FR3012527B1 - Metallisation d'un carter electriquement isolant d'un moteur aeronautique - Google Patents

Metallisation d'un carter electriquement isolant d'un moteur aeronautique

Info

Publication number
FR3012527B1
FR3012527B1 FR1360635A FR1360635A FR3012527B1 FR 3012527 B1 FR3012527 B1 FR 3012527B1 FR 1360635 A FR1360635 A FR 1360635A FR 1360635 A FR1360635 A FR 1360635A FR 3012527 B1 FR3012527 B1 FR 3012527B1
Authority
FR
France
Prior art keywords
metallizing
electrically insulating
insulating case
aeronautical
aeronautical motor
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
FR1360635A
Other languages
English (en)
Other versions
FR3012527A1 (fr
Inventor
Julien Sayn-Urpar
Jeremy Edmond Fert
Thierry Kohn
Julien Pavillet
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1360635A priority Critical patent/FR3012527B1/fr
Priority to US14/528,467 priority patent/US9919805B2/en
Priority to GB1419341.1A priority patent/GB2522101B/en
Publication of FR3012527A1 publication Critical patent/FR3012527A1/fr
Application granted granted Critical
Publication of FR3012527B1 publication Critical patent/FR3012527B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • 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
    • 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Elimination Of Static Electricity (AREA)
  • Prevention Of Electric Corrosion (AREA)
FR1360635A 2013-10-30 2013-10-30 Metallisation d'un carter electriquement isolant d'un moteur aeronautique Active FR3012527B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1360635A FR3012527B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter electriquement isolant d'un moteur aeronautique
US14/528,467 US9919805B2 (en) 2013-10-30 2014-10-30 Metallisation of an electrically insulating housing of an aeronautic engine
GB1419341.1A GB2522101B (en) 2013-10-30 2014-10-30 Metallisation of an electrically insulating case of an aeronautic engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1360635A FR3012527B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter electriquement isolant d'un moteur aeronautique

Publications (2)

Publication Number Publication Date
FR3012527A1 FR3012527A1 (fr) 2015-05-01
FR3012527B1 true FR3012527B1 (fr) 2015-10-30

Family

ID=50101974

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1360635A Active FR3012527B1 (fr) 2013-10-30 2013-10-30 Metallisation d'un carter electriquement isolant d'un moteur aeronautique

Country Status (3)

Country Link
US (1) US9919805B2 (fr)
FR (1) FR3012527B1 (fr)
GB (1) GB2522101B (fr)

Family Cites Families (14)

* 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
DK173460B2 (da) * 1998-09-09 2004-08-30 Lm Glasfiber As Vindmöllevinge med lynafleder
DK176298B1 (da) * 2003-09-15 2007-06-18 Lm Glasfiber As Metode til lynsikring af en vinge til et vindenergianlæg, en lynsikret vinge samt et vindenergianlæg med en sådan vinge
FR2866991B1 (fr) * 2004-02-26 2006-05-19 Airbus France Dispositif de retour d'alimentation electrique pour equipements avioniques
GB2452298B (en) * 2007-08-30 2010-01-13 Gkn Aerospace Services Ltd Composite structure
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
FR2948637B1 (fr) * 2009-07-31 2012-01-20 Airbus Operations Sas Aeronef comprenant des equipements electriques et des pieces en materiau composite
ES2396508B1 (es) * 2010-10-13 2014-02-12 Airbus Operations, S.L. Sistema de proteccion contra rayos para tapas de acceso en aeronaves.
FR2966508B1 (fr) * 2010-10-22 2015-04-03 Snecma Carter de soufflante de moteur aeronautique en materiau composite et procede pour sa fabrication
US20130075539A1 (en) * 2011-09-26 2013-03-28 Mark J. Seger Composite aerospace structure with integrated conveyance element
US9478896B2 (en) * 2011-12-22 2016-10-25 Rolls-Royce Plc Electrical connectors
GB2498006B (en) * 2011-12-22 2014-07-09 Rolls Royce Plc Gas turbine engine systems
FR2988978B1 (fr) * 2012-03-28 2014-06-27 Safran Support boitier fadec en materiau composite
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
GB2522101A (en) 2015-07-15
FR3012527A1 (fr) 2015-05-01
US20150115706A1 (en) 2015-04-30
GB201419341D0 (en) 2014-12-17
GB2522101B (en) 2020-09-02
US9919805B2 (en) 2018-03-20

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