CN112713468A - Aviation plug connector fixing device - Google Patents
Aviation plug connector fixing device Download PDFInfo
- Publication number
- CN112713468A CN112713468A CN202011483916.9A CN202011483916A CN112713468A CN 112713468 A CN112713468 A CN 112713468A CN 202011483916 A CN202011483916 A CN 202011483916A CN 112713468 A CN112713468 A CN 112713468A
- Authority
- CN
- China
- Prior art keywords
- connector
- fixing
- aviation plug
- fixing tool
- tool body
- 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
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Classifications
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- 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
- H01R13/73—Means for mounting coupling parts to apparatus or structures, e.g. to a wall
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- 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
- H01R13/627—Snap or like fastening
-
- 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
- H01R13/631—Additional means for facilitating engagement or disengagement of coupling parts, e.g. aligning or guiding means, levers, gas pressure electrical locking indicators, manufacturing tolerances for engagement only
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- 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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The invention relates to an aviation plug connector fixing device which comprises an aviation plug fixing tool and a connector, wherein the aviation plug fixing tool comprises an aviation plug fixing tool body, one side of the aviation plug fixing tool body is provided with a mounting platform fixing hole, and the mounting platform fixing hole is used for mounting the fixing tool body on an aviation plug platform; the fixed frock body opposite side of aviation plug is equipped with fixed square groove, the fixed connecting plate that installs of casing surface of connector, locking bolt in connector and the fixed frock has guaranteed fixed frock fixed and protection to the connector, prevents that the connector slope is unstable to lead to the project failure, realizes the high-efficient safe removal of connector and lays.
Description
Technical Field
The invention relates to the field of aviation plug connectors, in particular to an aviation plug connector fixing device.
Background
The existing aviation plug connector fixing device is fixed through a designated connector, the line length planning and the position needing to be placed are considered while the fixing is carried out, when other operations such as conversion and the like are to be realized, the fixing device and the connector need to be disassembled, the connector is continuously matched with a proper fixing tool, and the defects of low efficiency, time waste and labor waste exist when the fixing device in the prior art is used. According to the aviation plug fixing device disclosed by the prior patent application CN201821073525.8, two hole sleeves are fixedly arranged on a bottom plate of the aviation plug connector tail clamp fixing device along the axial direction of the bottom plate, and then the aviation plug fixing device is installed on an aviation plug installation platform.
Disclosure of Invention
In view of the above, it is desirable to provide an insert connector fixing device.
The aviation plug connector fixing device comprises an aviation plug fixing tool and a connector, wherein the aviation plug fixing tool comprises an aviation plug fixing tool body, one side of the aviation plug fixing tool body is provided with an installation platform fixing hole, and the installation platform fixing hole is used for enabling the fixing tool body to be installed on an aviation plug platform; the fixed tool body is connected with the connector; the upper end of the connector is provided with a fixing pin, one side of the fixing tool body is provided with a fixing circular groove, and the fixing circular groove is matched with the fixing pin for use, so that the connector of the type can smoothly pass through the connector fixing tool of the type; the other side of the aviation plug fixing tool body is provided with a fixing square groove, the outer surface of a shell of the connector is fixedly provided with a connecting plate, a first threaded hole is formed in the fixing square groove, a second threaded hole is correspondingly formed in the connecting plate, and the first threaded hole is fixedly connected with the second threaded hole through a bolt; the connector and the locking bolt in the fixing tool ensure that the fixing tool fixes and protects the connector, the connector is prevented from being unstable in inclination to cause project failure, and the connector is efficiently and safely moved and placed.
Further, a steel wire thread sleeve is embedded in the first threaded hole.
Furthermore, the number of the fixing pins is 3, and the fixing pins are distributed at equal circumferential intervals.
Further, the fixed square groove is provided with chamfers, and the number of the chamfers is 4.
Furthermore, the mounting platform fixing hole is a blind hole.
The connector and the locking bolt in the fixing tool ensure that the fixing tool fixes and protects the connector, the connector is prevented from being unstable in inclination to cause project failure, and the connector is efficiently and safely moved and placed. The connector 3 further comprises a contact element, an insulator, a shell and the like, wherein the contact element is divided into a male contact element and a female contact element, the male contact element is a cylindrical rigid part (such as a round pin), the male contact element is made of brass, the female contact element (such as a jack) is a key part for ensuring the contact reliability, and the female contact element generates an elastic force when the plug pin is inserted by virtue of an elastic structure and is in close contact with the male contact element to complete the connection. The insulator has the function of arranging the contacts according to the required positions and intervals, ensures the insulating performance between the contacts and the shell, and has the basic requirements of selecting an insulating material processed into the insulator, such as good insulation resistance, good voltage resistance and good machinability. The housing houses an insulating mounting plate and pins to provide mechanical protection and alignment when the plug and socket are inserted to secure the connector to the device.
