CN205882330U - Aviation connector - Google Patents

Aviation connector Download PDF

Info

Publication number
CN205882330U
CN205882330U CN201620780518.6U CN201620780518U CN205882330U CN 205882330 U CN205882330 U CN 205882330U CN 201620780518 U CN201620780518 U CN 201620780518U CN 205882330 U CN205882330 U CN 205882330U
Authority
CN
China
Prior art keywords
stitch
netting twine
socket contact
contact pin
jack
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.)
Expired - Fee Related
Application number
CN201620780518.6U
Other languages
Chinese (zh)
Inventor
赵永兵
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.)
Shenzhen Joy Navigation Technology Co Ltd
Original Assignee
Shenzhen Joy Navigation Technology Co 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 Shenzhen Joy Navigation Technology Co Ltd filed Critical Shenzhen Joy Navigation Technology Co Ltd
Priority to CN201620780518.6U priority Critical patent/CN205882330U/en
Application granted granted Critical
Publication of CN205882330U publication Critical patent/CN205882330U/en
Priority to PCT/CN2017/084047 priority patent/WO2018014635A1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R24/00Two-part coupling devices, or either of their cooperating parts, characterised by their overall structure
    • H01R24/20Coupling parts carrying sockets, clips or analogous contacts and secured only to wire or cable
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R31/00Coupling parts supported only by co-operation with counterpart
    • H01R31/06Intermediate parts for linking two coupling parts, e.g. adapter

Landscapes

  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Abstract

The utility model provides an aviation connector, include: quartzy head, net twine and electric connector, electric connector includes two above jacks, all includes four socket contact pins in each jack, each quartzy head all is connected to through the net twine two at least jacks of electric connector. The utility model discloses each quartzy head all is connected to through the net twine two jacks of electric connector to each socket contact pin all corresponds a stitch that is connected to quartzy head in the jack, and the mutual interference can be avoided at the data transmission in -process to feasible eight wires that are connected with same quartzy head, can reach the performance of giga data and can guarantee data, and then makes aviation connector can use giga data transmission method to realize data transmission, and this routine data transmission speed has improved 10 times nearly on prior art's basis.

