FR3079679B1 - Prise d'alimentation en energie electrique d'un aeronef - Google Patents

Prise d'alimentation en energie electrique d'un aeronef Download PDF

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Publication number
FR3079679B1
FR3079679B1 FR1852734A FR1852734A FR3079679B1 FR 3079679 B1 FR3079679 B1 FR 3079679B1 FR 1852734 A FR1852734 A FR 1852734A FR 1852734 A FR1852734 A FR 1852734A FR 3079679 B1 FR3079679 B1 FR 3079679B1
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FR
France
Prior art keywords
connection means
aircraft
electrical connection
socket
hand
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
FR1852734A
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English (en)
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FR3079679A1 (fr
Inventor
Gaspard Cayzac
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.)
Amphenol Air LB SAS
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Amphenol Air LB SAS
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Publication date
Application filed by Amphenol Air LB SAS filed Critical Amphenol Air LB SAS
Priority to FR1852734A priority Critical patent/FR3079679B1/fr
Publication of FR3079679A1 publication Critical patent/FR3079679A1/fr
Application granted granted Critical
Publication of FR3079679B1 publication Critical patent/FR3079679B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/648—Protective earth or shield arrangements on coupling devices, e.g. anti-static shielding  
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/35—Ground or aircraft-carrier-deck installations for supplying electrical power to stationary aircraft
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/66—Structural association with built-in electrical component
    • H01R13/6608—Structural association with built-in electrical component with built-in single component
    • H01R13/6641—Structural association with built-in electrical component with built-in single component with diode
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/66—Structural association with built-in electrical component
    • H01R13/665—Structural association with built-in electrical component with built-in electronic circuit
    • H01R13/6666—Structural association with built-in electrical component with built-in electronic circuit with built-in overvoltage protection
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R2201/00—Connectors or connections adapted for particular applications
    • H01R2201/26—Connectors or connections adapted for particular applications for vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Abstract

L'invention concerne une prise d'alimentation en énergie électrique (1) d'un aéronef, cette prise d'alimentation (1) comporte une prise de parc (2) qui comporte, d'une part, une embase (3) qui est destinée à être rendue solidaire de l'aéronef et, d'autre part, un moyen de liaison électrique neutre (4) et au moins un moyen de liaison électrique d'alimentation (5), chacun de ces moyens de liaison électrique (4 ; 5) traverse l'embase (3). Cette prise (1) est caractérisée en ce qu'elle comporte, encore, un système de protection (7) de l'aéronef contre la foudre, ce système de protection (7) comporte, d'une part, un moyen de réception neutre (8) configuré pour recevoir le moyen de liaison électrique neutre (4) de la prise de parc (2) ainsi qu'au moins un moyen de réception d'alimentation (9), chacun configuré pour recevoir le moyen de liaison électrique d'alimentation (5) ou l'un des moyens de liaison électrique d'alimentation (5) de la prise de parc (2), d'autre part, au moins un moyen de raccordement électrique (11 ; 11'), chacun configuré pour raccorder électriquement, audit moyen de réception neutre (8), le moyen de réception d'alimentation (9) ou l'un des moyens de réception d'alimentation (9).
FR1852734A 2018-03-29 2018-03-29 Prise d'alimentation en energie electrique d'un aeronef Active FR3079679B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1852734A FR3079679B1 (fr) 2018-03-29 2018-03-29 Prise d'alimentation en energie electrique d'un aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1852734 2018-03-29
FR1852734A FR3079679B1 (fr) 2018-03-29 2018-03-29 Prise d'alimentation en energie electrique d'un aeronef

Publications (2)

Publication Number Publication Date
FR3079679A1 FR3079679A1 (fr) 2019-10-04
FR3079679B1 true FR3079679B1 (fr) 2021-05-07

Family

ID=63294306

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1852734A Active FR3079679B1 (fr) 2018-03-29 2018-03-29 Prise d'alimentation en energie electrique d'un aeronef

Country Status (1)

Country Link
FR (1) FR3079679B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8922961B2 (en) * 2009-09-25 2014-12-30 Hamilton Sundstrand Corporation Two-level lightning protection circuit
US8808033B2 (en) * 2012-05-30 2014-08-19 Cooper Technologies Company Ground power connector saver
FR3028101B1 (fr) * 2014-11-04 2018-02-02 Airbus Operations Dispositif de securite pour une prise gigogne
FR3063839B1 (fr) * 2017-03-07 2019-06-07 Airbus Operations (S.A.S.) Systeme de protection contre la foudre pour un aeronef

Also Published As

Publication number Publication date
FR3079679A1 (fr) 2019-10-04

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