EP2999058A1 - Assemblage de connecteur électrique - Google Patents

Assemblage de connecteur électrique Download PDF

Info

Publication number
EP2999058A1
EP2999058A1 EP14185758.1A EP14185758A EP2999058A1 EP 2999058 A1 EP2999058 A1 EP 2999058A1 EP 14185758 A EP14185758 A EP 14185758A EP 2999058 A1 EP2999058 A1 EP 2999058A1
Authority
EP
European Patent Office
Prior art keywords
connector
drive mechanism
assembly
array
electrical connectors
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.)
Withdrawn
Application number
EP14185758.1A
Other languages
German (de)
English (en)
Inventor
John Rice
Paul Elliott
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.)
Airbus Operations SAS
Airbus Operations Ltd
Original Assignee
Airbus Operations SAS
Airbus Operations Ltd
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 Airbus Operations SAS, Airbus Operations Ltd filed Critical Airbus Operations SAS
Priority to EP14185758.1A priority Critical patent/EP2999058A1/fr
Publication of EP2999058A1 publication Critical patent/EP2999058A1/fr
Withdrawn legal-status Critical Current

Links

Images

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
    • H01R13/46—Bases; Cases
    • H01R13/516—Means for holding or embracing insulating body, e.g. casing, hoods
    • H01R13/518—Means for holding or embracing insulating body, e.g. casing, hoods for holding or embracing several coupling parts, e.g. frames
    • 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
    • H01R13/62955—Pivoting lever comprising supplementary/additional locking means
    • 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
    • H01R13/62977—Pivoting levers actuating linearly camming means
    • 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
    • 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

