FR3012516B1 - Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant - Google Patents

Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant Download PDF

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Publication number
FR3012516B1
FR3012516B1 FR1360639A FR1360639A FR3012516B1 FR 3012516 B1 FR3012516 B1 FR 3012516B1 FR 1360639 A FR1360639 A FR 1360639A FR 1360639 A FR1360639 A FR 1360639A FR 3012516 B1 FR3012516 B1 FR 3012516B1
Authority
FR
France
Prior art keywords
metallizing
casing
insulating material
electrically insulating
aeronautical
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1360639A
Other languages
English (en)
Other versions
FR3012516A1 (fr
Inventor
Murtaza Hussain ZAFARI
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1360639A priority Critical patent/FR3012516B1/fr
Priority to US14/528,486 priority patent/US9595774B2/en
Priority to GB1419340.3A priority patent/GB2522100B/en
Publication of FR3012516A1 publication Critical patent/FR3012516A1/fr
Application granted granted Critical
Publication of FR3012516B1 publication Critical patent/FR3012516B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/58—Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
    • H01R4/64—Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G3/00—Installations of electric cables or lines or protective tubing therefor in or on buildings, equivalent structures or vehicles
    • H02G3/02—Details
    • H02G3/08—Distribution boxes; Connection or junction boxes
    • H02G3/081—Bases, casings or covers
FR1360639A 2013-10-30 2013-10-30 Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant Active FR3012516B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1360639A FR3012516B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant
US14/528,486 US9595774B2 (en) 2013-10-30 2014-10-30 Metallisation of a housing of an aeronautic engine made of electrically insulating material
GB1419340.3A GB2522100B (en) 2013-10-30 2014-10-30 Metallisation of a housing of an aeronautic engine made of electrically insulating material

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1360639A FR3012516B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant
FR1360639 2013-10-30

Publications (2)

Publication Number Publication Date
FR3012516A1 FR3012516A1 (fr) 2015-05-01
FR3012516B1 true FR3012516B1 (fr) 2018-01-05

Family

ID=49876884

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1360639A Active FR3012516B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter d'un moteur aeronautique en materiau electriquement isolant

Country Status (3)

Country Link
US (1) US9595774B2 (fr)
FR (1) FR3012516B1 (fr)
GB (1) GB2522100B (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10465694B2 (en) * 2017-04-05 2019-11-05 Hamilton Sundstrand Corporation Fan inlet diffuser housing with conductive composite body
CN113969839B (zh) * 2021-09-30 2023-12-15 陕西航空电气有限责任公司 一种航空发动机点火电缆密封结构

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3710568A (en) * 1971-08-12 1973-01-16 Gen Electric Integral tubing and/or electrical lead support and mounting pad for gas turbine engine controls and accessories
US5174110A (en) * 1991-10-17 1992-12-29 United Technologies Corporation Utility conduit enclosure for turbine engine
US5845544A (en) * 1996-07-15 1998-12-08 Eaton Corporation Control module
FR2866991B1 (fr) * 2004-02-26 2006-05-19 Airbus France Dispositif de retour d'alimentation electrique pour equipements avioniques
US7246990B2 (en) * 2004-12-23 2007-07-24 General Electric Company Composite fan containment case for turbine engines
FR2913053B1 (fr) 2007-02-23 2009-05-22 Snecma Sa Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu
JP5173596B2 (ja) * 2008-05-27 2013-04-03 株式会社オートネットワーク技術研究所 電気接続箱
JP5146113B2 (ja) * 2008-05-30 2013-02-20 住友電装株式会社 電気接続箱
FR2932456B1 (fr) * 2008-06-17 2010-05-28 Airbus France Systeme de drainage d'un courant de foudre genere par une decharge orageuse sur un aeronef
FR2933378B1 (fr) * 2008-07-04 2010-08-27 Airbus France Procede de montage d'une antenne sur un aeronef, et aeronef equipe d'au moins une antenne montee suivant ce procede
US8231080B2 (en) * 2009-02-26 2012-07-31 The Boeing Company Distributing power in systems having a composite structure
FR2966508B1 (fr) * 2010-10-22 2015-04-03 Snecma Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication
GB2497807B (en) * 2011-12-22 2014-09-10 Rolls Royce Plc Electrical harness
GB2498006B (en) * 2011-12-22 2014-07-09 Rolls Royce Plc Gas turbine engine systems
US9478896B2 (en) * 2011-12-22 2016-10-25 Rolls-Royce Plc Electrical connectors
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine

Also Published As

Publication number Publication date
GB2522100A (en) 2015-07-15
GB2522100B (en) 2020-04-29
FR3012516A1 (fr) 2015-05-01
GB201419340D0 (en) 2014-12-17
US20150114677A1 (en) 2015-04-30
US9595774B2 (en) 2017-03-14

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