Metallisation of a housing of an aeronautic engine made of electrically insulating material

US2015114677A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2015114677-A1
Application numberUS-201414528486-A
CountryUS
Kind codeA1
Filing dateOct 30, 2014
Priority dateOct 30, 2013
Publication dateApr 30, 2015
Grant date

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

The invention relates to an aeronautic engine ( 1 ), comprising: a housing ( 10 ), made of electrically insulating material, a first metal piece ( 2, 3 ), and electrical equipment ( 30 ), fixed to the housing ( 10 ) and connected to the first metal piece ( 2, 3 ) by means of an electrically conductive connection path ( 16, 18 ) and a first connecting flange ( 12, 14 ) of the housing ( 10 ).

First claim

Opening claim text (preview).

1 . An aeronautic engine, comprising: a housing, a first metal piece, and electrical equipment, fixed on the housing and connected to the first metal piece with an electrically conductive connection path, wherein the housing is made of electrically insulating material, and the housing comprises at least one first connecting flange, adapted to fix the housing to the first metal piece, the connection path being connected to the first metal piece with said first connecting flange.…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • F02C7/32Primary

    Mechanical Engineering · mapped topic

  • F01D25/28Primary

    Mechanical Engineering · mapped topic

  • Electricity · mapped topic

  • H01R4/64Primary

    Electricity · mapped topic

Patent family

Related publications grouped by family.

External sources

Next steps

Free tools are coming soon. Tell us what you want to track and we'll notify you.

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2015114677A1 cover?
The invention relates to an aeronautic engine ( 1 ), comprising: a housing ( 10 ), made of electrically insulating material, a first metal piece ( 2, 3 ), and electrical equipment ( 30 ), fixed to the housing ( 10 ) and connected to the first metal piece ( 2, 3 ) by means of an electrically conductive connection path ( 16, 18 ) and a first connecting flange ( 12, 14 ) of the housin…
Who is the assignee on this patent?
Snecma
What technology area does this patent fall under?
Primary CPC classification F02C7/32. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Apr 30 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). 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).