Sealing system for flanged joint

US9388743B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9388743-B2
Application numberUS-201213718035-A
CountryUS
Kind codeB2
Filing dateDec 18, 2012
Priority dateDec 18, 2012
Publication dateJul 12, 2016
Grant dateJul 12, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A sealing system is provided for a flanged joint. The sealing system includes a split seal and a spring. The split seal includes a radial outer surface, an axial outer surface, and a chamfered surface inclined with respect to the radial outer surface and the axial outer surface. The spring is disposed in urging contact with the chamfered surface and configured to apply an axial force, and a radial force on the axial outer surface, and the radial outer surface respectively.

First claim

Opening claim text (preview).

I claim: 1. A sealing system for a flanged joint, the sealing system including: a split seal including: a radial outer surface; an axial outer surface; and a chamfered surface inclined with respect to the radial outer surface and the axial outer surface; and a spring disposed in urging contact with the chamfered surface and configured to apply an axial force, and a radial force on the axial outer surface, and the radial outer surface respectively; and wherein the flanged joint includes: a first flange; and a second flange releasably connected to the first flange, wherein the first and second flange together define a seal pocket including a forward surface, an aft surface, and a circumferential surface; wherein the spring of the sealing system acts between the chamfered surface and a forward surface of the seal pocket; wherein the forward and aft surfaces are forward and aft relative to the engine; and wherein the sealing system is housed in the seal pocket. 2. The sealing system of claim 1 , wherein the split seal is of a polygonal cross section. 3. The sealing system of claim 1 , wherein the spring is of a round cross section. 4. The sealing system of claim 1 , wherein the spring is one of a helical spring, a marcel expander, and a wavy spring. 5. The sealing system of claim 1 , wherein the split seal is configured to restrict a passage of fluid into and out of the flanged joint. 6. The flanged joint of claim 1 , wherein the radial outer surface of the seal is urged against a circumferential surface of the seal pocket and the axial outer surface of the seal is urged against an aft surface of the seal pocket. 7. A gas turbine engine comprising: a compressor system including a first flange; a combustor system including a second flange releasably connected to the first flange; and a sealing system disposed adjacent to the first and second flange, the sealing system including: a split seal including: a radial outer surface abutting the first flange; an axial outer surface abutting the second flange; and a chamfered surface inclined with respect to the radial outer surface and the axial outer surface; and a spring disposed in urging contact with the chamfered surface and configured to apply an axial force, and a radial force on the axial outer surface, and the radial outer surface respectively. 8. The gas turbine engine of claim 7 , wherein the first and second flange together define a seal pocket including a forward surface, an aft surface, and a circumferential surface. 9. The gas turbine engine of claim 8 , wherein the sealing system is housed in the seal pocket. 10. The gas turbine engine of claim 9 , wherein the radial outer surface of the seal is urged against a circumferential surface of the seal pocket and the axial outer surface of the seal is urged against an aft surface of the seal pocket. 11. The gas turbine engine of claim 9 , wherein the spring of the sealing system acts between the chamfered surface and a forward surface of the seal pocket. 12. The gas turbine engine of claim 8 , wherein forward and aft is relative to the gas turbine engine. 13. The gas turbine engine of claim 8 , wherein the spring of the sealing system acts between the chamfered surface and the forward surface of the seal pocket. 14. A gas turbine engine comprising: a sealing system for a flanged joint, the sealing system including: a split seal including having a radial outer surface, an axial outer surface, and a chamfered surface inclined with respect to the radial outer surface and the axial outer surface; and a spring disposed in urging contact with the chamfered surface and configured to apply an axial force, and a radial force on the axial outer surface, and the radial outer surface respectively.

Assignees

Inventors

Classifications

  • Cross-Sectional Technologies · mapped topic

  • F02C7/28Primary

    Arrangement of seals · CPC title

  • Coupler sealing means · CPC title

Patent family

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Frequently asked questions

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What does patent US9388743B2 cover?
A sealing system is provided for a flanged joint. The sealing system includes a split seal and a spring. The split seal includes a radial outer surface, an axial outer surface, and a chamfered surface inclined with respect to the radial outer surface and the axial outer surface. The spring is disposed in urging contact with the chamfered surface and configured to apply an axial force, and a rad…
Who is the assignee on this patent?
Solar Turbines Inc, Solar Turbines Inc
What technology area does this patent fall under?
Primary CPC classification F02C7/28. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jul 12 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).