This aviation plug connector fixing device is through the quick matching of the fixed frock of aviation plug and connector, can install in arbitrary borehole jack on the platform according to the needs of project, need not consider space limitations such as line length planning and mounted position, can improve device's work efficiency like this, also be difficult for makeing mistakes.
Drawings
FIG. 1 is a schematic view of a connector securing apparatus;
fig. 2 is a schematic view of the fixing tool of the aviation plug connector fixing device;
fig. 3 is a schematic view of the connector of an aviation plug connector fixing device.
Detailed Description
To facilitate an understanding of the invention, the invention will now be described more fully with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
An aviation plug connector fixing device comprises an aviation plug fixing tool 1 and a connector 3, wherein the aviation plug fixing tool 1 comprises an aviation plug fixing tool body 2, one side of the aviation plug fixing tool body 2 is provided with an installation platform fixing hole 8, the installation platform fixing hole 8 is used for enabling the fixing tool body 2 to be aligned with a corresponding fixing hole position of an aviation plug installation platform, and then a screw is screwed on, and the screw provides positive pressure of the fixing hole 8 and the aviation plug installation platform hole position so that the fixing tool body can be fixedly installed on the aviation plug platform; the fixing tool 1 is connected with the connector 3; the connector is characterized in that a fixing pin 4 is arranged at the upper end of the connector 3, a fixing circular groove 6 is formed in one side of the fixing tool body 2, and the fixing circular groove 6 is matched with the fixing pin 4 for use, so that the connector smoothly passes through the fixing tool.
The number of the fixing pins 4 is 3, and the fixing pins are distributed at equal circumferential intervals.
A fixed square groove 7 is formed in the other side of the aviation plug fixing tool body 2; a connecting plate 5 is fixedly installed on the outer surface of the shell of the connector 3, a first threaded hole 9 is formed in the fixed square groove 7, a second threaded hole is correspondingly formed in the connecting plate 5, and the first threaded hole and the second threaded hole are fixedly connected through bolts; the connector and the locking bolt in the fixing tool ensure that the fixing tool fixes and protects the connector, the connector is prevented from being unstable in inclination to cause project failure, and the connector is efficiently and safely moved and placed. The connector 3 further comprises a contact element, an insulator, a shell and the like, wherein the contact element is divided into a male contact element and a female contact element, the male contact element is a cylindrical rigid part (such as a round pin), the male contact element is made of brass, the female contact element (such as a jack) is a key part for ensuring the contact reliability, and the female contact element generates an elastic force when the plug pin is inserted by virtue of an elastic structure and is in close contact with the male contact element to complete the connection. The insulator has the function of arranging the contacts according to the required positions and intervals, ensures the insulating performance between the contacts and the shell, and has the basic requirements of selecting an insulating material processed into the insulator, such as good insulation resistance, good voltage resistance and good machinability. The housing houses an insulating mounting plate and pins to provide mechanical protection and alignment when the plug and socket are inserted to secure the connector to the device.
The specific working principle is as follows. Firstly, inserting a connector 3 into a fixing tool 1, ensuring that a fixing pin 4 on the connector 3 corresponds to a fixing circular groove 6 in the inserting process, placing a connecting plate 5 on the outer surface of a shell of the connector 3 in a fixing square groove 7 of the fixing tool 1, aligning threaded holes of the fixing square groove and the threaded holes of. In the use, when concrete operations such as position adjustment are required at every turn, only need through platform fixed orifices 8 change the position can. The connector fixing device has the advantages that complex steps of matching the connector with a proper fixing tool and the like are eliminated, the aviation plug connector fixing device can be installed in any hole sleeve on the aviation plug platform according to the requirement of a project through the quick matching of the aviation plug fixing tool and the connector, space limitations such as line length planning and placement positions do not need to be considered, the working efficiency of the device can be improved, and errors are avoided.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (9)
1. The aviation plug connector fixing device is characterized by comprising an aviation plug fixing tool and a connector, wherein the aviation plug fixing tool comprises an aviation plug fixing tool body, one side of the aviation plug fixing tool body is provided with an installation platform fixing hole, and the installation platform fixing hole is used for enabling the fixing tool body to be installed on an aviation plug platform; the fixed tool body is connected with the connector; the upper end of the connector is provided with a fixing pin, one side of the fixing tool body is provided with a fixing circular groove, and the fixing circular groove is matched with the fixing pin for use, so that the connector of the type can smoothly pass through the connector fixing tool of the type; the other side of the aviation plug fixing tool body is provided with a fixing square groove, the outer surface of a shell of the connector is fixedly provided with a connecting plate, a first threaded hole is formed in the fixing square groove, a second threaded hole is correspondingly formed in the connecting plate, and the first threaded hole is fixedly connected with the second threaded hole through a bolt; the connector and the locking bolt in the fixing tool ensure that the fixing tool fixes and protects the connector, the connector is prevented from being unstable in inclination to cause project failure, and the connector is efficiently and safely moved and placed.
