Trunnion hole repair utilizing interference fit inserts

US9404374B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9404374-B2
Application numberUS-8222908-A
CountryUS
Kind codeB2
Filing dateApr 9, 2008
Priority dateApr 9, 2008
Publication dateAug 2, 2016
Grant dateAug 2, 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 vane shroud for a gas turbine engine has a cylindrical shaped body and a hole arranged at a circumference of the body. The hole is for receiving a trunnion from a variable vane. A counterbore is arranged concentrically around the hole on a radially inward facing surface of the body, and receives a trunnion hub from the variable vane. A shrink-fit insert is seated into the counterbore such that the trunnion hub is provided with a contact surface, and the shrink-fit insert is secured to the shroud through an interference fit.

First claim

Opening claim text (preview).

The invention claimed is: 1. A vane shroud for a gas turbine engine, the vane shroud comprising: a cylindrical shaped body; a hole arranged at a circumference of the body, wherein the hole is for receiving a trunnion from a variable vane; a counterbore arranged concentrically around the hole on a radially inward facing surface of the body, wherein the counterbore is for receiving a trunnion hub from the variable vane; and an insert seated into the counterbore such that the trunnion hub is provided with a contact surface; wherein the insert is secured to the shroud through an interference fit. 2. The vane shroud of claim 1 wherein the insert is a pre-existing washer. 3. The vane shroud of claim 1 wherein the counterbore is over-sized by a process used to remove a damaged portion of the body. 4. The vane shroud of claim 3 wherein the insert seated into the counterbore restores the cylindrical shaped body to design dimensions. 5. The vane shroud of claim 2 wherein the insert contains tangs to further secure the insert within the shroud. 6. The vane shroud of claim 1 wherein the insert is custom made from dimensions of the counterbore prior to the installation of the insert. 7. The vane shroud of claim 1 wherein the insert is comprised of a material having a lower coefficient of friction than that of the body. 8. The vane shroud of claim 1 wherein the insert comprises at least one of the following materials: a metallic alloy and a plastic.

Assignees

Inventors

Classifications

  • by temperature differential [e.g., shrink fit] · CPC title

  • Mechanically attaching preform by separate fastener · CPC title

  • Metallurgically attaching preform · CPC title

  • Mechanically attaching preform with separate fastener · CPC title

  • Removing material · CPC title

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Frequently asked questions

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What does patent US9404374B2 cover?
A vane shroud for a gas turbine engine has a cylindrical shaped body and a hole arranged at a circumference of the body. The hole is for receiving a trunnion from a variable vane. A counterbore is arranged concentrically around the hole on a radially inward facing surface of the body, and receives a trunnion hub from the variable vane. A shrink-fit insert is seated into the counterbore such tha…
Who is the assignee on this patent?
Addis Mark E, Reynolds George H, United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D9/042. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 02 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).