EP1729376A2 - Verriegelungshebelmechanismus für Verbinder - Google Patents

Verriegelungshebelmechanismus für Verbinder Download PDF

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Publication number
EP1729376A2
EP1729376A2 EP06290728A EP06290728A EP1729376A2 EP 1729376 A2 EP1729376 A2 EP 1729376A2 EP 06290728 A EP06290728 A EP 06290728A EP 06290728 A EP06290728 A EP 06290728A EP 1729376 A2 EP1729376 A2 EP 1729376A2
Authority
EP
European Patent Office
Prior art keywords
locking lever
locking
plugging
cam path
lever
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.)
Granted
Application number
EP06290728A
Other languages
English (en)
French (fr)
Other versions
EP1729376B1 (de
EP1729376A3 (de
Inventor
Frédéric DUVAL
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.)
Connecteurs Electriques Deutsch SAS
Original Assignee
Connecteurs Electriques Deutsch 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 Connecteurs Electriques Deutsch SAS filed Critical Connecteurs Electriques Deutsch SAS
Publication of EP1729376A2 publication Critical patent/EP1729376A2/de
Publication of EP1729376A3 publication Critical patent/EP1729376A3/de
Application granted granted Critical
Publication of EP1729376B1 publication Critical patent/EP1729376B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • H01R13/62—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
    • H01R13/62938—Pivoting lever comprising own camming means

