Bracket doubler

US9964042B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9964042-B2
Application numberUS-201414527175-A
CountryUS
Kind codeB2
Filing dateOct 29, 2014
Priority dateOct 29, 2013
Publication dateMay 8, 2018
Grant dateMay 8, 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 bracket assembly for a gas turbine engine includes a bracket base with a separation between a first bended feature and a second bended feature. A doubler is mechanically fastened adjacent to the separation. Another bracket assembly for a gas turbine engine includes a bracket base with a separation between a first bended feature and a second bended feature. A cushioned tube support is welded to the bracket base. A doubler is mechanically fastened adjacent to the separation. A method of assembling a bracket assembly for a gas turbine engine includes mechanically fastening a doubler to a bracket base adjacent to a separation between a first bended feature and a second bended feature.

First claim

Opening claim text (preview).

What is claimed is: 1. An assembly for a gas turbine engine, comprising: a bracket base with a separation between a first bended feature and a second bended feature; a doubler fastened adjacent to the separation; a cushioned tube support welded to the bracket base; and a buffer tube supported by the cushioned tube support, wherein the doubler is “L” shaped, and wherein the doubler is fastened to the bracket base and the cushioned tube support. 2. The assembly as recited in claim 1 , wherein the doubler bridges the separation. 3. The assembly as recited in claim 1 , wherein the doubler includes a doubler separation adjacent to the separation. 4. The assembly as recited in claim 1 , wherein the first bended feature and the second bended feature are directed in generally opposite directions on either side of the separation. 5. The assembly as recited in claim 4 , wherein the first bended feature and the second bended feature each include at least one fastener aperture. 6. An assembly for a gas turbine engine, comprising: a bracket base with a separation between a first bended feature and a second bended feature, the bracket base including a crack in proximity to the separation; a cushioned tube support welded to the bracket base; and a doubler fastened adjacent to the separation, wherein the doubler is “L” shaped, wherein the doubler is fastened to the bracket base and the cushioned tube support, and wherein the crack is a result of a stress riser formed in the bracket base due to the separation. 7. The assembly as recited in claim 6 , wherein the doubler is riveted to the bracket base. 8. The assembly as recited in claim 6 , wherein the doubler is riveted to the bracket base and the cushioned tube support. 9. The assembly as recited in claim 6 , wherein the first bended feature and the second bended feature are directed in generally opposite directions. 10. The assembly as recited in claim 9 , wherein the first bended feature and the second bended feature each include at least one fastener aperture. 11. The assembly as recited in claim 1 , further comprising: a second cushioned tube support welded to the bracket base; and a second buffer tube supported by the second cushioned tube support. 12. The assembly as recited in claim 1 , wherein the doubler is mechanically fastened adjacent to the separation, and wherein the doubler is mechanically fastened to the bracket base and the cushioned tube support.

Assignees

Inventors

Classifications

  • F02C7/20Primary

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

  • Arrangement, mounting, or driving, of auxiliaries · CPC title

  • Protection of pipes or objects of similar shape against external or internal damage or wear ({protection under water F16L1/123;} supporting of pipes inside other pipes or sleeves F16L7/00; used in connection with end fittings of hoses F16L35/00; protection of pipes or pipe fittings against corrosion or incrustation F16L58/00; protection thereof during transport B65D59/00) · CPC title

  • each support having one transverse base for supporting the pipes (F16L3/23, F16L3/237 take precedence) · CPC title

  • in the form of specially adapted hangers or supports · CPC title

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What does patent US9964042B2 cover?
A bracket assembly for a gas turbine engine includes a bracket base with a separation between a first bended feature and a second bended feature. A doubler is mechanically fastened adjacent to the separation. Another bracket assembly for a gas turbine engine includes a bracket base with a separation between a first bended feature and a second bended feature. A cushioned tube support is welded t…
Who is the assignee on this patent?
United Technologies Corp
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 May 08 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).