BR112012015580A2 - conector elétrico de aeronave com engate diferencial e forças de retenção operacionais - Google Patents

conector elétrico de aeronave com engate diferencial e forças de retenção operacionais

Info

Publication number
BR112012015580A2
BR112012015580A2 BR112012015580A BR112012015580A BR112012015580A2 BR 112012015580 A2 BR112012015580 A2 BR 112012015580A2 BR 112012015580 A BR112012015580 A BR 112012015580A BR 112012015580 A BR112012015580 A BR 112012015580A BR 112012015580 A2 BR112012015580 A2 BR 112012015580A2
Authority
BR
Brazil
Prior art keywords
aircraft
electrical connector
differential
aircraft electrical
hitch
Prior art date
Application number
BR112012015580A
Other languages
English (en)
Inventor
Anatoly Gosis
Christopher A Tacklind
Folkert Fred Koch
Scott Takayuki Koizumi
Wolfgan Ott
Original Assignee
Illinois Tool Works
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 Illinois Tool Works filed Critical Illinois Tool Works
Publication of BR112012015580A2 publication Critical patent/BR112012015580A2/pt

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
    • H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
    • H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
    • H01R13/639—Additional means for holding or locking coupling parts together, after engagement, e.g. separate keylock, retainer strap
    • 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
    • H01R13/02—Contact members
    • H01R13/193—Means for increasing contact pressure at the end of engagement of coupling part, e.g. zero insertion force or no friction
    • 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
    • H01R13/62—Means for facilitating engagement or disengagement of coupling parts or for holding them in engagement
    • H01R13/629—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances
    • H01R13/62933—Comprising exclusively pivoting lever
    • 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
    • H01R13/02—Contact members
    • H01R13/15—Pins, blades or sockets having separate spring member for producing or increasing contact pressure
    • H01R13/18—Pins, blades or sockets having separate spring member for producing or increasing contact pressure with the spring member surrounding the socket
    • 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
    • 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
    • H01R4/28—Clamped connections, spring connections
    • H01R4/48—Clamped connections, spring connections utilising a spring, clip, or other resilient member
    • 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
    • H01R4/28—Clamped connections, spring connections
    • H01R4/48—Clamped connections, spring connections utilising a spring, clip, or other resilient member
    • H01R4/489—Clamped connections, spring connections utilising a spring, clip, or other resilient member spring force increased by screw, cam, wedge, or other fastening means

Landscapes

  • Details Of Connecting Devices For Male And Female Coupling (AREA)
  • Connector Housings Or Holding Contact Members (AREA)

Abstract

conector elétrico de aeronave com engate diferencial e forças de retenção operacionais. um sistema de energização de aeronave é proporcionado que inclui um conector elétrico de aeronave que é proporcionado com características para permitir o fácil engate com uma aeronave e fortes forças de retenção. o sistema de energização de aeronave pode incluir o conector elétrico de aeronave tendo um único mecanismo de direcionamento e construção modular, onde o mecanismo de direcionamento é configurado para dispor as forças diferenciais sobre conectores elétricos casados a partir de uma aeronave. o mecanismo de direcionamento pode ser operaracionalmente acoplado a uma haste ou gatilho, que pode ser facilmente engatável por um operador.
BR112012015580A 2009-12-22 2010-11-19 conector elétrico de aeronave com engate diferencial e forças de retenção operacionais BR112012015580A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/645,451 US7980875B2 (en) 2006-03-13 2009-12-22 Aircraft electrical connector with differential engagement and operational retention forces
PCT/US2010/057506 WO2011078929A1 (en) 2009-12-22 2010-11-19 Aircraft electrical connector with differential engagement and operational retention forces

Publications (1)

Publication Number Publication Date
BR112012015580A2 true BR112012015580A2 (pt) 2016-03-22

Family

ID=43430753

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012015580A BR112012015580A2 (pt) 2009-12-22 2010-11-19 conector elétrico de aeronave com engate diferencial e forças de retenção operacionais

Country Status (7)