Definitions

  • the present invention relates to a connector locking lever.
  • the present invention relates in particular, although not limited to, a locking lever for the rapid connection and disconnection of electronic boxes in an aircraft, the electronic boxes being used for example for video and / or audio applications .
  • contact elements of a first plug-in part which is in the form of a cable harness plug, are removably coupled to contact elements opposite one another.
  • plugging part which is in the form of a plug contained in an electronic box.
  • connection or disconnection operations of such interlocking elements can be difficult to perform when the mechanical stresses during connection are important.
  • a poor connection may result in false contacts or even damage to the contact elements.
  • the electronic boxes are arranged under the seats of an aircraft. This has the disadvantage that the passenger, sitting on the seat, can act on the electronic box.
  • the first and second plugging portions may move relative to each other, which may cause disconnection of the electronic unit. Such a connection therefore poses problems of reliability and security.
  • the object of the present invention is to propose a locking lever for a connector which avoids at least some of the aforementioned drawbacks, which allows connection and disconnection. simpler two plugging parts, and that keeps the two plugging parts in the connected position.
  • the subject of the invention is a locking lever for a connector, said connector comprising a first plug-in part, fixed, and a second plug-in part capable of being connected to said first plug-in part by a translation in a connection direction, said locking lever having two end portions adapted to be pivotably attached, along an axis substantially perpendicular to said connection direction, on two opposite faces of said first insertion part, characterized in each of said end portions comprises a cam path, said locking lever being pivotable between a release position, in which an open end of each of said cam paths is adapted to be positioned at a stub of said second plugging part, and a locking position in which each of said pins is able to position itself in a locking portion of said cam path, said end portion being resiliently deformable to allow said pin to penetrate said locking portion and exert a compressive force between said first plug portion and said second portion of said cam portion; plugging.
  • each of said end portions comprises a groove extending along a portion of said corresponding cam path, one end of said groove opening at an end of said cam path, so as to that said cam path defines with said groove a tongue adapted to be deformed elastically to allow deformation of said portion terminal in response to a pressing force exerted on said tongue of said cam path.
  • said tongue is able to elastically assume a stable position once said pin has positioned in said notch to maintain the connection force.
  • said second plugging part is connected to an electronic box, said first plugging part being connected to an electronic device integrated in a vehicle, said first plugging part being fixed to said vehicle .
  • the locking lever comprises two lateral branches interconnected by a transverse spacer, said lateral branches being able to extend along two opposite faces of said electronic unit when said locking lever is in said locking position.
  • said spacer is able to extend substantially parallel to a face of said electronic housing when said locking lever is in said locking position, at least a handle portion of said spacer being offset from said face of said housing.
  • said vehicle is an aircraft, said electronic box being disposed under the seat of a seat of said aircraft, so that, when said locking lever is in said locking position, said lever locking is substantially parallel to the plane of said seat, said seat being able to press on said locking lever to maintain said locking lever in said locking position.
  • a connector 1 having a first plugging portion 2 and a second plugging portion 3, intended to be assembled to one another by interlocking.
  • the first one Part 2 is connected to an electronic device (not shown), for example integrated in a structure of an aircraft, the first part 2 being fixed relative to the structure.
  • the second part 3 is connected to an electronic box 4.
  • the electronic box is intended to be disposed under the seat of a seat (not shown) of the aircraft.
  • the second part 3 can be connected to the first part 2 by a translation in an X connection direction.
  • the second part 3 comprises for example, as contact elements (not shown), a multiplicity of plug sockets arranged in line.
  • the plug sockets are intended to surround, in the connected position, opposite contact elements (not shown) of the first part 2, for example pins.
  • Such a connector is known per se.
  • the connector 1 comprises a U-shaped locking lever 5.
  • the lever 5 comprises two substantially identical lateral branches 6, connected together by a transverse spacer 8.
  • the lateral branches 6 extend parallel to each other.
  • the free ends 9 of the branches 6 are pivotally attached to pivot elements 11 arranged on two opposite lateral faces 12 of the first part 2.
  • the locking lever 5 can thus pivot with respect to the first part 2 around a Y axis substantially orthogonal to the X axis, between a rest position ( Figure 1) and a locking position (Figure 8).
  • the spacer 8 has a central portion 13 serving as a handle during the manipulation of the lever 5, as will be described in detail below.
  • Each branch 6 has, starting from the spacer 8, a rectilinear central portion 16 arranged to form a right angle with the corresponding end portion 15. At the free end 9, each branch 6 has an end portion 17.
  • Each end portion 17 is substantially planar and disposed in the same plane as the middle portion 16.
  • Each end portion 17 has a groove 18 defining a cam path, the curvature of the cam path 18 being directed so that the cam path 18 is wound around the pivot 11.
  • the distance of the cam path 18 to the pivot 11 decreases from its end 19 towards the opposite end 24 of the cam path 18.
  • a groove 21 extends along a portion 22 of the cam path 18, one end 23 of the groove 21 opening at the end 24.
  • the cam path 18 defines with the groove 21 a tongue 25 adapted to be elastically deformed in response to a pressing force exerted on the tab 25 of the cam path 18, as will be described in detail below.
  • the second part 3 comprises, on each of two opposite lateral faces 30 corresponding to the faces 12, a lug 31 adapted to engage in the cam path 18.
  • the lugs 31 are arranged so that, when the second portion 3 is in position. abutting against the first part 2, each lug 31 is at one of the openings 20.
  • the tongue 25 In the vicinity of the end 24, the tongue 25 has a rounded notch which defines a recess 32 adapted to receive the pin 31 in the locking position of the lever 5.
  • each pin 31 slides in the corresponding cam path 18, towards the end 24.
  • the second part 3 under the effect of the cam tracks 18 acting on the pins 31, engages in the first part 2.
  • the tongue 25 begins to deform by elasticity, due to the pressing force exerted by the lug 31 on the tongue 25.
  • the tongue 25 assumes a stable position by elasticity, which causes the creation of a hard point 33 to maintain the lug 31 in the recess 32 and exert a force of compression between parts 2 and 3. This allows in particular to compensate for the tolerance intervals of the coupling. In this position, the contact elements of the first and second parts 2 and 3 are correctly connected.
  • the central portion 13 of the spacer 8 extends parallel to the upper face 34 of the housing 4, substantially parallel to the axis Y.
  • End portions 15 of the spacer 8 are extend along the opposite side faces 35 of the housing, substantially perpendicular to the axis X.
  • the branches 6 extend along the side faces 35, substantially parallel to the axis X.
  • the lever 5, when in the locked position, is substantially parallel to the casing 4. This allows the casing 4 to be placed under the seat of a seat of the aircraft substantially parallel to the plane of the seat. sitting, that is to say horizontally.
  • the support of the seat on the lever 5 helps maintain the lever 5 in its horizontal position, that is to say in its locking position, which prevents inadvertent disconnection of the housing 4.
  • a passenger can not access the housing 4, the latter being disposed under the seat of his seat.
  • the cam paths 18 of the lever 5 thus make it possible to ensure good distribution of the forces during the connection and disconnection operations, which facilitates these operations for the user.
  • the lever also makes it possible to define the insertion depth and to ensure the guidance along the X axis of the second part 3 with respect to the first part 2, which avoids twisting or breaking contact elements.

Landscapes

  • Details Of Connecting Devices For Male And Female Coupling (AREA)
EP06290728A 2005-05-31 2006-05-05 Verriegelungshebelmechanismus für Verbinder Expired - Lifetime EP1729376B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0505505A FR2886474A1 (fr) 2005-05-31 2005-05-31 Levier de verrouillage pour connecteur

Publications (3)

Publication Number Publication Date
EP1729376A2 true EP1729376A2 (de) 2006-12-06
EP1729376A3 EP1729376A3 (de) 2007-10-03
EP1729376B1 EP1729376B1 (de) 2009-09-23

Family

ID=35708645

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06290728A Expired - Lifetime EP1729376B1 (de) 2005-05-31 2006-05-05 Verriegelungshebelmechanismus für Verbinder

Country Status (8)