Definitions

  • the present invention relates to electrical connection equipment for use in an aircraft.
  • the invention relates to an assembly for connecting an array of multiple electrical connectors to a second array of electrical connectors in a reliable and efficient manner.
  • Modem aircraft include large numbers of items of electronic equipment, used for various functions, ranging from peripheral systems, such as passenger entertainment systems, through to system-critical avionics equipment, which may relate to navigation, auto pilot, engine management systems etc.
  • Electronic equipment can be held in racks in aircraft and each piece of equipment may be connected to a number of connectors, which are mounted to a wiring harness to communicate electronic signals to and from the avionics equipment and on to other parts of the aircraft or its systems. The security of these connections is important and so each connector is generally secured using a multi-turn retaining nut, screw or bolt.
  • Each piece of equipment may have a relatively large number of connectors to connect, for example, eight connectors, arranged as two rows of four.
  • Each connector can be secured using one or more retaining bolts, and each bolt is to be tightened to a within narrow range of torque values using a specific tool, in order to ensure the security of the connection.
  • access to each retaining bolt can be difficult, due to the obstruction created by the wiring harness and/or adjacent connectors.
  • each individual connector can be subject to significant wear and stress, which can at least in part be transmitted through the wiring harness to the electrical connector.
  • a first aspect of the invention provides an assembly for connecting a first array of electrical connectors to a second array of electrical connectors, comprising: a connector mount, for receiving the first array of electrical connectors; and at least one connector locking element for retaining the connector mount to lock the first array of electrical connectors in engagement with the second array of electrical connectors; the connector locking element comprising a drive mechanism arranged to drive the connector mount and the first array of electrical connectors toward the second array of electrical connectors upon a first mechanical user input to the drive mechanism.
  • the drive mechanism is also arranged to drive the connector mount and the first array of electrical connectors away from the second array of electrical connectors upon a second mechanical user input to the drive mechanism, different from the first mechanical user input.
  • the drive mechanism may be configured to convert a rotational user input into a linear driving motion.
  • the drive mechanism may be rotatable and may have an eccentric surface able to push the connector mount or a connector locking element, in order to drive the connector mount and the first array of electrical connectors toward the second array of electrical connectors when the drive mechanism is rotated.
  • the eccentric surface is also able to push the connector mount or a connector locking element, in order to drive the connector mount and the first array of electrical connectors away from the second array of electrical connectors when the drive mechanism is rotated in a different way, for example in the other direction or an opposite direction.
  • the connector locking elements may be attached to one of: a second electrical connector mount; electrical equipment; and a mounting area for mounting electrical equipment.
  • the connector locking element or elements comprising the drive mechanism can be used to engage and lock together an array of electrical connectors to an array of corresponding electrical connectors, and retained in place by locking elements which are fixed relative to the corresponding connectors in numerous alternative configurations.
  • At least one of the connector locking elements may be movably mounted, so as to be movable into and out of engagement with the connector mount. This allows the connector mount to be advanced forward in a substantially linear direction without any obstruction by the connector locking elements. Subsequently the connector locking elements can be moved into engagement with the connector mount to hold it in place and may be subsequently actuated by mechanical user input to drive the electrical connectors into full engagement with one another.
  • the movement of the connector locking elements is preferably in a substantially lateral direction relative to a plane of the connector mount, so that the connector mount can be advanced in a direction substantially perpendicular to the plane of the connector mount to connect the connectors and then the connector locking elements can be moved into engagement in a direction substantially parallel to the plane of the connector mount, and/or perpendicularly to the direction in which the connector mount is advanced to join the electrical connectors.
  • At least one of the connector locking elements may comprise a shaft, the shaft being rotatably mounted at a first end and having the drive mechanism located at the second end, so that rotation of the shaft about its first end can move the drive mechanism into and/or out of engagement with the connector mount.
  • An axis of rotation of the drive mechanism may be substantially perpendicular to the direction of substantially linear motion of the connectors created by the drive mechanism. This allows a rapid creation of linear motion by rotation of the drive mechanism, and can include mechanisms such as a cam-based devices or other mechanisms as described herein.
  • the assembly may further comprise secondary locking means for maintaining the drive mechanism in a locked position. This helps to ensure security of the engagement of the connectors on the equipment.
  • the assembly may further comprise drive connection means connected to at least a first connector locking element and a second connector locking element of the assembly, so that a drive input to one of the first and second connector locking elements is transferred to the other of the first and second connector locking elements, to drive the first and second connector locking elements simultaneously.