Country Link
US (2) US7980875B2 (pt)
EP (1) EP2517309B1 (pt)
CN (1) CN102782949B (pt)
BR (1) BR112012015580A2 (pt)
CA (1) CA2785399C (pt)
MX (1) MX2012007425A (pt)
WO (1) WO2011078929A1 (pt)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7980875B2 (en) 2006-03-13 2011-07-19 Illinois Tool Works Inc. Aircraft electrical connector with differential engagement and operational retention forces
US8387466B2 (en) * 2009-01-22 2013-03-05 Nissin Kogyo Co., Ltd. Electric part protection member and assembling method therefor
US9763657B2 (en) 2010-07-21 2017-09-19 Mitraltech Ltd. Techniques for percutaneous mitral valve replacement and sealing
US8840405B2 (en) * 2010-08-11 2014-09-23 John Bean Technologies Corporation Aircraft GPU connection method and apparatus
US8845206B2 (en) * 2011-03-29 2014-09-30 International Business Machines Corporation Apparatus for plugging multiple connectors with spring loaded sleeves into an adapter simultaneously
US20120309214A1 (en) * 2011-06-03 2012-12-06 James Beluse Aircraft power receptacle protection system
GB201200331D0 (en) * 2012-01-09 2012-02-22 Dialight Europ Ltd Improvements in switching contactors (II)
US8808033B2 (en) * 2012-05-30 2014-08-19 Cooper Technologies Company Ground power connector saver
CN103531973A (zh) * 2013-10-18 2014-01-22 河南天海电器有限公司 汽车用小结合力多线插接器
US9263816B1 (en) * 2015-03-20 2016-02-16 Tyco Electronics Brasil Ltda Retention member for use with an electrical junction box
JP6501119B2 (ja) * 2015-09-24 2019-04-17 株式会社オートネットワーク技術研究所 端子の接続構造およびコネクタ装置
CN105896154A (zh) * 2016-05-26 2016-08-24 四川永贵科技有限公司 飞机地面电源插头结构
FR3063839B1 (fr) * 2017-03-07 2019-06-07 Airbus Operations (S.A.S.) Systeme de protection contre la foudre pour un aeronef
CN107611750A (zh) * 2017-07-26 2018-01-19 同济大学 水下湿插拔辅助结构
US10014594B1 (en) * 2017-09-07 2018-07-03 Dinkle Enterprise Co., Ltd. Terminal block assembly and wiring wrench thereof
US10840640B1 (en) * 2019-07-18 2020-11-17 Optoway Technology Inc. Pluggable connector

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1119864A (en) * 1912-09-11 1914-12-08 Simplex Electric Heating Co Electric connector.
GB398541A (en) 1931-03-17 1933-09-18 Electrical Res Prod Inc Improvements in or relating to electrical connectors
US2476365A (en) * 1947-06-05 1949-07-19 Frank C Greco Contact plug for electric cords
US3643202A (en) * 1970-03-06 1972-02-15 James A Coon Quick release female plug
US3902075A (en) * 1972-06-05 1975-08-26 Stefan Oros Car anti-theft device
DE3900991C1 (pt) * 1989-01-12 1990-02-01 Krone Ag, 1000 Berlin, De
US6358082B1 (en) * 2001-02-12 2002-03-19 Berg Technology, Inc. Latch and release mechanism for an electrical connector
US6676428B2 (en) * 2001-02-28 2004-01-13 Burton Technologies, Llc Securing device for electrical connectors
US7980875B2 (en) 2006-03-13 2011-07-19 Illinois Tool Works Inc. Aircraft electrical connector with differential engagement and operational retention forces
US7871282B2 (en) 2006-03-13 2011-01-18 Illinois Tool Works Inc. Aircraft power connector with differential engagement and operational retention forces

Also Published As

Publication number Publication date
US20110269325A1 (en) 2011-11-03
MX2012007425A (es) 2012-08-31
US8113866B2 (en) 2012-02-14
US7980875B2 (en) 2011-07-19
US20100197159A1 (en) 2010-08-05
CN102782949B (zh) 2015-06-10
CA2785399A1 (en) 2011-06-30
CA2785399C (en) 2015-02-03
EP2517309B1 (en) 2017-01-04
EP2517309A1 (en) 2012-10-31
CN102782949A (zh) 2012-11-14
WO2011078929A1 (en) 2011-06-30

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B11E Dismissal acc. art. 34 of ipl - requirements for examination incomplete
B11T Dismissal of application maintained [chapter 11.20 patent gazette]