Country Link
US (1) US7335038B2 (de)
EP (1) EP1729376B1 (de)
JP (1) JP2006339154A (de)
CA (1) CA2548636C (de)
DE (1) DE602006009337D1 (de)
ES (1) ES2333899T3 (de)
FR (1) FR2886474A1 (de)
MX (1) MXPA06005971A (de)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008138613A1 (de) * 2007-05-15 2008-11-20 Phoenix Contact Gmbh & Co. Kg Verriegelungsbügel für steckverbindergehäuse
EP2133959A3 (de) * 2008-06-13 2013-12-18 Harting Electric GmbH & Co. KG Verriegelungsvorrichtung für Steckverbindergehäuse
EP3012922A1 (de) * 2014-10-20 2016-04-27 Multi-Holding AG Schwenkhebelanordnung für Gehäuseanordnung
EP2451021B1 (de) * 2010-11-05 2018-08-01 Lapp Engineering & Co. Verriegelungseinrichtung und Gehäuse für einen Steckverbinder mit dieser Verriegelungseinrichtung
CN108695646A (zh) * 2017-04-04 2018-10-23 泰连德国有限公司 插头连接器和产生插头连接的方法

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004033911B3 (de) * 2004-07-14 2005-12-01 Bernd Lenz Vorrichtung zur Aufnahme eines tragbaren Computers (Notebooks, Laptops)
JP5102519B2 (ja) 2007-03-15 2012-12-19 Ｄｏｗａメタルマイン株式会社 砒素含有固形物およびその製法
US7344394B1 (en) * 2007-10-16 2008-03-18 International Business Machines Corporation Multiple location latch mechanism with single actuation
EP2180558A1 (de) 2008-10-23 2010-04-28 Tyco Electronics AMP GmbH Verbinder mit Selbsthaltefeststellvorrichtung
JP5419224B2 (ja) 2010-04-13 2014-02-19 日立金属株式会社 レバー式コネクタ
JP4947181B2 (ja) * 2010-04-13 2012-06-06 日立電線株式会社 レバー式コネクタ
JP5666180B2 (ja) 2010-07-06 2015-02-12 矢崎総業株式会社 レバー式コネクタ
EP2559596B1 (de) * 2011-08-17 2015-10-07 Harman Becker Automotive Systems GmbH Rahmen mit Schnellverbindung für ein Fahrzeug
US20170005444A1 (en) * 2014-04-11 2017-01-05 HARTING Electronics GmbH Plug-in connector
DE102016120929B4 (de) * 2016-11-03 2018-10-31 Harting Electric Gmbh & Co. Kg Verriegelungsbügel für ein Steckverbindergehäuse
US10490938B2 (en) * 2017-10-20 2019-11-26 Lear Corporation Electrical connector with assist lever
US10270207B1 (en) * 2017-10-20 2019-04-23 Lear Corporation Electrical connector with assist lever
US10601177B1 (en) * 2018-09-07 2020-03-24 Lear Corporation Electrical connector lock with reverse stop
USD937068S1 (en) * 2019-07-08 2021-11-30 Harting Electric Gmbh & Co. Kg Locking device
JP7025464B2 (ja) * 2020-02-28 2022-02-24 矢崎総業株式会社 コネクタ

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2595402B2 (ja) * 1992-03-17 1997-04-02 矢崎総業株式会社 コネクタの結合装置
US5474462A (en) * 1992-05-01 1995-12-12 Yazaki Corporation Connector system with a lever requiring small force
JP3002940B2 (ja) * 1994-02-18 2000-01-24 矢崎総業株式会社 レバー式コネクタ
DE10223928A1 (de) * 2001-05-29 2003-01-23 Sumitomo Wiring Systems Hebeltyp-Verbinder und Verfahren zum Zusammenbauen
JP2006324227A (ja) * 2005-04-18 2006-11-30 Yazaki Corp コネクタ

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008138613A1 (de) * 2007-05-15 2008-11-20 Phoenix Contact Gmbh & Co. Kg Verriegelungsbügel für steckverbindergehäuse
EP2133959A3 (de) * 2008-06-13 2013-12-18 Harting Electric GmbH & Co. KG Verriegelungsvorrichtung für Steckverbindergehäuse
EP2451021B1 (de) * 2010-11-05 2018-08-01 Lapp Engineering & Co. Verriegelungseinrichtung und Gehäuse für einen Steckverbinder mit dieser Verriegelungseinrichtung
EP3012922A1 (de) * 2014-10-20 2016-04-27 Multi-Holding AG Schwenkhebelanordnung für Gehäuseanordnung
CN105522527A (zh) * 2014-10-20 2016-04-27 马尔遆公开股份有限公司 用于外壳装置的转动杠杆装置
CN108695646A (zh) * 2017-04-04 2018-10-23 泰连德国有限公司 插头连接器和产生插头连接的方法

Also Published As

Publication number Publication date
EP1729376B1 (de) 2009-09-23
US20060270257A1 (en) 2006-11-30
FR2886474A1 (fr) 2006-12-01
CA2548636C (fr) 2014-07-15
CA2548636A1 (fr) 2006-11-30
DE602006009337D1 (de) 2009-11-05
JP2006339154A (ja) 2006-12-14
ES2333899T3 (es) 2010-03-02
MXPA06005971A (es) 2007-01-26
US7335038B2 (en) 2008-02-26
EP1729376A3 (de) 2007-10-03

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