Description

A kind of aerospace connectors
Technical field
This utility model relates to a kind of adapter, particularly relates to a kind of aerospace connectors.
Background technology
In prior art, crystal head is all the network using wherein 4 lines to transmit 100,000,000 data, but sending out along with technology Exhibition and the increase of network data, 100,000,000 networks used in the transmission of former data, its message transmission rate is relatively low, can not Adapt to the transmission of current big data, in order to solve the transmission means of this low rate, it is desirable to provide a kind of new transmission method and The mode of connection of adapter.
Summary of the invention
Technical problem to be solved in the utility model is to need to provide a kind of aviation that can improve message transmission rate Adapter.
To this, this utility model provides a kind of aerospace connectors, including crystal head, netting twine and electric connector, described in be electrically connected Connect device and include two or more jack, each jack all includes four socket contact pins;Each crystal head is all by netting twine even It is connected at least two jack of described electric connector.
Further improvement of the utility model is, described electric connector includes the first jack and the second jack, described One jack and the second jack are connected on the different stitch of same crystal head by netting twine respectively.
Further improvement of the utility model is, also includes that trailing frog, described first jack and the second jack lead to respectively Crossing netting twine and be connected to one end of trailing frog, the other end of described trailing frog is connected to described crystal head by netting twine.
Further improvement of the utility model is, described crystal head include the first stitch, the second stitch, the 3rd stitch, 4th stitch, the 5th stitch, the 6th stitch, the 7th stitch and the 8th stitch, described first jack include the first socket contact pin, Two socket contact pins, the 3rd socket contact pin and the 4th socket contact pin, described second jack includes that the 5th socket contact pin, the 6th socket are inserted Pin, the 7th socket contact pin and the 8th socket contact pin, described first stitch is connected to the 3rd socket contact pin, institute by the wire of netting twine Stating the second stitch and be connected to the first socket contact pin by the wire of netting twine, described 3rd stitch is connected to by the wire of netting twine Seven socket contact pins, described 4th stitch is connected to the second socket contact pin by the wire of netting twine, and described 5th stitch passes through netting twine Wire be connected to the 4th socket contact pin, described 6th stitch is connected to the 5th socket contact pin by the wire of netting twine, described Seven stitch are connected to the 6th socket contact pin by the wire of netting twine, and described 8th stitch is connected to the 8th by the wire of netting twine and inserts Seat contact pin.
Further improvement of the utility model is, described crystal head is RJ45 connector.
Further improvement of the utility model is, institute's netting twine is super Category 5, Shielded netting twine.
Further improvement of the utility model is, described electric connector includes socket and four jacks, inserts for described four Hole is uniformly distributed on described socket.
Further improvement of the utility model is, the quantity of described crystal head is two.
Further improvement of the utility model is, also includes that spooler, described netting twine are arranged in described spooler.
Further improvement of the utility model is, described spooler is automatic line receiver.
Compared with prior art, the beneficial effects of the utility model are: each crystal head is all connected to by netting twine In two jacks, and jack of described electric connector, each socket contact pin is correspondingly connected to a stitch of crystal head, Make eight wires being connected with same crystal head in data transmission procedure it can be avoided that interfere, and can protect Card data can reach the performance of gigabit data, and then makes described aerospace connectors that gigabit data transmission method can be used to realize Data are transmitted, and the message transmission rate of this example improves nearly 10 times on the basis of existing technology.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of embodiment of this utility model;
Fig. 2 is the structural representation of electric connector in a kind of embodiment of this utility model;
Fig. 3 is the structural representation of four jacks of electric connector in a kind of embodiment of this utility model;
Fig. 4 is the wiring construction schematic diagram in a kind of embodiment of this utility model between crystal head and electric connector.
Detailed description of the invention
Below in conjunction with the accompanying drawings, preferably embodiment of the present utility model is described in further detail.
As depicted in figs. 1 and 2, this example provides a kind of aerospace connectors, including: crystal head 1, netting twine 2 and electric connector 3, Described electric connector 3 includes two or more jack, all includes four socket contact pins in each jack;Each crystal head 1 is equal At least two jack of described electric connector 3 it is connected to by netting twine 2.
As shown in Figures 1 to 4, electric connector 3 described in this example includes the first jack 31 and the second jack 32, and described first inserts Hole 31 and the second jack 32 are connected on the different stitch of same crystal head 1 by netting twine 2 respectively.Preferably, this example is also wrapped Including trailing frog 4, described first jack 31 and the second jack 32 are connected to one end of trailing frog 4, described doubling respectively by netting twine 2 The other end of device 4 is connected to described crystal head 1 by netting twine 2, is directly connected to by two netting twines 2 as it is shown in figure 1, avoid Crystal head 1 is attractive in appearance and be easy to wiring.
As shown in Figure 4, crystal head 1 described in this example includes first stitch the 11, second stitch the 12, the 3rd stitch the 13, the 4th pin Foot the 14, the 5th stitch the 15, the 6th stitch the 16, the 7th stitch 17 and the 8th stitch 18;Described first jack 31 includes the first socket Contact pin the 311, second socket contact pin the 312, the 3rd socket contact pin 313 and the 4th socket contact pin 314;Described second jack 32 includes Five socket contact pin the 321, the 6th socket contact pin the 322, the 7th socket contact pin 323 and the 8th socket contact pins 324;Described first stitch 11 Being connected to the 3rd socket contact pin 313 by the wire of netting twine 2, the cable specification of its wire is preferably brown;Described second stitch 12 are connected to the first socket contact pin 311 by the wire of netting twine 2, and the cable specification of its wire is preferably white brown;Described 3rd Stitch 13 is connected to the 7th socket contact pin 323 by the wire of netting twine 2, and the cable specification of its wire is preferably green;Described Four stitch 14 are connected to the second socket contact pin 312 by the wire of netting twine 2, and the cable specification of its wire is preferably white blue;Institute Stating the 5th stitch 15 and be connected to the 4th socket contact pin 314 by the wire of netting twine 2, the cable specification of its wire is preferably blueness; Described 6th stitch 16 is connected to the 5th socket contact pin 321 by the wire of netting twine 2, and the cable specification of its wire is preferably the greenest Color;Described 7th stitch 17 is connected to the 6th socket contact pin 322 by the wire of netting twine 2, and the cable specification of its wire is preferably Orange;Described 8th stitch 18 is connected to the 8th socket contact pin 324 by the wire of netting twine 2, and the cable specification of its wire is preferred For the most orange.It is noted that first, described wire refers to thin wire, each netting twine 2 can include 4 or The wire of other quantity;And described crystal head 1 this wire with the first jack 31 and the second jack 32 respectively is connected pass at this System is a kind of preferably annexation, in actual applications, it is also possible to there is other annexation, as long as meeting data to transmit it Between will not interfere.
Electric connector 3 described in this example preferably includes socket 5 and four jacks, as shown in Figure 1, Figure 2 and Figure 3, described four Jack is uniformly distributed on described socket 5, and the most described jack includes the first jack 31 and the second jack 32, in this case, right Answering, the quantity of described crystal head 1 is two;Two other of described electric connector 3 do not have labelled jack and crystal head it Between annexation, as the annexation being connected to described crystal head 1 with described first jack 31 and the second jack 32.
Described in this example, crystal head 1 is preferably RJ45 connector;Institute's netting twine 2 is super Category 5, Shielded netting twine;Described electric connector It is preferably MIL-C-38999;Described socket 5 is preferably CA140266-62, i.e. JJB socket.
This example can also preferably include spooler, and described netting twine 2 is arranged in described spooler, realizes net by spooler The storage of line 2, it is possible to netting twine how long 2 is stored, on the basis of being easy to take-up, additionally it is possible to change the length of netting twine 2; Described spooler is automatic line receiver, it is possible to the most user-friendly so that the length of netting twine 2 can be according to reality Needs quickly elongate and receive.
Each crystal head 1 of this example is all connected in two jacks, and jack of described electric connector 3 by netting twine 2 Each socket contact pin is correspondingly connected to a stitch of crystal head 1 so that lead for eight be connected with same crystal head 1 Line in data transmission procedure it can be avoided that interfere, and can guarantee that data can reach the performance of gigabit data, and then Making described aerospace connectors that gigabit data transmission method can be used to realize data transmission, the message transmission rate of this example is existing Improve nearly 10 times on the basis of having technology.
The detailed description of the invention of the above is better embodiment of the present utility model, not limits this practicality with this new The scope that is embodied as of type, scope of the present utility model includes being not limited to this detailed description of the invention, all according to this utility model Shape, structure made equivalence change all in protection domain of the present utility model.

