IP Library Granted Patent US 10,030,585
Granted Patent B2
US 10,030,585 · App. 14/843,607 · Granted Jul 24, 2018

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

Inventors: Michael Flouros (Munich, DE); Richard Scharl (Karlsfeld, DE); Francois Cottier (Unterschleissheim, DE)
Assignee: MTU Aero Engines AG
F02C7/28F01D11/02F01D11/04F04D19/02F04D29/102F16J15/164F16J15/406
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Quick Facts
Patent No.
US 10,030,585
App. No.
14/843,607
Granted
Jul 24, 2018
Kind
B2
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.

Claims (14)

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 .

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 2, 2015
From: FLOUROS, MICHAEL; COTTIER, FRANCOIS; SCHARL, RICHARD
To: MTU AERO ENGINES AG
Reel/Frame 037190/0208 →
Priority Claims (1)
DE 10 2014 217 647 · Sep 3, 2014 · national
Continuity (1)
Related Publication 20160061116A1 · Mar 3, 2016