  • the connector locking elements being simultaneously driven means that the drive mechanisms of plural connector locking elements are driven simultaneously. This can ensure even application of drive to separate points on the connector mount, to ensure even, parallel and steady connection of all connectors mounted to the connector mount.
  • the first connector locking element may comprise a lever for a user to provide a drive input and the second connector locking element may preferably be driven by the first connector locking element, via the drive connection means.
  • the drive mechanism may be a cam mechanism. This provides an efficient way for reliably translating rotational motion into a linear drive.
  • the cam mechanism may be configured with an over-centre locked position, configured to bias the cam mechanism to its locked position when it is in its locked position. This helps to ensure that the cam mechanism isn't accidently or undesirably opened or released without positive release input by a user.
  • the connector locking elements may comprise:
  • This configuration provides an alternative mechanism for converting rotary motion to linear motion, and allows the provision of a different form of follower member, which can extend away from the connector mount to engage corresponding engagement points on all adjacent to the equipment to which the connectors are being connected.
  • the assembly may further comprise a fixed ramp and the follower member may comprise a ramp engagement portion arranged to be driven along the ramp when the follower member is moved to a disengaged position to move the follower member laterally.
  • the fixed ramp can drive at least a portion of the follower member, or a projecting portion connected to the follower member, perpendicularly to its axis of linear movement, to assist with its disengagement from corresponding engagement portions for holding the connector mount in its engaged position. This facilitates easier assembly and disassembly of the connector mount at the equipment before the drive mechanism is actuated for engagement, and after the drive mechanism is activated for disassembly.
  • the assembly may further comprise a detent for arresting rotational movement of the drive mechanism. This can provide a way of locking the drive mechanism in its fully engaged position to hold the connectors securely in place.
  • the detent may comprise a fixed element comprising an arcuate portion and a notch; and a lever of the connector locking element comprises a protrusion which is biased towards the notch to engage the notch and lock the drive mechanism.
  • a further aspect of the invention provides a connector locking arrangement for receiving and locking in the place a connector mount, comprising: at least one connector locking element for retaining the connector mount to lock the first array of electrical connectors in engagement with a second array of electrical connectors; the connector locking element comprising a drive mechanism arranged to drive the connector mount and the first array of electrical connectors toward the second array of electrical connectors upon mechanical user input to the drive mechanism.
  • a further aspect of the invention provides a connector mount for receiving a first array of electrical connectors, comprising:
  • the invention removes the need to secure each of an array of connectors with its own individual retaining bolt(s), which has the following benefits:
  • the present invention permits the installation of all of the aircraft harness connectors onto a single mount at harness production time, which can have the following benefits:
  • the present invention can improve the robustness of the installation by transmitting forces applied through the aircraft harness to the mounting mechanism and not to the electrical connectors.
  • the present invention can remove the need for individual connector retaining bolts, and individual backshells, which can reduce the number of parts required and operations required to assemble / disassemble the aircraft harness.
  • FIG. 1A shows a connector mount 10 of the present invention.
  • Connector mount 10 comprises a mounting plate 101 and a plurality of connectors 11, which are mounted to mounting plate 101.
  • Connectors 11 have a plurality of electrical wires 12 extending therefrom, which electrical wires can be connected to an electrical harness of a vehicle such as an aircraft.
  • Connectors useful in the invention can include those specified in aerospace standard EN4165.
  • the mounting plate 101 and connectors 11 can be manufactured as a single item in order to make it weigh less and to reduce the component count.
  • Figure 1B shows a top view of the connector mount 10 of figure 1A .
  • the connector plate 101 comprises at each end an engagement portion 102 for engaging a locking element, to connect the connector mount 10 and its connectors 11 to a piece of equipment, or to corresponding electrical connectors.
  • the engagement portion 102 comprises a notch 103, which is flanked either side by a protrusion 104. A connector locking element can therefore be received in the notch 103 and can engage the pair of protrusions 104 to lock the connector mount 10 in place with respect to a corresponding set of connectors arranged for connection to electrical connectors 11.
  • the connector mount 10 may further comprise a secondary engagement portion 105, arranged in a spaced configuration from the primary engagement portion 102, such that a connector locking element can be received in the gap 106 formed therebetween. This allows a connector locking element to drive against the primary engagement portion 102 to drive the connectors 11 into engagement with corresponding connectors, or alternatively against the secondary engagement portion 105 to drive the connector mount 10 away from, and out of engagement with, the corresponding connectors, to disengage connectors 11 therefrom.
  • Figures 2A to 2D show how covers can be assembled on the connector mount of figures 1A to 1D .
  • a central divider wall 107 may separate the 2 longitudinal rows of electrical connectors and can provide at least a degree of electromagnetic isolation between adjacent rows of connectors.