Claims (10)

1. an aerospace connectors, it is characterised in that including: crystal head, netting twine and electric connector, described electric connector includes two Individual above jack, all includes four socket contact pins in each jack;Each crystal head is all connected to described electricity by netting twine At least two jack of adapter.
Aerospace connectors the most according to claim 1, it is characterised in that described electric connector includes the first jack and second Jack, described first jack and the second jack are connected on the different stitch of same crystal head by netting twine respectively.
Aerospace connectors the most according to claim 2, it is characterised in that also include trailing frog, described first jack and Two jacks are connected to one end of trailing frog respectively by netting twine, and the other end of described trailing frog is connected to described crystal by netting twine Head.
Aerospace connectors the most according to claim 2, it is characterised in that described crystal head includes the first stitch, the second pin Foot, the 3rd stitch, the 4th stitch, the 5th stitch, the 6th stitch, the 7th stitch and the 8th stitch, described first jack includes One socket contact pin, the second socket contact pin, the 3rd socket contact pin and the 4th socket contact pin, described second jack includes that the 5th socket is inserted Pin, the 6th socket contact pin, the 7th socket contact pin and the 8th socket contact pin, described first stitch is connected to by the wire of netting twine Three socket contact pins, described second stitch is connected to the first socket contact pin by the wire of netting twine, and described 3rd stitch passes through netting twine Wire be connected to the 7th socket contact pin, described 4th stitch is connected to the second socket contact pin by the wire of netting twine, described Five stitch are connected to the 4th socket contact pin by the wire of netting twine, and described 6th stitch is connected to the 5th by the wire of netting twine and inserts Seat contact pin, described 7th stitch is connected to the 6th socket contact pin by the wire of netting twine, and described 8th stitch is led by netting twine Line is connected to the 8th socket contact pin.
5. according to the aerospace connectors described in Claims 1-4 any one, it is characterised in that described crystal head is RJ45 water Crystal-tipped.
6. according to the aerospace connectors described in Claims 1-4 any one, it is characterised in that institute's netting twine is super Category 5, Shielded Netting twine.
7. according to the aerospace connectors described in Claims 1-4 any one, it is characterised in that described electric connector includes inserting Seat and four jacks, described four jacks are uniformly distributed on described socket.
Aerospace connectors the most according to claim 7, it is characterised in that the quantity of described crystal head is two.
9. according to the aerospace connectors described in Claims 1-4 any one, it is characterised in that also include spooler, described net Line is arranged in described spooler.
Aerospace connectors the most according to claim 9, it is characterised in that described spooler is automatic line receiver.
CN201620780518.6U 2016-07-22 2016-07-22 Aviation connector Expired - Fee Related CN205882330U (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201620780518.6U CN205882330U (en) 2016-07-22 2016-07-22 Aviation connector
PCT/CN2017/084047 WO2018014635A1 (en) 2016-07-22 2017-05-12 Aviation connector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620780518.6U CN205882330U (en) 2016-07-22 2016-07-22 Aviation connector

Publications (1)

Publication Number Publication Date
CN205882330U true CN205882330U (en) 2017-01-11

Family

ID=57697576

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620780518.6U Expired - Fee Related CN205882330U (en) 2016-07-22 2016-07-22 Aviation connector

Country Status (2)

Country Link
CN (1) CN205882330U (en)
WO (1) WO2018014635A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018014635A1 (en) * 2016-07-22 2018-01-25 深圳喜乐航科技有限公司 Aviation connector

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2738418Y (en) * 2004-09-30 2005-11-02 联想网御科技(北京)有限公司 Connecting apparatus used between network equipment and management host machine serial interface
US9236688B2 (en) * 2013-02-15 2016-01-12 Tyco Electronics Services Gmbh Electrical connectors having differential pairs
CN203150861U (en) * 2013-02-21 2013-08-21 江苏捷诚车载电子信息工程有限公司 Connection conversion device between network interface and aviation connector
CN203367535U (en) * 2013-06-04 2013-12-25 上海寰创通信科技股份有限公司 Network interface connection structure for rail transport communication devices
CN105406284A (en) * 2015-12-09 2016-03-16 国网北京市电力公司 Network line connector and network line
CN205882330U (en) * 2016-07-22 2017-01-11 深圳喜乐航科技有限公司 Aviation connector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018014635A1 (en) * 2016-07-22 2018-01-25 深圳喜乐航科技有限公司 Aviation connector

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Legal Events

Date Code Title Description
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170111

Termination date: 20200722