IP Library Granted Patent US 11,486,268
Granted Patent B2
US 11,486,268 · App. 15/871,677 · Granted Nov 1, 2022

Turbocharger assembly

Inventors: Sachinkumar Babu Naik (Bengaluru, IN); Shankar Pandurangasa Solanki (Bengaluru, IN); Saneel Rajan Gandhi (Pune, IN); Joel Castan (Chantraine, FR)
Assignee: Garrett Transportation I Inc.
F01D25/162F01D25/166F01D25/24F02C6/12F02C7/06F16C35/06F02B37/00F05D2220/40F05D2230/64F05D2240/60F05D2260/30F05D2260/37F16C2360/24
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,486,268
App. No.
15/871,677
Granted
Nov 1, 2022
Kind
B2
Abstract

A turbocharger includes a center housing that includes a through bore and a stepped locating pin socket that includes a stop surface; a bearing disposed in the through bore where the bearing includes an opening; and a stepped locating pin where the stepped locating pin includes a pin portion received in part by the opening of the bearing and a seating portion secured via an interference fit in the stepped locating pin socket where a maximum radius of the seating portion exceeds a maximum radius of the pin portion and where the stepped locating pin includes a stop surface that contacts the stop surface of the stepped locating pin socket to axially position the stepped locating pin in the stepped locating pin socket.

Claims (23)

1. A turbocharger comprising:

a center housing that comprises a through bore and a stepped locating pin socket that comprises a pin socket axis, a through bore opening, a stepped locating pin opening and an annular stop surface disposed at a step between a pin portion and a seating portion of the stepped locating pin socket, wherein the pin portion and the seating portion define a first axial distance (z 4 +z 5 ) along the pin socket axis from the through bore opening to an end of the seating portion, and wherein the through bore opening and the stepped locating pin opening define a second axial distance (z 7 ) along the pin socket axis from the through bore opening to the stepped locating pin opening that is greater than the first axial distance;

a bearing disposed in the through bore wherein the bearing comprises an opening; and

a stepped locating pin wherein the stepped locating pin comprises a stepped locating pin axis, a pin portion received in part by the opening of the bearing, a seating portion, and a transition region between the pin portion and the seating portion with a minimum radius of the stepped locating pin, wherein a maximum radius of the seating portion of the stepped locating pin socket exceeds a maximum radius of the pin portion of the stepped locating pin socket, wherein the stepped locating pin comprises a stop surface adjacent to the transition region that contacts the annular stop surface of the stepped locating pin socket to axially position the stepped locating pin in the stepped locating pin socket, and wherein the pin portion and the transition region of the stepped locating pin comprise an axial length (z 12 +z 13 ) along the stepped locating pin axis between an end of the stepped locating pin and the seating portion of the stepped locating pin that is greater than the first axial distance (z 4 +z 5 ) and less than the second axial distance (z 7 ) to locate the stepped locating pin in the opening of the bearing prior to the formation of an interference fit between a cylindrical surface of the seating portion of the stepped locating pin and a cylindrical surface of the seating portion of the stepped locating pin socket.

2. The turbocharger of claim 1 wherein the stepped locating pin is threadless.

3. The turbocharger of claim 1 wherein the stepped locating pin comprises an end recess.

4. The turbocharger of claim 1 wherein the housing comprises a lubricant passage and wherein the bearing comprises another opening that is accessible via the lubricant passage.

5. The turbocharger of claim 1 wherein an axial length of the seating portion of the stepped locating pin is less than the axial length of the pin portion and the transition region of the stepped locating pin.

6. The turbocharger of claim 1 wherein the stepped locating pin comprises a maximum diameter that exceeds the second axial distance of the stepped locating pin socket of the housing.

7. The turbocharger of claim 1 wherein the seating portion of the stepped locating pin is recessed in the stepped locating pin socket.

8. The turbocharger of claim 1 wherein the stepped locating pin socket comprises a threaded portion and wherein the seating portion of the stepped locating pin socket is threadless.

9. The turbocharger of claim 1 wherein the stepped locating pin socket comprises a threaded portion and wherein the stepped locating pin is seated in the seating portion of the stepped locating pin socket.

10. The turbocharger of claim 9 comprising a component wherein the component comprises a threaded extension that comprises threads received at least in part in the threaded portion of the stepped locating pin socket.

11. The turbocharger of claim 1 wherein the stepped locating pin is scar-less.

12. The turbocharger of claim 1 wherein the seating portion of the stepped locating pin comprises a diameter less than 12 mm.

13. The turbocharger of claim 1 wherein the stepped locating pin, as secured via the interference fit in the stepped locating pin socket, comprises an interference fit length in a range of 1 mm to 4 mm.

14. A method comprising:

providing a turbocharger center housing that comprises a through bore and a stepped locating pin socket that comprises a stop surface, a bearing disposed in the through bore wherein the bearing comprises an opening, and a stepped locating pin wherein the stepped locating pin comprises a pin portion, a seating portion, and a transition region between the pin portion and the seating portion with a minimum radius of the stepped locating pin, wherein a maximum radius of the pin portion is less than a maximum radius of the seating portion and wherein the stepped locating pin comprises a stop surface;

positioning the stepped locating pin partially in the stepped locating pin socket;

locating the pin portion of the stepped locating pin in the opening of the bearing without utilizing an interference fit or threads; and

interference fitting a cylindrical surface of the seating portion of the stepped locating pin against a cylindrical surface in the stepped locating pin socket wherein the stop surface of the stepped locating pin contacts the stop surface of the stepped locating pin socket to axially position the stepped locating pin in the stepped locating pin socket.

15. The method of claim 14 wherein the interference fitting comprises thermal processing and wherein the stepped locating pin comprises a scar-less stepped locating pin.

16. A turbocharger comprising: a center housing that comprises a through bore and a stepped locating pin socket that comprises a through bore opening, a stepped locating pin opening, a step from a smaller diameter pin portion to a larger diameter threadless seating portion and a threaded portion between the threadless seating portion and the stepped locating pin opening, wherein the step forms a stop surface defined by a smaller inner diameter and a larger outer diameter of the stepped locating pin socket; a bearing disposed in the through bore wherein the bearing comprises an opening; and a stepped locating pin, wherein the stepped locating pin comprises a step from a smaller diameter pin portion, received in part in the pin portion of the stepped locating pin socket and in part by the opening of the bearing, to a larger diameter seating portion, secured via an interference fit between a cylindrical surface of the seating portion of the stepped locating pin and a cylindrical surface in the seating portion of the stepped locating pin socket, wherein the step of the stepped locating pin forms a stop surface that contacts the stop surface of the stepped locating pin socket to axially position the stepped locating pin in the stepped locating pin socket.

Assignments (8)
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 NATURE OF CONVEYANCE FROM CHANGE OF NAME TO ASSIGNMENT AND "1" TO "I" IN ASSIGNEE NAME PREVIOUSLY RECORDED AT REEL: 046103 FRAME: 0590. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Aug 30, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 046867/0656 →
CHANGE OF NAME Recorded Jun 15, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORTATION 1 INC.
Reel/Frame 046103/0590 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2018
From: NAIK, SACHINKUMAR BABU; SOLANKI, SHANKAR PANDURANGASA; GANDHI, SANEEL RAJAN; CASTAN, JOEL
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 044623/0262 →
Continuity (1)
Related Publication 20190218934A1 · Jul 18, 2019