CN201421877Y - Satellite communication antenna rapid locking fastener - Google Patents

Satellite communication antenna rapid locking fastener Download PDF

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Publication number
CN201421877Y
CN201421877Y CN2009200333790U CN200920033379U CN201421877Y CN 201421877 Y CN201421877 Y CN 201421877Y CN 2009200333790 U CN2009200333790 U CN 2009200333790U CN 200920033379 U CN200920033379 U CN 200920033379U CN 201421877 Y CN201421877 Y CN 201421877Y
Authority
CN
China
Prior art keywords
locking
groove
satellite communication
fixed seat
locking shaft
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
CN2009200333790U
Other languages
Chinese (zh)
Inventor
张勇
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.)
Shaanxi Kebo New Material Technology Co Ltd
Original Assignee
Shaanxi Kebo New Material 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 Shaanxi Kebo New Material Technology Co Ltd filed Critical Shaanxi Kebo New Material Technology Co Ltd
Priority to CN2009200333790U priority Critical patent/CN201421877Y/en
Application granted granted Critical
Publication of CN201421877Y publication Critical patent/CN201421877Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a satellite communication antenna rapid locking fastener, which comprises a left fixed seat 1 and a right fixed seat 3, wherein two positioning holes 2 are arranged at both ends of the left fixed seat 1, a locking hole 7 is arranged in the middle, a groove is arranged on the locking hole 7, two positioning pins 4 are arranged at the front end of the right fixed seat 3,a locking shaft 5 capable of moving back and forth is arranged in the middle of the right fixed seat 3, a groove is arranged at the front end of the locking shaft 5, and the locking shaft 5 is connected with a handle 6. The positioning pins 4 are inserted into the corresponding positioning holes 2, and the locking shaft 5 is rotated through the handle 6, so the groove and the groove are engaged with the locking shaft 5 and enter the locking hole 7; when the groove at the front end of the locking shaft 5 penetrates through the groove of the locking hole 7, then the handle 6 is rotated to drivethe locking shaft 5 to rotate, and the groove of the locking shaft 5 fastens the left fixed seat 1. The satellite communication antenna rapid locking fastener realizes rapid assembly and locking strength through the combination of double-pin positioning and cam locking mechanisms, and has the characteristics of simple operation and accurate positioning.

Description

The quick lock fastener of a kind of satellite communication antena
Technical field
The utility model relates to a kind of lock fastener, the quick lock fastener of particularly a kind of satellite communication antena.
Background technology
Existing antenna distinguish splicing connected mode is many, and connection speed is slow with being threaded, and positioning accuracy is poor, and bonding strength is low, the splicing intensity difference.
Summary of the invention
In order to overcome the characteristics of above-mentioned prior art, the purpose of this utility model is to provide a kind of satellite communication antena quick lock fastener, its locking mode adopts double-pin location, camlock principle, double-pin positioning accuracy height, and the camlock mode has quick locking function, in the assembling process of antenna, guarantee assembly precision and assembling speed like this, when emergency communication, more can bring into play the advantage of portable communication antenna.
In order to achieve the above object, the technical solution of the utility model is: the quick lock fastener of a kind of satellite communication antena, comprise left holder 1 and right holder 3, the two ends of left side holder 1 have 2 location holes 2, the centre has locking hole 7, the front end of right holder 3 is provided with 2 alignment pins 4, and the middle part of right holder 3 is provided with the lock shaft 5 that can move around, and is connected with handle 6 on the lock shaft 5.
Described locking hole 7 has groove.
The front end of described lock shaft 5 has tongue.
The utility model combines with cam lock holding mechanism by the double-pin location, has realized quick assembling and locking intensity, has characteristics simple to operate, accurate positioning.
Description of drawings
Accompanying drawing is a structure principle chart of the present utility model.
Embodiment
Below in conjunction with accompanying drawing structural principle of the present utility model and operation principle are described in detail.
With reference to accompanying drawing, the quick lock fastener of a kind of satellite communication antena, comprise left holder 1 and right holder 3, the two ends of left side holder 1 have 2 location holes 2, and the centre has locking hole 7, and locking hole 7 has groove, the front end of right holder 3 is provided with 2 alignment pins 4, the middle part of right holder 3 is provided with the lock shaft 5 that can move around, and lock shaft 5 front ends have tongue, are connected with handle 6 on the lock shaft 5.
Operation principle of the present utility model is: alignment pin 4 is inserted corresponding location hole 2, handle 6 rotation lock mandrels 5, make tongue and groove bitelock mandrel 5 enter locking hole 7, pass the groove of locking hole 7 when the tongue of lock shaft 5 front ends, then swing handle 6 drives lock shaft 5 rotations, and the tongue of lock shaft 5 fastens left holder 1.