  • the connector mount may further comprise a central outer wall portion 108 comprising a plurality of openings 109 into which wires 12 extending from the connectors 11 can be located, to enable them to pass from an interior space of the connector mount body to an exterior of the connector mount body.
  • side portions 110 can be provided to the connector mount, and may comprise openings 111, arranged to coincide with openings 109 so that the covers comprising the central divider wall 107, the central outer wall portion 108 and the side portions 110 constitute a back shell of the connector mount wherein a plurality of openings 111/109 is provided for the passage of wires 12, as illustrated in figure 2D .
  • the enclosed back shell encloses the plural connectors 11 within the body of the connector mount 10. This can provide electromagnetic shielding to the full array of connectors by use of a single outer shell.
  • Figures 3A to 3D show how the connector mount 10 can be driven into, and locked in, engagement with a corresponding set of connectors 13 by connector locking elements 31.
  • FIG. 3A shows an item of electronic equipment 30, which may be avionics equipment in an aircraft.
  • the equipment 30 comprises a plurality of electrical connectors 13, for connecting the equipment to a wiring harness of a system or vehicle such as an aircraft.
  • a plurality of connector locking elements 31 Either mounted to equipment 30, or provided adjacent to and in a fixed configuration relative to equipment 30, is a plurality of connector locking elements 31, in this embodiment a pair of connector locking elements 31 is shown.
  • each connector locking element comprises a shaft 32 which is rotatable about a pivot point 33 located adjacent a first end 34 of the shaft 32.
  • a cam mechanism 35 is located at a second end, opposite the first end 34, of the shaft, for converting a rotational mechanical user input into a linear motion of the connector mount, when engaged with the connector mount.
  • cam mechanisms 31 are similarly configured and the levers 36 are simultaneously actuated, then the connector mount plate 101, carrying in connectors 11 will be advanced in a uniform manner, so that connectors 11 are all advanced together in a uniform manner. This allows the connectors 11 to be reliably and evenly connected to the equipment 30 via corresponding connectors 13, in a fast and efficient manner.
  • Each cam mechanism 31 constitute therefore a drive mechanism arranged to drive the connector mount 10 and the array of electrical connectors 11 toward the corresponding array of electrical connectors 13, upon mechanical user input to the drive mechanism.
  • the complete rotation of the cam mechanism 35 results in full engagement of connectors 11 with corresponding connectors 13 and so by configuring the cam mechanisms with a linear stroke equal to or greater than the distance of motion required to engage the connectors 11 with corresponding connectors 13, the full engagement of the connectors can be driven in a controlled manner by the drive mechanisms.
  • FIG 3D illustrates how, by rotation of the cam mechanisms 35 in an opposite direction to that illustrated in figure 3B , the cam mechanism can exert a force in the direction of arrow 39, against secondary engagement portions 105, to lift the connector mount 10, and the connectors 11 mounted thereto, away from electrical equipment 30 and its corresponding connectors 13 in a similarly even and controlled manner.
  • each cam mechanism 35 constitutes a drive mechanism arranged to drive the connector mount 10 and the array of electrical connectors 11 away from the corresponding array of electrical connectors 13, upon mechanical user input to the drive mechanism. Therefore, an appropriately configured drive mechanism can drive both engagement and disengagement of the connectors 11 mounted to the connector mount 10, in a controlled and even manner.
  • Figure 4 illustrates means by which the locking elements 31 can be configured to secure or lock the connector mount plate 101 and connectors 11 in place.
  • a first means by which this can be achieved is with an over-centre cam arrangement.
  • the cam mechanism When the cam mechanism is fully rotated, by fully rotating lever 36 to its engaged position, a point of greatest radius 361 of the cam profile 360, relative to pivot 362, has moved past, and is located beyond, a contact point 363 between the cam mechanism and the connector mounting plate 101.
  • resilient sealing means such as rubber seals in the connectors, then this elasticity can provide a degree of bias, which encourages the point of greatest radius 361 to be biased away from the plate 101 in a direction of arrow 364.
  • This resilience may alternatively be provided in shafts 32 or in the plate 101 itself, or in engagement portions 102.
  • This bias in the direction of arrow 364 imparts a moment on the cam mechanism in a direction of arrow 365, which maintains the connector locking element 31 in its closed or locked configuration as illustrated. Therefore, to disengage the connector locking element, a user must apply a force at lever 36 in a direction of arrow 366, to overcome the force in the direction of arrow 364 and disengage the connector locking element.
  • a secondary means which may further prevent the connector locking element from being inadvertently disengaged is to apply a secondary locking means, such as a mechanical locking means as exemplified by locking pin 40, to prevent lever 36 from being rotated in a direction of arrow 366 to disengage the connector locking element.
  • a secondary locking means such as a mechanical locking means as exemplified by locking pin 40
  • a drive connection means can be provided to ensure that the mechanisms rotate simultaneously.
  • this can be achieved by providing the cam mechanisms in an orientation which is rotated by 90 degrees about the axis of the shafts 32 relative to that shown in the drawings, so that the axes about which the cam mechanism 35 rotate are parallel and coincident. Then, by providing a shaft connecting the two cam mechanisms, their simultaneous rotation about their respective axes can be ensured.
  • An alternative form of drive mechanism and locking elements will now be described in relation to figures 5 to 8 .
