Bolt retention assembly for gas turbine engine

US10415624B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10415624-B2
Application numberUS-201715606580-A
CountryUS
Kind codeB2
Filing dateMay 26, 2017
Priority dateMay 26, 2017
Publication dateSep 17, 2019
Grant dateSep 17, 2019

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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 bolt retention clip for a gas turbine engine rotor assembly includes a main plate section defining a central aperture, the central aperture sized to receive a bolt therethrough. Also included is a pair of bolt retention tabs extending away from a first face of the main plate section to axially retain a head of the bolt. Further included is a first clip retaining tab extending away from the first face of the main plate section for insertion into a groove of a rotor structure. Yet further included is a second clip retaining tab extending away from a second face of the main plate section for engagement with an edge of the rotor structure.

First claim

Opening claim text (preview).

What is claimed is: 1. A bolt retention assembly for a gas turbine engine rotor assembly comprising: a plurality of rotor stages and a rotor hub disposed in a stacked arrangement, each of the rotor stages and the rotor hub defining respective holes; a bolt extending through the holes of the rotor stages and the rotor hub; and a retention clip comprising: a main plate section defining a central aperture, the central aperture sized to receive the bolt therethrough; a pair of bolt retention tabs extending away from a first face of the main plate section to axially retain a head of the bolt; a first clip retaining tab extending away from the first face of the main plate section for insertion into a groove defined by a rotor structure that is one of the rotor stages or the rotor hub, wherein the groove is defined by a main portion of the rotor structure and a rail of the rotor structure; and a second clip retaining tab extending away from a second face of the main plate section for engagement with an edge of the rotor structure. 2. The bolt retention assembly of claim 1 , wherein the bolt retention tabs are flexibly hinged to the main plate section. 3. The bolt retention assembly of claim 1 , wherein the bolt retention tabs extend perpendicularly to the main plate section. 4. The bolt retention assembly of claim 1 , wherein the first clip retaining tab extends perpendicularly to the main plate section. 5. The bolt retention assembly of claim 1 , wherein the second clip retaining tab comprises a first segment and a second segment, the first segment extending perpendicularly from the main plate section and the second segment extending perpendicularly from the first segment to define a U-shaped slot with the main plate section. 6. The bolt retention assembly of claim 5 , wherein the edge of the rotor structure is disposed in the U-shaped groove in an assembled condition of the bolt retention clip and the rotor structure. 7. The bolt retention assembly of claim 6 , wherein the rotor structure includes a recess located adjacent the edge engaged with the second clip retaining tab. 8. The bolt retention assembly of claim 6 , wherein the edge of the rotor structure and the second clip retaining tab are sized to be in an interference fit. 9. The bolt retention assembly of claim 1 , wherein the bolt is a T-bolt. 10. The bolt retention assembly of claim 1 , further comprising a nut secured to the bolt. 11. The bolt retention assembly of claim 1 , wherein the plurality of rotor stages comprises a first rotor stage, a second rotor stage, and a third rotor stage. 12. The bolt retention assembly of claim 11 , wherein the rotor structure is part of the third rotor stage.

Assignees

Inventors

Classifications

  • for surfaces not surrounding the bolt, e.g. hook adaptors for bolts · CPC title

  • Measures against loss of bolts, nuts or pins (devices for fastening nuts to surfaces F16B37/04) · CPC title

  • with snap action · CPC title

  • Disassembly methods · CPC title

  • Retaining bolts or nuts · CPC title

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Frequently asked questions

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What does patent US10415624B2 cover?
A bolt retention clip for a gas turbine engine rotor assembly includes a main plate section defining a central aperture, the central aperture sized to receive a bolt therethrough. Also included is a pair of bolt retention tabs extending away from a first face of the main plate section to axially retain a head of the bolt. Further included is a first clip retaining tab extending away from the fi…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F01D5/066. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Sep 17 2019 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).