Pressure-energized sealing rings

5630593
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Inventors

Swensen, Jeffrey E.
Barrett, Robert A.

Application #

302467

Filed

Sep-12-1994

Published

May-20-1997

Current US Class

277/626
277/627
277/647
277/650

International Classes

F16J 015/00

Field of Search

277/206

Assignee

EG&G Pressure Science, Inc. (Beltsville, MD)

Examiners

DePumpo; Daniel G.

Attorney, Agent or Firm

Roylance, Abrams, Berdo & Goodman, L.L.P.

US Patent References

4067585   Deformable metalli...
4121843   Multiple convolutio...
4218067   Multi-ply sealing ri...
4361335   Annular gasket for...
4477086   Seal ring with slida...
4589666   Slip joint assembly...
4602795   Thermally expansi...
4602888   Flexible metallic jo...
4759555   Split ring seal with...
4784397   Hollow metallic sea...
5249814   Multi-ply sealing ri...

Referenced by:

View Backward References

Other References

Nicholson's Aircraft Seal Ltd.--Catalog for Corruplus Gaskets-Issue VI.; May 1985.

Citation

Cite This Patent

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Abstract
A pressure-energized sealing ring having a bight portion, a first leg portion and a second leg portion for providing a fluid-tight seal between a pair of components. The first and second leg portions include a curved section having first and second sealing surfaces. The sealing surfaces are spaced from the free ends of the leg portion. The free ends of the leg portions are positioned between the bight portion and the sealing surfaces so that the ends of the seal are located in the area of low pressure. Accordingly, when sealing ring is a multi-ply seal, the free ends of the seal are positioned in the low pressure area so that the high pressure does not separate the seal. The curved sections of the leg portions and the curve of the bight portion securely couple the plies together without welding. Preferably, the plies are connected together and in intimate contact at their interfaces therebetween. In some embodiments, the leg portions include planar or crowned sections so that the sealing surfaces are faced farther from the bight portions to lower the contact force and stress level in the bight portion. In other embodiments, the bight portion has at least one convolution. Still in other embodiments, the sealing ring is arranged for an externally pressurized-type application.
 
Claims
What is claimed is:

1. A pressure-energized sealing ring in its unstressed state, comprising:

an annular bight portion having at least one curved section extending through an arc with a first substantially smooth concave surface adapted to be in fluid contact with a first high pressure fluid and a second convex surface adapted to be fluid contact with a second low pressure fluid of a lower pressure than the first fluid;

a first annular leg portion extending from one end of said bight portion to a first free end thereof, and having a first substantially smooth surface extending coextensively from said first surface of said bight portion to said first free end of said first leg portion, and a second surface extending from said second surface of said bight portion to said first free end of said first leg portion said first leg portion having a first substantially u-shaped bent section reversing direction of said first leg portion and a first annular sealing surface formed on said first surface of said first leg portion with said first free end of said first leg portion being in fluid contact with the second low pressure fluid; and



Description
FIELD OF THE INVENTION

The invention relates to fluid-tight sealing rings which are pressure-energized for confining fluid at high temperatures and pressures. More specifically, this invention relates to single ply and multi-ply sealing rings with improved sealing contact and lower localized stress.

BACKGROUND OF THE INVENTION

Resilient, metallic sealing rings are currently utilized in a wide variety of applications due to their ability to repeatedly accommodate large variations in lengths due to thermal expansions and contractions of assemblies surrounding them and/or engaging them in sealing contact. For example, in the hot sections of an aircraft gas turbine engine, a seal must be created between components that are at variable distances from one another, depending upon the sum of manufacturing tolerances on several components in the assembly and on relative thermal expansion during operation of the engine. The seal must be capable of conforming to out-of-flat flanges or surfaces to provide low leakage.