2. The aircraft connector securing device of claim 1, wherein a wire thread bushing is embedded in the first threaded bore.
3. The aviation plug connector fixing device according to claim 1, wherein the number of the fixing pins is 3, and the fixing pins are distributed at equal circumferential intervals.
4. The aviation plug connector fixing device according to claim 1, wherein the fixing square groove is provided with a chamfer, and the number of the fixing square grooves is 4.
5. The aircraft connector securing device of claim 1, wherein the mounting platform securing hole is a blind hole.
6. The aircraft connector securing device of claim 1, wherein the connector structure further comprises a contact, an insulator, and a housing.
7. The aircraft connector securing device according to claim 6, wherein the contact members are divided into male and female contact members.
8. The aircraft connector securing device according to claim 7, wherein the male contact is a round pin.
9. The aircraft connector securing device of claim 7, wherein the female contact is a receptacle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011483916.9A CN112713468B (en) | 2020-12-16 | 2020-12-16 | Aviation plug connector fixing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011483916.9A CN112713468B (en) | 2020-12-16 | 2020-12-16 | Aviation plug connector fixing device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112713468A true CN112713468A (en) | 2021-04-27 |
| CN112713468B CN112713468B (en) | 2022-07-12 |
Family
ID=75542206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011483916.9A Active CN112713468B (en) | 2020-12-16 | 2020-12-16 | Aviation plug connector fixing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112713468B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113363778A (en) * | 2021-06-21 | 2021-09-07 | 北京计算机技术及应用研究所 | Laser is warded off tin and is inserted fixing device by plane |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5417587A (en) * | 1993-01-22 | 1995-05-23 | Yazaki Corporation | Instrument directly mounted shielded connector |
| CN201623339U (en) * | 2009-08-12 | 2010-11-03 | 中国航空工业第六一八研究所 | Back-plate-free threaded flange connector |
| CN202050118U (en) * | 2011-05-10 | 2011-11-23 | 山东超越数控电子有限公司 | Novel waterproof aviation plug |
| CN203039161U (en) * | 2012-12-28 | 2013-07-03 | 成都市大富科技有限公司 | Connector fixing device and radio frequency component |
| CN203103689U (en) * | 2012-12-18 | 2013-07-31 | 古洪勇 | Connector |
| CN210779060U (en) * | 2019-10-24 | 2020-06-16 | 深圳市锐明技术股份有限公司 | Aviation head connector and connecting assembly |
-
2020
- 2020-12-16 CN CN202011483916.9A patent/CN112713468B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5417587A (en) * | 1993-01-22 | 1995-05-23 | Yazaki Corporation | Instrument directly mounted shielded connector |
| CN201623339U (en) * | 2009-08-12 | 2010-11-03 | 中国航空工业第六一八研究所 | Back-plate-free threaded flange connector |
| CN202050118U (en) * | 2011-05-10 | 2011-11-23 | 山东超越数控电子有限公司 | Novel waterproof aviation plug |
| CN203103689U (en) * | 2012-12-18 | 2013-07-31 | 古洪勇 | Connector |
| CN203039161U (en) * | 2012-12-28 | 2013-07-03 | 成都市大富科技有限公司 | Connector fixing device and radio frequency component |
| CN210779060U (en) * | 2019-10-24 | 2020-06-16 | 深圳市锐明技术股份有限公司 | Aviation head connector and connecting assembly |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113363778A (en) * | 2021-06-21 | 2021-09-07 | 北京计算机技术及应用研究所 | Laser is warded off tin and is inserted fixing device by plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112713468B (en) | 2022-07-12 |
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