IP Library Granted Patent US 10,473,114
Granted Patent B2
US 10,473,114 · App. 15/570,356 · Granted Nov 12, 2019

Compressor assembly for a turbocharger

Inventors: Daniel Rusch (Wettingen, CH); Gerd Mundinger (Wettingen, CH)
Assignee: ABB Turbo Systems AG
F04D29/441F02B37/10F04D17/10F04D27/0238F04D29/4206F02C6/12F05B2220/40F05D2220/40F05D2250/52Y02T10/144
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 10,473,114
App. No.
15/570,356
Granted
Nov 12, 2019
Kind
B2
Abstract

The present invention relates to a compressor assembly for a turbocharger. The compressor assembly may comprise a spiral housing with a flow channel which is designed to convey a fluid which can be sucked up from outside the compressor assembly, a compressor outlet flange which is fluidically connected to the spiral housing via the flow channel, and an injection device designed to introduce a fluid from outside the compressor assembly into the flow channel, wherein the injection device is arranged outside the flow channel of the spiral housing.

Claims (25)

1. A turbocharger for an internal combustion engine, the turbocharger comprising a compressor assembly, the compressor assembly comprising:

a spiral housing having a flow channel defined therein, the flow channel designed to convey a first fluid which can be sucked up from outside the compressor assembly and to feed said first fluid to a compressor outlet, wherein the spiral housing comprises a conical diffuser,

a compressor outlet flange arranged on the spiral housing adjacent to the conical diffuser, and

an air injection device for improving the load response behavior of the internal combustion engine, wherein the injection device is configured to introduce air from outside the spiral housing into the flow channel, wherein the air injection device is arranged outside the flow channel of the spiral housing, and wherein the air injection device is arranged to inject the air into the conical diffuser.

2. The turbocharger as claimed in claim 1 , wherein the air injection device is at least partially incorporated into the spiral housing, and wherein the injection device comprises at least one opening to the flow channel so that the air can be introduced from outside the compressor assembly into the flow channel by the injection device.

3. The turbocharger as claimed in claim 1 , wherein the injection device comprises an air channel.

4. The turbocharger as claimed in claim 1 , wherein the injection device is attached to an outer wall of the spiral housing so that the air can be introduced from outside the compressor assembly via the injection device into the flow channel through an opening in the spiral housing.

5. The turbocharger as claimed in claim 4 , wherein the outer wall of the spiral housing, to which the injection device is attached, forms part of an outer wall of the conical diffuser.

6. The turbocharger as claimed in claim 1 , wherein the compressor outlet flange at least partially comprises the injection device so that the air can be introduced from outside the compressor assembly by the injection device into the flow channel of the spiral housing.

7. The turbocharger as claimed in claim 6 , wherein the injection device comprises an air channel in the compressor outlet flange, wherein the air channel comprises a first opening and a second opening, wherein the air can be introduced from outside the compressor assembly into the air channel via the first opening of the air channel, and wherein the second opening of the air channel fluidically connects the air channel to the flow channel of the spiral housing so that the air can be introduced into the flow channel.

8. The turbocharger as claimed in claim 7 , wherein a portion of the air channel is formed by a connection piece which is connectable to the compressor outlet flange.

9. The turbocharger as claimed in claim 7 , wherein the air injection device has a reservoir for storing the air and for the uniform distribution of the air over the circumference of the flow channel, wherein the reservoir comprises part of the air channel.

10. The turbocharger as claimed in claim 1 , wherein the air injection device comprises a connection element arranged to introduce the air from outside the compressor assembly into the injection device via an injection element which is insertable into the connection element.

11. The turbocharger as claimed in claim 10 , wherein the injection device is of nozzle-shaped design.

12. The turbocharger as claimed in claim 8 , wherein the air injection device has a reservoir for storing the air and for the uniform distribution of the air over the circumference of the flow channel, wherein the reservoir comprises part of the air channel.

13. The turbocharger as claimed in claim 10 , wherein the connection element is disposed at least partially within the housing.

14. A turbocharger for load responsiveness, the turbocharger comprising:

a housing defining a flow channel for conveying a first fluid,

a diffuser through which the flow channel passes,

an outlet flange forming part of the housing at an end of the flow channel, and

an air injection communication port arranged to introduce injection air as a second fluid into the flow channel within the diffuser, wherein the air injection communication port extends through a portion of the housing in communication with the flow channel within the diffuser, wherein the air injection communication port is arranged opened to outside of the turbocharger housing for receiving injection air from outside the housing.

15. The turbocharger as recited in claim 14 , wherein the air injection communication port extends through an outer wall of an outlet flange of the housing, the outer wall being thicker than another outer wall of the housing defining a spiral portion of the flow channel.

16. A method of operation of a compressor assembly of a turbocharger for load responsiveness, the method comprising:

drawing a first fluid within a flow channel of a housing and into a diffuser through which the flow channel passes to an outlet flange forming part of the housing at an end of the flow channel, and

injecting injection air through an air injection communication port arranged to introduce injection air as a second fluid into the flow channel within the diffuser, wherein the air injection communication port extends through a portion of the housing in communication with the flow channel within the diffuser for providing injection air from outside the housing.

Assignments (6)
CHANGE OF NAME Recorded Mar 3, 2025
From: TURBO SYSTEMS SWITZERLAND LTD.
To: ACCELLERON SWITZERLAND LTD.
Reel/Frame 070378/0198 →
CHANGE OF NAME Recorded Sep 26, 2022
From: ABB SCHWEIZ AG
To: ABB SWITZERLAND LTD
Reel/Frame 061219/0175 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 26, 2022
From: ABB SWITZERLAND LTD
To: TURBO SYSTEMS SWITZERLAND LTD
Reel/Frame 061541/0473 →
MERGER Recorded Aug 21, 2020
From: ABB TURBO SYSTEMS AG
To: ABB TURBO SYSTEMS HOLDING AG
Reel/Frame 053574/0340 →
MERGER Recorded Aug 21, 2020
From: ABB TURBO SYSTEMS HOLDING AG
To: ABB SCHWEIZ AG
Reel/Frame 053575/0854 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 9, 2017
From: RUSCH, DANIEL; MUNDINGER, GERD
To: ABB TURBO SYSTEMS, AG
Reel/Frame 044077/0881 →
Priority Claims (1)
DE 10 2015 106 596 · Apr 29, 2015 · national
Continuity (1)
Related Publication 20180142699A1 · May 24, 2018