Shaft seal system and a compressor having a corresponding shaft seal system

Patent metadata

Field	Value
Publication number	US-10030585-B2
Application number	US-201514843607-A
Country	US
Kind code	B2
Filing date	Sep 2, 2015
Priority date	Sep 3, 2014
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

A shaft seal system which is disposed axially between a first chamber and a second chamber is disclosed. The shaft seal system includes a shaft, a casing that surrounds the shaft, and a seal which is disposed axially closer to the second chamber where the first chamber has a fluid and the second chamber is to be protected from the fluid. In this arrangement, the seal includes a pressure booster.

First claim

What is claimed is:

1. A shaft seal system which is disposed axially between a first chamber and a second chamber, comprising:
a shaft;
a casing that surrounds the shaft; and
a seal, wherein the seal is disposed axially closer to the second chamber than the first chamber;
wherein the first chamber includes a fluid;
wherein the seal includes a mechanical pressure booster, wherein the mechanical pressure booster is shaped such that a pressure of a sealing gas flowing at the seal and in a direction of the first chamber is increased by the mechanical pressure booster, wherein the sealing gas is flowable from the second chamber to the first chamber along the shaft, and wherein the sealing gas is provided from a compressor;
wherein the mechanical pressure booster comprises a first pressure booster and a second pressure booster and wherein the first pressure booster comprises a helical groove on the casing and the second pressure booster comprises a radially opposite series of spaced apart longitudinal indentations on the shaft.

2. The shaft seal system according to claim 1 , wherein the indentations extend parallel to a rotational axis of the shaft.

3. The shaft seal system according to claim 1 , wherein the indentations extend at an angle to a rotational axis of the shaft.

4. The shaft seal system according to claim 1 , further comprising a second seal, wherein the second seal is disposed axially closer to the first chamber than the second chamber or is disposed radially between the shaft and the casing.

5. The shaft seal system according to claim 4 , wherein an annular space is disposed axially between the seal and the second seal and is disposed radially between the shaft and the casing.

6. The shaft seal system according to claim 4 , wherein a shoulder is disposed on an inside of the casing between the seal and the second seal and is disposed radially between the shaft and the casing.

7. The shaft seal system according to claim 4 , wherein the second seal includes a sealing fin on an outer surface of the shaft or a lining on an inside of the casing.

8. An engine compressor comprising a shaft seal system according to claim 1 .

Assignees

• MTU Aero Engines AG

Inventors

• Flouros Michael
• Scharl Richard
• Cottier Francois

Classifications

• F04D19/02

  Multi-stage pumps · CPC title

• F16J15/406

  by at least one pump · CPC title

• F01D11/02

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F16J15/164 Primary

  the sealing action depending on movements; pressure difference, temperature or presence of leaking fluid · CPC title