Claims (3)

1, the quick lock fastener of a kind of satellite communication antena, it is characterized in that, comprise left holder (1) and right holder (3), the two ends of left side holder (1) have 2 location holes (2), the centre has locking hole (7), the front end of right holder (3) is provided with 2 alignment pins (4), and the middle part of right holder (3) is provided with the lock shaft (5) that can move around, and is connected with handle (6) on the lock shaft (5).
2, the quick lock fastener of a kind of satellite communication antena according to claim 1 is characterized in that, described locking hole (7) has groove.
3, the quick lock fastener of a kind of satellite communication antena according to claim 1 is characterized in that, the front end of described lock shaft (5) has tongue.
CN2009200333790U 2009-06-02 2009-06-02 Satellite communication antenna rapid locking fastener Expired - Fee Related CN201421877Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009200333790U CN201421877Y (en) 2009-06-02 2009-06-02 Satellite communication antenna rapid locking fastener

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009200333790U CN201421877Y (en) 2009-06-02 2009-06-02 Satellite communication antenna rapid locking fastener

Publications (1)

Publication Number Publication Date
CN201421877Y true CN201421877Y (en) 2010-03-10

Family

ID=41808539

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009200333790U Expired - Fee Related CN201421877Y (en) 2009-06-02 2009-06-02 Satellite communication antenna rapid locking fastener

Country Status (1)

Country Link
CN (1) CN201421877Y (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102544681A (en) * 2010-12-14 2012-07-04 中国航天科工集团第二研究院二十三所 Axial-locking device for radar antenna
CN105437111A (en) * 2015-12-22 2016-03-30 上海紫燕模具工业有限公司 Detachable module capable of rapidly locking
CN105552513A (en) * 2016-01-15 2016-05-04 江苏亨鑫无线技术有限公司 Structure capable of vertically fixing isolating bar on reflection plate
CN106563876A (en) * 2016-10-20 2017-04-19 南京君哲工业自动化有限公司 Roll spring electrode cap storage unit

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102544681A (en) * 2010-12-14 2012-07-04 中国航天科工集团第二研究院二十三所 Axial-locking device for radar antenna
CN105437111A (en) * 2015-12-22 2016-03-30 上海紫燕模具工业有限公司 Detachable module capable of rapidly locking
CN105552513A (en) * 2016-01-15 2016-05-04 江苏亨鑫无线技术有限公司 Structure capable of vertically fixing isolating bar on reflection plate
CN106563876A (en) * 2016-10-20 2017-04-19 南京君哲工业自动化有限公司 Roll spring electrode cap storage unit

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract

Assignee: Shannxi Tianyi Compound Material Co., Ltd.

Assignor: Shaanxi Kebo New Material Technology Co., Ltd.

Contract record no.: 2010610000015

Denomination of utility model: Satellite communication antenna rapid locking fastener

Granted publication date: 20100310

License type: Exclusive License

Record date: 20100430

DD01 Delivery of document by public notice

Addressee: Shaanxi Kebo New Material Technology Co., Ltd.

Document name: Notification to Pay the Fees

DD01 Delivery of document by public notice
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100310

Termination date: 20180602

CF01 Termination of patent right due to non-payment of annual fee