  • Figure 5A shows a piece of electrical equipment 30.
  • the connector locking element comprises a projecting portion 51 and a hook portion 52 extending substantially perpendicularly to the projecting portion 51, for engaging a notch 55a.
  • the connector locking element is provided on the connector mount 50, which again carries a plurality of connectors 11.
  • Notch 55a is provided in a fixed configuration relative to the equipment 30.
  • the notch 55a may be provided on the equipment or on a mounting portion adjacent the equipment.
  • the connector locking element further comprises a mechanism for converting a rotational input into a linear extension or retraction of the projecting portion 51 and its corresponding hook portion 52.
  • This mechanism is described later in relation to figures 6A and 6B .
  • Figure 5B shows a top view of the arrangement of figure 5A , viewed from the direction of arrow 501.
  • a shaft 53 is shown, for connecting a rotational movement of a first connector locking element 52a to a second connector locking element 52b.
  • a lever 54 may be provided, attached to either the shaft 53, or to one of the first and second connector locking elements 52a and 52b.
  • connector locking elements 52a and 52b Simultaneous rotation of connector locking elements 52a and 52b is therefore ensured by their connection to shaft 53, and a single input can therefore advance or retract connector mount 50 and connectors 11 towards and away from electrical equipment 30 as shown by arrow 502 in figure 5a .
  • Figure 6A and 6B show how the connector locking elements 52 translate a rotational motion of the shaft 53 into a linear motion of the projecting portions 51.
  • Figure 6A shows a side view of the drive mechanism of figure 5A , as if viewed from the left hand end of figure 5A .
  • the projecting portion 51, and its corresponding hook portion 52 are engaged with the notch 55a in the receiving portion 55.
  • An axial protrusion 61 is mounted to a rotatable element 60 of the drive mechanism, and engages with a slot 62 provided in a follower member connected to the projecting portion 51. It will therefore be apparent that rotation of element 60 about its central axis 63 (i.e. shaft 53) will be translated into linear motion of the follower member and its extension 51, in the direction of arrows 64.
  • each connector locking element 52a and 52b constitutes a drive mechanism arranged to drive the connector mount 50 and the array of electrical connectors 11 toward the corresponding array of electrical connectors 13, upon a first mechanical user input to the drive mechanism.
  • these drive mechanisms are also arranged to drive the connector mount 10 and the array of electrical connectors 11 away from the corresponding array of electrical connectors 13, upon a second mechanical user input to the drive mechanism, different from the first mechanical user input.
  • FIG. 7A A mechanism which can assist with this motion is illustrated in figures 7A and 7B .
  • the rotatable element 60 can be seen with its axial protrusion 61 engaging with the slot 62 (not shown in Figure 7A ) of a follower member 51a connected to the lower part 51c of the projecting portion 51.
  • the connection between follower member 51a and the lower part 51c of the projecting portion 51 is provided with a pivot 70, such as a hinge.
  • the follower member 51a therefore moves in a linear fashion up and down in figure 7A when driven by the rotatable member 60 as described in relation to figures 6A and 6B .
  • the lower part 51c of the projecting portion 51, and an upwardly extending part 51b are able to pivot about pivot point 70.
  • a fixed ramp 72 is provided in fixed relation to the position of the rotatable member 60.
  • fixed ramp 72 can engage a corresponding ramp or ramp engagement portion 73 provided to the upwardly extending part 51b of the projecting portion 51.
  • Linear motion in a direction of arrow 71 can then be converted to a lateral motion of the upwardly extending part 51b of the projecting portion 51, which causes the lower part 51c of the projecting portion 51 to extend in the opposite direction by pivoting around pivot point 70.
  • this lateral motion will act to disengage the protrusions 52 from the notches 55a in receiving elements 55, leaving the connector mount 50 free to be completely removed from the equipment 30.
  • the desired lateral motion can be created by providing either one, or both of, the fixed ramp 72 and/or the movable ramp 73.
  • the follower member 51a, the upwardly extending part 51b, the ramp engagement portion 73, the lower part 51c and the protrusions 52 can be manufactured as a single formed and welded part, comprising a flexible hinge 70.
  • Figures 8A and 8B show how a detent can be used to lock the arrangement shown in figures 5A to 7B in a locked configuration.
  • Internal components such as spring 82 and first part 541, are shown in the figures in dotted lines, but may in practice be at least partially concealed within the assembly.
  • the lever 54 of figure 5B and 5C can comprise a first part 541 linked to the shaft 53, a second part 542, surrounding the first part 541, and able to translate on the first part 541 in a direction radial to the axis of rotation of the shaft 53.
  • This second part 542 is biased toward the axis of rotation of the shaft 53, thanks to a tension spring 82.
  • the detent is provided by a wall portion 83, arranged in a plane perpendicular to the axis of rotation of the shaft 53, which has an arcuate section 83a and a notch 83b.
  • An corner portion 81 of the second part 542, which may be considered a pin 81, is in contact with the border of the wall portion. It will be appreciated that while the portion 81 of the second part 542 is in contact with the arcuate section 83a, then the lever 54 is free to rotate about the axis of the shaft 53.
EP14185758.1A 2014-09-22 2014-09-22 Assemblage de connecteur électrique Withdrawn EP2999058A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP14185758.1A EP2999058A1 (fr) 2014-09-22 2014-09-22 Assemblage de connecteur électrique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP14185758.1A EP2999058A1 (fr) 2014-09-22 2014-09-22 Assemblage de connecteur électrique

