Detachable fan blade platform and method of repairing same

US10024177B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10024177-B2
Application numberUS-201213471718-A
CountryUS
Kind codeB2
Filing dateMay 15, 2012
Priority dateMay 15, 2012
Publication dateJul 17, 2018
Grant dateJul 17, 2018

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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 fan section for a gas turbine engine includes a hub. A fan blade is secured to the hub. A platform is removably secured to the hub and is arranged adjacent to the fan blade. The platform has a body with lateral sides that each include a channel. A seal is removably received in each of the channels, with one of the seals abutting the fan blade. A method of repairing the fan blade platform includes the steps of removing a nose cone to provide access to a hub, detaching a platform from the hub, and pulling the seal from a groove in the platform.

First claim

Opening claim text (preview).

What is claimed is: 1. A method of repairing a fan blade platform comprising the steps of: removing a nose cone to provide access to a fan hub; detaching the platform from the fan hub; pulling a removable seal from a groove in the platform; sliding a new seal in the groove and retaining the new seal therein without adhesive. 2. The method according to claim 1 , wherein the removing step includes removing a cap and a spinner. 3. The method according to claim 1 , wherein the pulling step includes sliding a pin out of the seal and removing the seal from a channel in the platform. 4. The method according to claim 3 , wherein the installing step includes sliding the pin into a longitudinal hole in the new seal. 5. The method according to claim 4 , wherein the installing step includes reattaching the nose cone to the fan hub, the nose cone blocking the pin in an axial direction.

Assignees

Inventors

Classifications

  • Repairing or disassembling · CPC title

  • Platforms for stationary or moving blades · CPC title

  • F01D5/3053Primary

    by means of pins · CPC title

  • by spacer elements between the blades, e.g. independent interblade platforms · CPC title

  • of axial insertion type · CPC title

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What does patent US10024177B2 cover?
A fan section for a gas turbine engine includes a hub. A fan blade is secured to the hub. A platform is removably secured to the hub and is arranged adjacent to the fan blade. The platform has a body with lateral sides that each include a channel. A seal is removably received in each of the channels, with one of the seals abutting the fan blade. A method of repairing the fan blade platform incl…
Who is the assignee on this patent?
Brown Charles W, United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D5/3053. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jul 17 2018 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).