the arcuate oil passage comprises a maximum axial length that, measured parallel to the through bore axis, is 50 percent to 150 percent of the axial length of the axial through bore,

an oil passage in fluid communication with the arcuate oil passage and an opening in the bore wall, and

an oil drainage passage in fluid communication with the opposing axial openings of the axial through bore and in fluid communication with the oil outlet.

2. The turbocharger of claim 1 wherein the bearing boss comprises a pin bore.

3. The turbocharger of claim 1 wherein the bearing boss comprises an oil bypass passage that is in fluid communication with an opening-of the bore wall and in fluid communication with the oil drainage passage.

4. The turbocharger of claim 3 comprising an orifice that regulates oil flow from the oil bypass passage to the oil drainage passage, wherein the orifice provides a desired amount of resistance to the oil flow.

5. The turbocharger of claim 1 wherein the bearing boss comprises a pin bore that comprises a pin bore axis that, upon extension thereof, passes through the oil inlet.

6. The turbocharger of claim 1 wherein the bearing boss comprises an oil bypass passage that is in fluid communication with an opening of the bore wall and in fluid communication with the oil drainage passage, wherein the oil bypass passage comprises a passage axis that, upon extension thereof, passes through the oil outlet.

7. The turbocharger of claim 1 wherein the arcuate oil passage- spans an arc angle of 180 degrees about the axis of the axial through bore.

8. The turbocharger of claim 1 wherein the arcuate oil passage-is defined in part by a first wall of the oil cooled center housing that comprises a first radius and a second wall of the center housing that comprises a second, larger radius.

9. The turbocharger of claim 1 wherein the arcuate oil passage comprises a semi-annular cross-sectional shape.

10. The turbocharger of claim 1 wherein the oil cooled center housing is oriented with respect to gravity according to a predetermined orientation or range of orientations.

11. The turbocharger of claim 10 wherein the range of orientations comprises plus 25 degrees to minus 25 degrees as to an axis of the oil outlet and the direction of the acceleration of gravity.

12. The turbocharger of claim 1 wherein the arcuate oil passage comprises an arc angle that is greater than 45 degrees about an axis of the axial through bore.

13. The turbocharger of claim 1 wherein the arcuate oil passage comprises an arc angle that is less than or equal to 360 degrees about an axis of the axial through bore.

14. The turbocharger of claim 1 comprising a bypass passage that comprises an opening in fluid communication with the arcuate oil passage and an opening in fluid communication with the oil drainage passage.

15. The turbocharger of claim 1 wherein the bore wall comprises grooves.

16. The turbocharger of claim 1 , wherein the oil cooled center housing does not include one or more water passages and corresponding water inlet and outlet openings.

17. A method comprising:

in a center housing that comprises a bearing boss that comprises a bore wall with opposing axial ends that define an axial through bore having opposing axial openings, an oil inlet, an oil outlet, an arcuate oil passage in fluid communication with the oil inlet, an oil passage in fluid communication with the arcuate oil passage and an opening in the bore wall, and an oil drainage passage in fluid communication with the opposing axial openings of the axial through bore and in fluid communication with the oil outlet, flowing oil to the oil inlet;

receiving at least a portion of the flowing oil in the oil drainage passage from the opposing axial openings of the axial through bore;

receiving another portion of the flowing oil in the oil drainage passage via an oil bypass passage disposed in the bearing boss; and

flowing oil from the oil drainage passage to the oil outlet.

18. A turbocharger comprising:

a center housing;

a compressor assembly operatively coupled to the center housing; and

a turbine assembly operatively coupled to the center housing,

wherein the center housing comprises

a bearing boss that comprises a bore wall with opposing axial ends that define an axial through bore having opposing axial openings,

an oil inlet,

an oil outlet,

an arcuate oil passage in fluid communication with the oil inlet,

an oil passage in fluid communication with the arcuate oil passage and an opening in the bore wall, and

an oil drainage passage in fluid communication with the opposing axial openings of the axial through bore and in fluid communication with the oil outlet, and

wherein the bearing boss comprises an oil bypass passage that is in fluid communication with an opening of the bore wall and in fluid communication with the oil drainage passage.

19. A turbocharger comprising:

a center housing;

a compressor assembly operatively coupled to the center housing; and

a turbine assembly operatively coupled to the center housing,

wherein the center housing comprises

a bearing boss that comprises a bore wall with opposing axial ends that define an axial through bore having opposing axial openings,

an oil inlet,

an oil outlet,

an arcuate oil passage in fluid communication with the oil inlet,

an oil passage in fluid communication with the arcuate oil passage and an opening in the bore wall, and

an oil drainage passage in fluid communication with the opposing axial openings of the axial through bore and in fluid communication with the oil outlet, and

wherein the bearing boss comprises a pin bore that comprises a pin bore axis that, upon extension thereof, passes through the oil inlet.

Assignments (9)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE TYPOS IN THE APPLICATION NUMBER PREVIOUSLY RECORDED AT REEL: 056111 FRAME: 0583. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Feb 25, 2022
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 059250/0792 →
SECURITY AGREEMENT Recorded May 3, 2021
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 056111/0583 →
RELEASE OF SECURITY INTEREST Recorded Apr 30, 2021
From: WILMINGTON SAVINGS FUND SOCIETY, FSB
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 056427/0298 →
ASSIGNMENT AND ASSUMPTION OF SECURITY INTEREST IN PATENTS Recorded Jan 15, 2021
From: JPMORGAN CHASE BANK, N.A., AS RESIGNING ADMINISTRATIVE AND COLLATERAL AGENT
To: WILMINGTON SAVINGS FUND SOCIETY, FSB, AS SUCCESSOR ADMINISTRATIVE AND COLLATERAL AGENT
Reel/Frame 055008/0263 →
SECURITY INTEREST Recorded Oct 1, 2018
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047172/0220 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE NAME AND EXECUTION DATE PREVIOUSLY RECORDED AT REEL: 046103 FRAME: 0144. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Sep 21, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 047119/0864 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 6, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 047024/0127 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 21, 2017
From: ZHANG, RONG
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 041313/0564 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 20, 2017
From: WOOD, DANIEL; FENG, JIAN; SHEN, JIAN; TAN, QIQI
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 041303/0958 →