Adjustable holding assembly

US10690267B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10690267-B2
Application numberUS-201816036628-A
CountryUS
Kind codeB2
Filing dateJul 16, 2018
Priority dateJul 16, 2018
Publication dateJun 23, 2020
Grant dateJun 23, 2020

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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

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A mounting assembly for restricting movement of an electrical harness of a gas turbine engine includes a base, a first channel formed in the base and extending between a first surface and a second surface of the base, and a second channel formed in the base and extending between the first surface and a third surface of the base. The second surface and the third surface are distinct. At least one flexible connector is receivable within the first channel and the second channel. At least a portion of the at least one flexible connector extends about the electrical harness to couple the electrical harness to the base.

First claim

Opening claim text (preview).

What is claimed is: 1. A mounting assembly for restricting movement of an electrical harness of a gas turbine engine, comprising: a base; a first channel formed in the base and extending between a first surface and a second surface of the base; a second channel formed in the base and extending between the first surface and a third surface of the base, the second surface and the third surface being distinct; and at least one connector receivable within the first channel and the second channel, wherein at least a portion of the at least one connector operable to retain and conform to the shape of an electrical harness to the base, a first end of the at least one connector being fastened to the base within the first channel by a first fastener and a second end of the at least one connector being fastened to the base within the second channel by a second fastener. 2. The mounting assembly of claim 1 , wherein the first channel is located adjacent a first side of the base and the second channel is positioned adjacent a second side of the base. 3. The mounting assembly of claim 1 , wherein the first channel extends from an upper surface of the base to a first side surface of the base and the second channel extends from the upper surface of the base to a second side surface of the base. 4. The mounting assembly of claim 3 , wherein the first side surface is disposed opposite the second side surface. 5. The mounting assembly of claim 1 , wherein the at least one connector is a single connector. 6. The mounting assembly of claim 1 , wherein the at least one connector includes a first connector and a second connector, wherein the first end of the at least one connector is a first end of the first connector being affixed within the first channel and wherein the first end of the at least one connector is a first end of the second connector being affixed within the second channel. 7. The mounting assembly of claim 6 , wherein a second end of the first connector is coupleable to a second end of the second connector to couple the electrical harness to the base. 8. The mounting assembly of claim 7 , wherein the second end of the first connector is coupleable to the second end of the second connector via a hook and loop-type attachment. 9. The mounting assembly of claim 6 , wherein a tab is formed at the second end of at least one of the first connector and the second connector. 10. The mounting assembly of claim 1 , wherein the at least one connector includes a single connector having a first end and a second end, the first end being extendable through the first channel and the second end being extendable through the second channel. 11. The mounting assembly of claim 10 , wherein the first end is connectable to the second end to couple the electrical harness to the base. 12. The mounting assembly of claim 11 , wherein the first end is coupleable to the second end via a hook and loop-type attachment. 13. The mounting assembly of claim 1 , wherein a force applied by the at least one connector to the electrical harness is adjustable. 14. The mounting assembly of claim 1 , wherein the at least one connector defines a body joined with and perpendicular to the first end, and the first end defines a mounting hole sized to receive the first fastener. 15. A gas turbine engine comprising: a mounting surface; an electrical harness; a mounting assembly for affixing the electrical harness to the mounting surface at a location, the mounting assembly including: a base connected to the mounting surface; a first channel formed in the base and extending between a first surface and a second surface of the base; a second channel formed in the base and extending between the first surface and a third surface of the base, the second surface and the third surface being distinct; and at least one connector receivable within the first channel and the second channel, wherein at least a portion of the at least one connector extends about the electrical harness to couple the electrical harness to the base, a first end of the at least one connector being fastened to the base within the first channel by a first fastener and a second end of the at least one connector being fastened to the base within the second channel by a second fastener. 16. The gas turbine engine of claim 15 , wherein the gas turbine engine further comprises a casing and the mounting surface is an exterior surface of the casing. 17. The gas turbine engine of claim 15 , wherein the at least one connector defines a body joined with and perpendicular to the first end, and the first end and the mounting surface define respective mounting holes sized to receive the first fastener.

Assignees

Inventors

Classifications

  • F16L3/123Primary

    and extending along the attachment surface · CPC title

  • Protecting, fastening and routing means therefor · CPC title

  • using mounting clamps · CPC title

  • Supporting or mounting arrangements, e.g. for turbine casing · CPC title

  • in combination with supports for lines, e.g. for pipes or cables · CPC title

Patent family

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Frequently asked questions

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What does patent US10690267B2 cover?
A mounting assembly for restricting movement of an electrical harness of a gas turbine engine includes a base, a first channel formed in the base and extending between a first surface and a second surface of the base, and a second channel formed in the base and extending between the first surface and a third surface of the base. The second surface and the third surface are distinct. At least on…
Who is the assignee on this patent?
United Technologies Corp, Raytheon Tech Corp
What technology area does this patent fall under?
Primary CPC classification F16L3/123. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 23 2020 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).