Attachment assembly and gas turbine engine with attachment assembly

US10119424B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10119424-B2
Application numberUS-201514707704-A
CountryUS
Kind codeB2
Filing dateMay 8, 2015
Priority dateMay 8, 2015
Publication dateNov 6, 2018
Grant dateNov 6, 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.

An attachment assembly for attaching a center structure to an outer structure at least partially circumscribing the center structure, the attachment assembly having a bushing provided within the center structure or the outer structure, the bushing defining a first through passage, a bushing adapter slidably mounted within the first through passage and defining a second through passage, a threaded passage provided on the other of the center structure or the outer structure and a bolt passing through the first through passage and the second through passage and threaded into the threaded passage.

First claim

Opening claim text (preview).

What is claimed is: 1. An attachment assembly for attaching a center structure to an outer structure at least partially circumscribing the center structure, the attachment assembly comprising: a bushing provided within the center structure or the outer structure, the bushing defining a first through passage; a bushing adapter slidably mounted within the first through passage and defining a second through passage; a threaded passage provided on the other of the center structure or the outer structure; and a bolt having a head and a shank with a threaded portion wherein the bolt passes through the first through passage and the second through passage, with the head abutting the bushing adapter and the threaded portion threaded into the threaded passage, wherein the bushing adapter is able to move along the length of the first through passage after the attachment assembly is fully assembled. 2. The attachment assembly according to claim 1 , further comprising a belleville washer that clamps the bushing to the center structure. 3. The attachment assembly of claim 1 wherein the bolt further comprises a third through passage extending through its length and the third through passage defines a fluid path from the center structure to the outer structure. 4. The attachment assembly of claim 1 wherein the bushing has a cylindrical body that terminates in a shoulder, which forms a stop. 5. The attachment assembly of claim 1 wherein the bushing has a cylindrical internal portion. 6. The attachment assembly of claim 1 , further comprising a nut having a threaded opening forming the threaded passage. 7. The attachment assembly of claim 1 wherein an upper portion of the bushing adapter is concentric with other features of the bushing adapter. 8. An attachment assembly for attaching a center structure to an outer structure at least partially circumscribing the center structure, the attachment assembly comprising: a bushing provided within the center structure or the outer structure, the bushing defining a first through passage; a bushing adapter slidably mounted within the first through passage and defining a second through passage; a threaded passage provided on the other of the center structure or the outer structure; and a bolt having a head and a shank with a threaded portion wherein the bolt passes through the first through passage and the second through passage, with the head abutting the bushing adapter and the threaded portion threaded into the threaded passage; wherein the bushing adapter has an annular shoulder with a rounded surface that enables a swivel joint between the bushing and the bushing adapter. 9. An attachment assembly for attaching a center structure to an outer structure at least partially circumscribing the center structure, the attachment assembly comprising: a bushing provided within the center structure or the outer structure, the bushing defining a first through passage; a bushing adapter slidably mounted within the first through passage and defining a second through passage; a threaded passage provided on the other of the center structure or the outer structure; and a bolt having a head and a shank with a threaded portion wherein the bolt passes through the first through passage and the second through passage, with the head abutting the bushing adapter and the threaded portion threaded into the threaded passage; wherein an upper portion of the bushing adapter is eccentric and enables adjustment of an axial position of the center structure. 10. The attachment assembly of claim 9 wherein other features of the bushing adapter are concentric to an axis of the bolt. 11. A gas turbine engine, comprising: a centerbody; a support structure circumscribing the centerbody; and an attachment assembly for operably coupling the centerbody to the support structure and configured to allow a cooling air flow to the centerbody, comprising: a bushing provided on the centerbody or the support structure, the bushing defining a first through passage; a bushing adapter slidably mounted within the first through passage and defining a second through passage; a threaded passage provided on the other of the centerbody or the support structure; and a bolt having a head and a shank with a threaded portion wherein the bolt passes through the first through passage and the second through passage, with the head abutting the bushing adapter and the threaded portion threaded into the threaded passage; wherein the bushing adapter is able to move along the length of the first through passage after the attachment assembly is fully assembled. 12. The gas turbine engine of claim 11 wherein a plurality of attachment assemblies are circumferentially spaced about the centerbody and the support structure. 13. The gas turbine engine of claim 11 wherein the bolt further comprises a third through passage extending through its length. 14. The gas turbine engine of claim 11 wherein a controlled gap is located between the centerbody and a portion of the support structure. 15. The gas turbine engine of claim 11 wherein the support structure comprises an exhaust frame of the gas turbine engine. 16. The gas turbine engine of claim 11 wherein the centerbody is formed from a ceramic matrix composite.

Assignees

Inventors

Classifications

  • Ceramic matrix composites [CMC] · CPC title

  • in gas turbines · CPC title

  • F02C7/20Primary

    Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title

  • Mounting of an exhaust cone in the jet pipe · CPC title

  • Mounting on supporting structures or systems · CPC title

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What does patent US10119424B2 cover?
An attachment assembly for attaching a center structure to an outer structure at least partially circumscribing the center structure, the attachment assembly having a bushing provided within the center structure or the outer structure, the bushing defining a first through passage, a bushing adapter slidably mounted within the first through passage and defining a second through passage, a thread…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F02C7/20. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 06 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).