Gas turbine engine variable stator vane assembly

US9062560B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9062560-B2
Application numberUS-201213418451-A
CountryUS
Kind codeB2
Filing dateMar 13, 2012
Priority dateMar 13, 2012
Publication dateJun 23, 2015
Grant dateJun 23, 2015

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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 variable stator vane assembly for a gas turbine engine includes a variable stator vane and a non-structural fairing on the variable stator vane.

First claim

Opening claim text (preview).

What is claimed: 1. A variable stator vane assembly for a gas turbine engine comprising: a variable stator vane including a platform adjacent to an airfoil, said airfoil comprises a leading edge and a trailing edge extending beyond an outer circumference of said platform; a fillet adjacent said platform, said platform includes a flat and said fillet extends from said trailing edge to said flat; and a fairing covering said fillet, wherein said fairing comprises a generally cylindrical member with an airfoil shaped aperture and a tab, said tab configured to interface with said flat. 2. The assembly as recited in claim 1 , wherein said fairing surrounds said airfoil. 3. The assembly as recited in claim 1 , further comprising a trunnion which extends from said platform. 4. The assembly as recited in claim 3 , wherein said fairing surrounds said airfoil opposite said trunnion. 5. The assembly as recited in claim 1 , wherein said airfoil extends beyond said platform. 6. The assembly as recited in claim 1 , further comprising a metal alloy sheath on said fairing. 7. A variable stator vane assembly for a gas turbine engine comprising: a first platform, said first platform includes a flat; a second platform; an airfoil between said first platform and said second platform along an axis of rotation, said airfoil comprises a leading edge and a trailing edge extending beyond an outer circumference of said first platform; a fillet adjacent said first platform, said fillet extends from said trailing edge to said flat; and a fairing which surrounds said airfoil adjacent to said first platform and covers said fillet, wherein said fairing comprises a generally cylindrical member with an airfoil shaped aperture and a tab, said tab configured to interface with said flat. 8. The assembly as recited in claim 7 , further comprising a first trunnion which extends from said first platform and a second trunnion which extends from said second platform. 9. The assembly as recited in claim 7 , wherein said airfoil extends beyond said first and second platform. 10. The assembly as recited in claim 7 , further comprising a metal alloy sheath on said fairing. 11. A method of manufacturing a variable stator vane assembly for a gas turbine engine comprising: molding a fairing onto a fillet of a variable stator vane; wherein said fairing comprises a generally cylindrical member with an airfoil shaped aperture and a tab, said tab configured to interface with a flat of an airfoil platform. 12. The method as recited in claim 11 , further comprising: molding the fairing adjacent to a platform of the variable stator vane. 13. The method as recited in claim 11 , further comprising: sheathing one side of the fairing. 14. The assembly as recited in claim 1 , wherein said fairing comprises: a non-metallic material configured to be formed onto said variable stator vane. 15. The assembly as recited in claim 1 , wherein said fairing is configured to prevent said fillet from blocking fluid flow.

Assignees

Inventors

Classifications

  • specially adapted for elastic fluid pumps · CPC title

  • Synthetic polymers, e.g. plastics; Rubber · CPC title

  • F01D17/162Primary

    for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

  • Sealing means between non relatively rotating elements · CPC title

  • Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member · CPC title

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Frequently asked questions

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What does patent US9062560B2 cover?
A variable stator vane assembly for a gas turbine engine includes a variable stator vane and a non-structural fairing on the variable stator vane.
Who is the assignee on this patent?
Hayford Richard K, Dube David P, United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D17/162. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 23 2015 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).