IP Library Granted Patent US 8,157,267
Granted Patent B2
US 8,157,267 · App. 11/662,829 · Granted Apr 17, 2012

Free-floating gas seal

Assignee: Textron Innovations Inc.
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Quick Facts
Patent No.
US 8,157,267
App. No.
11/662,829
Granted
Apr 17, 2012
Kind
B2
Abstract

A seal system is adapted for use in gas flow systems. The seal system has two seal faces and a longitudinally compressible seal spring-biased between the seal faces. The seal has a bellows configuration and opposite ends in sealing contact with the seal faces, such that at least one end of the seal is free to move relative to the corresponding seal face while maintaining the sealing contact. The seal system is particularly suited for use in sealing an engine to an exhaust member.

Claims (18)

1. A seal system for sealing an engine to an exhaust member, the seal system comprising:

a stationary ring member operably associated with the engine, the ring having:

a first seal face; and

an inner circumferential surface configured to channel a flow of engine exhaust;

an aft seal ring having:

a liner in gaseous communication with the stationary ring, the liner being configured to redirect flow direction of the flow of engine exhaust, the liner having:

a second seal face, the second seal face being spaced from and opposing the first seal face, the second seal face being configured to move in the longitudinal, transverse, and tilting directions relative to the first seal face in response to a force exerted against the liner by the flow of engine exhaust;

a spring-biased bellows disposed between the first and second seal faces, the bellows being longitudinally compressible and having opposing ends in sealing contact with each corresponding seal face;

a flow-directing means attached to the stationary ring member and configured to extend in a direction relatively parallel the inner surface of the stationary ring member for directing the flow of engine exhaust away from the bellow;

a first stop located on the first seal face; and

a second stop located on the second seal face;

wherein the first stop and the second stop prevent transverse movement of the bellow relative to the respective first seal face and the second seal face; and

wherein each end of the bellows slidingly engages the corresponding seal face so as to allow longitudinal and transverse movement of the seal faces relative to each other.

2. The seal system according to claim 1 , wherein the at least one end of the seal is formed as a face seal for sealing against the corresponding seal face.

3. The seal system according to claim 1 , wherein the bellows is at least partially formed from a metallic material.

4. The seal system according to claim 1 , wherein at least one of the two seal faces is at least partially coated with a wear resistant and heat resistant coating.

5. The seal system according to claim 1 , wherein at least one of the two seal faces is at least partially coated with a heat resistant material coating.

6. The seal system according to claim 1 , wherein at least one of the two seal faces is at least partially coated with a chromium carbide coating.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2009
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 022182/0461 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 3, 2007
From: MAST, THOMAS M.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 019105/0111 →
Continuity (1)
Related Publication 20070257442A1 · Nov 8, 2007