Sealing arrangement for fuel cell compressor

Patent metadata

Field	Value
Publication number	US-9709068-B2
Application number	US-201414184122-A
Country	US
Kind code	B2
Filing date	Feb 19, 2014
Priority date	Feb 19, 2014
Publication date	Jul 18, 2017
Grant date	Jul 18, 2017

Abstract

A mechanism for differential pressure sealing for use in a compressor, such as for fuel cell applications, is described. In a dual-stage compressor, a low pressure side and/or a high pressure side of the dual-stage compressor may include a compressor wheel supported by a shaft that can rotate about an axis of the shaft. A seal carrier may be provided that rotates with the compressor wheel and includes a groove for receiving a sealing ring, which may be a split expansion ring. A static seal plate may be positioned around a periphery of a portion of the seal carrier, such that the sealing ring can seal against a contact surface of the static seal plate when received in the groove in order to create a pressure differential seal. The low pressure side may include one sealing ring, whereas the high pressure side may include two sealing rings positioned in series.

First claim

What is claimed is:

1. A dual-stage compressor for use with a fuel cell, said dual-stage compressor comprising:
a low pressure side comprising:
a low pressure compressor wheel supported by a shaft and configured to rotate about an axis of the shaft;
a low pressure seal carrier configured to rotate with the low pressure compressor wheel;
a static low pressure seal plate disposed around a periphery of a portion of the low pressure seal carrier; and
at least one low pressure sealing ring;

a high pressure side comprising:
a high pressure compressor wheel supported by the shaft and configured to rotate about the axis of the shaft;
a high pressure seal carrier configured to rotate with the high pressure compressor wheel;
a static high pressure seal plate disposed around a periphery of a portion of the high pressure seal carrier; and
at least one high pressure sealing ring,

wherein the low pressure seal carrier defines at least one seal groove configured to receive the low pressure sealing ring, the low pressure sealing ring being configured to seal against a contact surface of the static low pressure seal plate when received in the groove in order to create a pressure differential seal for the low pressure side,
wherein the high pressure seal carrier defines at least one seal groove configured to receive the high pressure sealing ring, the high pressure sealing ring being configured to seal against a contact surface of the static high pressure seal plate when received in the groove in order to create a pressure differential seal for the high pressure side,
wherein the static high pressure seal plate includes a stepped section on the contact surface thereof, wherein the stepped section is configured to limit axial travel of the high pressure sealing ring, and
wherein the high pressure side comprises an inner high pressure sealing ring and an outer high pressure sealing ring, wherein the high pressure seal carrier defines an inner seal groove configured to receive the inner high pressure sealing ring and an outer seal groove, spaced apart from the inner seal groove, configured to receive the outer high pressure sealing ring, and wherein the stepped section of the static high pressure seal plate is configured to abut the inner high pressure sealing ring so as to limit axial travel of the inner high pressure sealing ring in a direction towards the low pressure side.

2. The dual-stage compressor of claim 1 , wherein at least one of the low pressure sealing ring or the high pressure sealing ring comprises a split expansion ring.

3. The dual-stage compressor of claim 1 , wherein the low pressure seal carrier defines only one seal groove configured to receive a single low pressure sealing ring, and the high pressure seal carrier defines two seal grooves spaced apart from each other and each configured to receive a single high pressure sealing ring.

4. The dual-stage compressor of claim 1 , wherein the low pressure sealing ring and the high pressure sealing ring are constructed of a low friction metallic material.

5. The dual-stage compressor of claim 1 , wherein the at least one high pressure sealing ring has a diametral size that is different than a diametral size of the at least one low pressure sealing ring.

6. The dual-stage compressor of claim 5 , wherein the diametral size of the at least one high pressure sealing ring is smaller than the diametral size of the at least one low pressure sealing ring.

7. The dual-stage compressor of claim 1 , wherein the low pressure seal carrier and the high pressure seal carrier are constructed of non-magnetic materials.

8. The dual-stage compressor of claim 1 , wherein the static low pressure seal plate and the static high pressure seal plate are constructed of non-magnetic materials.

9. A compressor for use with a fuel cell, said compressor comprising:
a compressor wheel supported by a shaft and configured to rotate about an axis of the shaft;
a seal carrier configured to rotate with the compressor wheel, wherein the seal carrier defines at least one seal groove in a peripheral edge of the seal carrier;
a static seal plate disposed around a periphery of a portion of the seal carrier; and
at least one sealing ring configured to be received within the corresponding seal groove, such that the sealing ring seals against a contact surface of the static seal plate when received in the groove in order to create a pressure differential seal between a compressor side of the sealing ring and a shaft side of the sealing ring,
wherein the static seal plate includes a stepped section on the contact surface thereof, wherein the stepped section is configured to limit axial travel of the sealing ring, and
wherein the at least one sealing ring comprises an inner sealing ring and an outer sealing ring, wherein the seal carrier includes an inner seal groove configured to receive the inner sealing ring and an outer seal groove, spaced apart from the inner seal groove, configured to receive the outer sealing ring, and wherein the stepped section of the static seal plate is configured to abut the inner sealing ring so as to limit axial travel of the inner sealing ring.

10. The compressor of claim 9 , wherein the at least one sealing ring comprises a split expansion ring.

11. The compressor of claim 9 , wherein the seal carrier defines two seal grooves spaced apart from each other and each configured to receive a single sealing ring.

12. The compressor of claim 9 , wherein the sealing ring is constructed of a low friction metallic material.

13. The compressor of claim 9 , wherein the seal carrier is constructed of a non-magnetic material.

14. The compressor of claim 9 , wherein the static seal plate is constructed of a non-magnetic material.

Assignees

• Honeywell Int Inc

Inventors

• Thompson Glenn F
• Johnson Rick
• Mason John
• Guidry Mike
• Beresewicz Patrick

Classifications

• F04D19/02

  Multi-stage pumps · CPC title

• F04D29/164 Primary

  of an axial flow wheel · CPC title

• F04D29/102 Primary

  especially adapted for elastic fluid pumps · CPC title

• F04D17/125

  the casing being vertically split · CPC title

• F04D29/584

  cooling or heating the machine (F04D29/5846, F04D29/5853 take precedence) · CPC title