Assembly for passing an electrical harness into a turbine engine

US10436119B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10436119-B2
Application numberUS-201615561156-A
CountryUS
Kind codeB2
Filing dateMar 24, 2016
Priority dateMar 31, 2015
Publication dateOct 8, 2019
Grant dateOct 8, 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.

An assembly for passing an electrical harness through a wall includes a tubular metal end piece passing right through the wall and housing the electrical harness. The assembly further includes a sleeve made from heat-shrinkable material extending around an end part of the tubular end piece and of the electrical harness. The assembly further includes structures for extracting heat from the tubular end piece that are arranged on the side of the end piece surrounded by the heat-shrinkable sleeve.

First claim

Opening claim text (preview).

The invention claimed is: 1. An assembly for passing an electrical harness through a wall, the assembly comprising: a tubular metal end piece passing right through an orifice in the wall and housing the electrical harness; a heat-shrinkable sleeve made from heat-shrinkable material extending around an end part of the tubular metal end piece and of the electrical harness; and means for extracting heat from the tubular metal end piece, the means for extracting heat arranged, with respect to the wall, on a side of the tubular metal end piece surrounded by the heat-shrinkable sleeve, wherein the means for extracting heat includes a metal sheath entirely surrounding the heat-shrinkable sleeve, and wherein the tubular metal end piece comprises an annular collar applied to the wall and disposed between the wall and said means for extracting heat. 2. The assembly according to claim 1 , wherein the metal sheath is fixed to a first end situated on the wall side by clamping on the tubular metal end piece. 3. The assembly according to claim 2 , wherein said first end of the metal sheath is folded on itself radially inwards and clamped by a first member interposed radially between the first end and the remainder of the metal sheath. 4. The assembly according to claim 3 , wherein a second clamping member is applied to a second end of the metal sheath opposite to the first end that is in contact with the heat-shrinkable sleeve. 5. The assembly according to claim 2 , wherein said metal sheath is produced from a material having a thermal conductivity greater than that of the tubular metal end piece. 6. The assembly according to claim 2 , wherein the metal sheath is a metal braid. 7. The assembly according to claim 1 , wherein the means for extracting heat comprise: annular grooves disposed in alternation along an axis of the tubular metal end piece with annular ribs on the tubular metal end piece. 8. An intermediate casing for a turbine engine, comprising an assembly according to claim 1 , wherein said wall is a substantially cylindrical wall delimiting a radially internal flow surface of a gas flow. 9. A turbine engine comprising an assembly according to claim 1 . 10. An assembly for passing an electrical harness through a wall, comprising: a tubular metal end piece passing right through an orifice in the wall and housing the electrical harness; and a heat shrinkable sleeve made from heat-shrinkable material extending around an end part of the tubular metal end piece and of the electrical harness paid; and means for extracting heat from the tubular metal end piece, the means for extracting heat arranged, with respect to the wall, on the side of the tubular metal end piece surrounded by the heat-shrinkable sleeve, wherein the means for extracting heat includes a metal sheath entirely surrounding the heat-shrinkable sleeve.

Assignees

Inventors

Classifications

  • with a circular cross-section (H02G3/0468, H02G3/0475 take precedence) · CPC title

  • Cooling · CPC title

  • H02G3/22Primary

    Installations of cables or lines through walls, floors or ceilings, e.g. into buildings · CPC title

  • Sealing means for cable inlets (inlets for cables filled with, or surrounded by, gas or oil H02G15/32) · CPC title

  • Cable-harnesses · CPC title

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Frequently asked questions

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What does patent US10436119B2 cover?
An assembly for passing an electrical harness through a wall includes a tubular metal end piece passing right through the wall and housing the electrical harness. The assembly further includes a sleeve made from heat-shrinkable material extending around an end part of the tubular end piece and of the electrical harness. The assembly further includes structures for extracting heat from the tubul…
Who is the assignee on this patent?
Safran Aircraft Engines
What technology area does this patent fall under?
Primary CPC classification H02G3/22. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue Oct 08 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).