Finger-foil seals and gas turbine engines employing the same

US9506566B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9506566-B2
Application numberUS-201314061498-A
CountryUS
Kind codeB2
Filing dateOct 23, 2013
Priority dateOct 23, 2013
Publication dateNov 29, 2016
Grant dateNov 29, 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.

Embodiments of a gas turbine engine including a finger-foil seal are provided, as are embodiments of a finger-foil seal. In one embodiment, the finger-foil seal includes an aerodynamic foil having a generally annular body through which a first opening is formed. A finger seal retention structure is disposed around the aerodynamic foil. A finger seal backing spring is coupled to the finger seal retention structure and extends radially inward therefrom to contact an outer circumference of the aerodynamic foil. A first anti-rotation pin extends radially from the finger seal retention structure and into the first opening formed in the aerodynamic foil to inhibit rotation of the aerodynamic foil during operation of the finger-foil seal.

First claim

Opening claim text (preview).

What is claimed is: 1. A finger-foil seal, comprising: an aerodynamic foil having a generally annular body through which a first opening is formed; a finger seal retention structure disposed around the aerodynamic foil; a finger seal backing spring coupled to the finger seal retention structure and extending radially inward therefrom to contact an outer circumferential surface of the aerodynamic foil; and a first anti-rotation pin extending radially from the finger seal retention structure and into the first opening in the aerodynamic foil to inhibit rotation of the aerodynamic foil during operation of the finger-foil seal. 2. The finger-foil seal of claim 1 wherein the aerodynamic foil comprises a plurality of circumferentially-spaced openings formed through the generally annular body and including the first opening, and wherein the finger-foil seal further comprises a plurality of anti-rotation pins in which the first anti-rotation pin is included, the plurality of anti-rotation pins extending radially from the finger seal retention structure and into the plurality of circumferentially-spaced openings to inhibit rotation of the aerodynamic foil during operation of the finger-foil seal. 3. The finger-foil seal of claim 1 wherein an annular clearance is provided between the finger seal retention structure and the aerodynamic foil when the aerodynamic foil is in a non-expanded state, and wherein the first anti-rotation pin extends through the annular clearance and into the first opening. 4. The finger-foil seal of claim 1 wherein the finger seal retention structure comprises: a low pressure cover plate positioned over a first face of the finger seal backing spring; and a high pressure cover plate positioned over a second, opposing face of the finger seal backing spring. 5. The finger-foil seal of claim 4 wherein the anti-rotation pin is affixed to and extends radially inward from the low pressure cover plate, and wherein the low pressure cover plate further comprises an inner circumferential shoulder abutting an end of the aerodynamic foil to prevent axial dislodgement of the aerodynamic foil during operation of the finger-foil seal. 6. The finger-foil seal of claim 4 wherein the first anti-rotation pin is affixed to and extends radially inward from the high pressure cover plate. 7. The finger-foil seal of claim 6 wherein the first anti-rotation pin retains the aerodynamic foil in an axial direction to prevent axial dislodgement of the aerodynamic foil during operation of the finger-foil seal. 8. The finger-foil seal of claim 1 wherein the finger seal backing spring includes a first laminate, the first laminate comprising: an outer circumferential flange portion fixedly coupled to the finger seal retention structure; and a plurality of radially-resilient fingers extending radially inward from the outer circumferential flange portion to contact the aerodynamic foil. 9. The finger-foil seal of claim 8 wherein the finger seal backing spring further comprises: a second laminate disposed adjacent the first laminate and having a thickness greater than the first laminate; and a third laminate disposed between the first and second laminates having a thickness less than the second laminate. 10. The finger-foil seal of claim 1 wherein the radial stiffness of the plurality of radially-resilient fingers varies in a predetermined manner, as taken about the inner circumference of the finger seal backing spring. 11. The finger-foil seal of claim 10 wherein the plurality of radially-resilient fingers are divided into a plurality of finger groupings, each grouping comprising: a first finger having a first predetermined radial stiffness; and a second finger downstream of the first finger and having a second predetermined radial stiffness greater than the first predetermined radial stiffness. 12. The finger-foil seal of claim 11 wherein each of the plurality of finger groupings further comprises a third finger downstream of the second finger and having a third predetermined radial stiffness less than the second predetermined radial stiffness. 13. The finger-foil seal of claim 11 wherein the first finger has a length greater than the second finger. 14. The finger-foil seal of claim 1 wherein the finger seal backing spring comprises a plurality of laminates, and wherein the radial stiffness of the finger seal backing spring varies in a predetermined manner when moving axially through the finger seal backing spring from laminate to laminate. 15. The finger-foil seal of claim 14 wherein the finger-foil seal has a high pressure side and a low pressure side, and wherein the plurality of laminates comprise: a first laminate disposed adjacent the high pressure side of the finger-foil seal; a second laminate disposed adjacent the low pressure side of the finger-foil seal; and a third laminate disposed between the first and second laminates, the third laminate having a predetermined maximum radial stiffness greater than the radial stiffness of the first laminate and greater than the stiffness of the second laminate. 16. A finger-foil seal, comprising: an aerodynamic foil having a generally annular body through which a first opening is formed; a finger seal retention structure disposed around the aerodynamic foil; and a finger seal backing spring coupled to the finger seal retention structure and extending radially inward therefrom to contact an outer circumference of the aerodynamic foil, the finger seal backing spring comprising at least one laminate having a predetermined radial stiffness profile that varies as taken around the inner circumference of the at least one laminate; wherein the at least one laminate comprises a plurality of radially-resilient fingers contacting the aerodynamic foil, wherein the plurality of radially-resilient fingers is divided into multiple finger groupings, each finger grouping increasing in radial finger stiffness and then decreasing in radial finger stiffness when moving from finger to finger in a first direction around the inner circumference of the at least one laminate. 17. The finger-foil seal of claim 16 wherein the at least one laminate comprises: an outer circumferential flange portion fixedly coupled to the finger seal retention structure; and a plurality of slits formed in the at least one laminate and at least partially defining the plurality of radially-resilient fingers, the plurality of slits encroaching into the outer circumferential flange portion to varying extents to impart the plurality of radially-resilient fingers with different lengths and disparate radial stiffnesses. 18. A finger-foil seal, comprising: an aerodynamic foil having a generally annular body through which a first opening is formed; a finger seal retention structure disposed around the aerodynamic foil; and a finger seal backing spring coupled to the finger seal retention structure and extending radially inward therefrom to contact an outer circumference of the aerodynamic foil, the finger seal backing spring comprising a plurality of laminates and having a predetermined radial stiffness profile that varies as taken axially through the finger seal backing spring from laminate to laminate; wherein the plurality of laminates includes at least one intermediate laminate, wherein the finger seal backing spring increases in radial stiffness when moving axially through the finger seal backing spring in a downstream direction until reaching the at least one intermediate laminate, and wherein the finger seal backing spring decreases in r

Assignees

Inventors

Classifications

  • Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations · CPC title

  • F16J15/164Primary

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

  • Shaft sealings · CPC title

  • with means for adjusting the clearance · CPC title

  • with metal springs · CPC title

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What does patent US9506566B2 cover?
Embodiments of a gas turbine engine including a finger-foil seal are provided, as are embodiments of a finger-foil seal. In one embodiment, the finger-foil seal includes an aerodynamic foil having a generally annular body through which a first opening is formed. A finger seal retention structure is disposed around the aerodynamic foil. A finger seal backing spring is coupled to the finger seal …
Who is the assignee on this patent?
Honeywell Int Inc
What technology area does this patent fall under?
Primary CPC classification F16J15/164. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 29 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).