Publications (1)

Publication Number Publication Date
EP2999058A1 true EP2999058A1 (fr) 2016-03-23

Family

ID=51609939

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14185758.1A Withdrawn EP2999058A1 (fr) 2014-09-22 2014-09-22 Assemblage de connecteur électrique

Country Status (1)

Country Link
EP (1) EP2999058A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106848744A (zh) * 2017-01-24 2017-06-13 董小凯 一种防松动电力供电装置

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0549371A2 (fr) * 1991-12-27 1993-06-30 Sumitomo Wiring Systems, Ltd. Système de connexion
DE29505601U1 (de) * 1995-03-31 1995-05-24 Amphenol Tuchel Elect EMV-dichte Gehäuse für schwere Steckverbinder der Serie C146
FR2717319A1 (fr) * 1994-03-11 1995-09-15 Cinch Connecteurs Sa Boîtier de connecteur électrique.
WO1996032761A1 (fr) * 1995-04-12 1996-10-17 The Whitaker Corporation Connecteur electrique modulaire
US7329132B1 (en) * 2006-07-31 2008-02-12 Yazaki North America, Inc. Low-insertion force-lever connector for blind mating
DE102007037176B3 (de) * 2007-08-07 2009-02-26 Tyco Electronics Amp Gmbh Modularer Steckverbinder
US20140273551A1 (en) * 2013-03-14 2014-09-18 Molex Incorporated Cable module connector assembly suitable for use in blind-mate applications

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0549371A2 (fr) * 1991-12-27 1993-06-30 Sumitomo Wiring Systems, Ltd. Système de connexion
FR2717319A1 (fr) * 1994-03-11 1995-09-15 Cinch Connecteurs Sa Boîtier de connecteur électrique.
DE29505601U1 (de) * 1995-03-31 1995-05-24 Amphenol Tuchel Elect EMV-dichte Gehäuse für schwere Steckverbinder der Serie C146
WO1996032761A1 (fr) * 1995-04-12 1996-10-17 The Whitaker Corporation Connecteur electrique modulaire
US7329132B1 (en) * 2006-07-31 2008-02-12 Yazaki North America, Inc. Low-insertion force-lever connector for blind mating
DE102007037176B3 (de) * 2007-08-07 2009-02-26 Tyco Electronics Amp Gmbh Modularer Steckverbinder
US20140273551A1 (en) * 2013-03-14 2014-09-18 Molex Incorporated Cable module connector assembly suitable for use in blind-mate applications

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106848744A (zh) * 2017-01-24 2017-06-13 董小凯 一种防松动电力供电装置
CN106848744B (zh) * 2017-01-24 2017-11-21 温州正合知识产权服务有限公司 一种防松动电力供电装置

Similar Documents

Publication Publication Date Title
KR102431136B1 (ko) 직접 정합 및 정합해제를 위한 cpa 장치
RU2478166C1 (ru) Устройство для крепления модульного элемента в воздушном судне
US20170155211A1 (en) Float plate for blind matable electrical cable connectors
US9112307B2 (en) Connector locking system using a temperature responsive spring
EP2770587A1 (fr) Connecteur de verrouillage rotatif
US7066763B1 (en) Junction box assembly with cam levers
EP3027954A1 (fr) Raccord à montage rapide
US20160190729A1 (en) End-position fixing of a plug-in connection for increasing the vibration resistance
US20230150145A1 (en) Separable Robotic Interface
US20160332309A1 (en) Robotic tool interchange system
CN103650254B (zh) 杠杆式连接器
EP2913550B1 (fr) Système de verrouillage d'arbre cannelé à verrou
EP2999058A1 (fr) Assemblage de connecteur électrique
US20200378447A1 (en) Device for connecting an end of a first shaft to an end of a second shaft, and associated transmission assembly
EP4235978A2 (fr) Ensemble connecteur électrique à assistance de connexion
CA2863340C (fr) Ensemble helice et ensemble de retenue de pales d'helice
US10707605B2 (en) Bayonet connector
KR101508501B1 (ko) 커넥터 어셈블리
CN103711782A (zh) 连接件以及包括该连接件的医疗设备
EP3132174B1 (fr) Ensemble raccord de traversée de cloison à rétroaction
US10511085B2 (en) System for fastening a telematic module to the roof of a motor vehicle
CN109119836B (zh) 一种连接器组件及其公端连接器、母端连接器
US9761386B2 (en) Encapsulating protective cover for a switch
EP3060833B1 (fr) Ensemble porte-aimant
EP4310347A1 (fr) Kit de pièces d'accouplement pour un agencement de montage pour monter une sous-structure intérieure sur une structure primaire d'un coussin d'air

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN

18W Application withdrawn

Effective date: 20160708