CN202103157U - Fastener for reinforcing carbon fiber satellite communication antenna boards - Google Patents
Fastener for reinforcing carbon fiber satellite communication antenna boards Download PDFInfo
- Publication number
- CN202103157U CN202103157U CN2011201902048U CN201120190204U CN202103157U CN 202103157 U CN202103157 U CN 202103157U CN 2011201902048 U CN2011201902048 U CN 2011201902048U CN 201120190204 U CN201120190204 U CN 201120190204U CN 202103157 U CN202103157 U CN 202103157U
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- CN
- China
- Prior art keywords
- lock
- hole
- lock core
- pin
- spring
- 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
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Abstract
The utility model relates to a fastener for reinforcing carbon fiber satellite communication antenna boards, which comprises a lock, a lock catch, a lock cylinder, a spring, a spring sleeve, a lock handle and a pin shaft for hinging. Both the lock and the lock catch are provided with a mounting surface and a lock cylinder hole, each mounting surface is provided with fixing holes, the lock cylinder holes are used for the lock cylinder to penetrate through, the lock is provided with a pair of positioning pins, the lock catch is provided with positioning pin holes corresponding to the positioning pins, the lock cylinder penetrates through the lock cylinders of the lock and the lock catch, one end of the lock cylinder is provided with a bolt for clamping the lock latch, the other of the lock cylinder is provided with a lock handle pin hole and is exposed out of the lock, the lock cylinder is positioned at one section, sleeved by the spring and the spring sleeve, in the lock, the head end of the lock handle is provided with a hinging head similar to a cam, and the hinging head is connected with the pin hole of the lock cylinder through the pin shaft. The fastener is capable of effectively reinforcing connection between among carbon fiber satellite communication antenna boards, and the reinforcing mode is reversible, reinforcement can be released as required and the fastener is convenient in mounting and demounting.
Description
Technical field
The utility model relates to a kind of securing member that is used for reinforcing carbon fiber satellite communication antena plate.
Background technology
Existing carbon fiber satellite communication antena plate usually is damaged owing to the connection between the antenna plate plate is insecure, and if make dead connection for very inconvenience of dismounting.
The utility model content
The technical problem that the utility model will solve is: a kind of securing member that is used for reinforcing carbon fiber satellite communication antena plate is provided, is used for the connection between the reinforcing carbon fiber satellite communication antena plate plate, simultaneously this reinforcing mode satisfy can convenient dismounting requirement.
The utility model solves the technical scheme that its technical problem adopted: a kind of securing member that is used for reinforcing carbon fiber satellite communication antena plate; It includes lock body, snap close, lock core, spring, spring housing, shank of the key and is used for hinged bearing pin, and lock body and snap close all have the installed surface of band fixing hole and the lock core hole that is used to place lock core, and lock body has a pair of alignment pin; Snap close then has and the corresponding dowel hole of alignment pin; Lock core connects the lock core hole of lock body and snap close, and an end of lock core has the dead bolt that blocks snap close, and the other end has the shank of the key pin-and-hole; The end that lock core has the shank of the key pin-and-hole exposes lock body; One section of being in the lock body of lock core is coated with spring and spring housing, and the head end of shank of the key has the hinge head of similar cam, and it is hinged that the pin-and-hole of hinge head and lock core passes through bearing pin.The lock body of this securing member, snap close use bolt and nut to be mounted to respectively on two adjacent antenna plate by the installed surface that respectively carries installing hole, can lock reinforcing to the adjacent antenna plate.The state of this securing member is divided into relaxed state and locking state.Under the relaxed state, separate fully under lock body and the effect that latches in spring, shank of the key is in upright state basically; Under the locking state, lock body and snap close are adjacent to, and a pair of alignment pin of lock body inserts in the dowel hole in the snap close fully, and this moment, shank of the key was in level basically.The all-pass that converts of lax and two states of locking of this securing member is crossed the realization of switching shank of the key.
The beneficial effect of the utility model is: this is used for the securing member connection between the reinforcing carbon fiber satellite communication antena plate plate effectively of reinforcing carbon fiber satellite communication antena plate; And this reinforcing mode is a reversible; Can remove reinforcing when promptly needing, dismounting is very convenient.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the utility model is described further.
Fig. 1 is the assembly structure sketch map (dotted line representes to assemble annexation) of the utility model.
Among the figure: 1. lock body 1-1. alignment pin 2. snap closes 3. lock core 3-1. dead bolt 3-2. shank of the key pin-and-holes 4. springs 5. spring housings 6. shank of the key 6-1. cut with scissors 7. bearing pin
Embodiment
A kind of securing member that is used for reinforcing carbon fiber satellite communication antena plate, as shown in Figure 1, it includes lock body 1, snap close 2, lock core 3, spring 4, spring housing 5, shank of the key 6 and is used for hinged bearing pin 7; Lock body 1 all has the installed surface of band fixing hole and the lock core hole that is used to place lock core with snap close 2; Lock body 1 has a pair of alignment pin 1-1, and 2 of snap closes have the corresponding dowel hole with alignment pin 1-1, and lock core 3 connects the lock core hole of lock body 1 and snap close 2; One end of lock core 3 has the dead bolt 3-1 that blocks snap close 2; The other end has shank of the key pin-and-hole 3-2, and the end that lock core 3 has shank of the key pin-and-hole 3-2 exposes lock body 1, and lock core 3 is in the lock body 1 one section and is coated with spring 4 and spring housing 5; The head end of shank of the key 6 has a hinge 6-1 of similar cam, and the shank of the key pin-and-hole 3-2 of a hinge 6-1 and lock core 3 is hinged through bearing pin 7.
The lock body 1 of this securing member, snap close 2 use bolt and nut to be mounted to respectively on two adjacent antenna plate by the installed surface that respectively carries installing hole, can lock reinforcing to the adjacent antenna plate.The state of this securing member is divided into relaxed state and locking state.Under the relaxed state, lock body 1 separates under the effect of spring 4 with snap close 2 fully, and shank of the key 6 is in upright state basically; Under the locking state, lock body 1 is adjacent to snap close 2, and a pair of alignment pin 1-1 of lock body 1 inserts in the dowel hole in the snap close 2 fully, and this moment, shank of the key 6 was in level basically.The all-pass that converts of lax and two states of locking of this securing member is crossed 6 realizations of switching shank of the key.
Claims (1)
1. securing member that is used for reinforcing carbon fiber satellite communication antena plate; It is characterized in that: include lock body (1), snap close (2), lock core (3), spring (4), spring housing (5), shank of the key (6) and be used for hinged bearing pin (7); Lock body (1) all has the installed surface of band fixing hole and the lock core hole that is used to place lock core with snap close (2); Lock body (1) has a pair of alignment pin (1-1), and snap close (2) then has and the corresponding dowel hole of alignment pin (1-1), and lock core (3) connects the lock core hole of lock body (1) and snap close (2); One end of lock core (3) has the dead bolt (3-1) that blocks snap close (2); The other end has shank of the key pin-and-hole (3-2), and the end that lock core (3) has shank of the key pin-and-hole (3-2) exposes lock body (1), and lock core (3) is in the lock body (1) one section and is coated with spring (4) and spring housing (5); The head end of shank of the key (6) has the hinge head (6-1) of similar cam, and hinge head (6-1) is hinged through bearing pin (7) with the pin-and-hole (3-2) of lock core (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201902048U CN202103157U (en) | 2011-06-08 | 2011-06-08 | Fastener for reinforcing carbon fiber satellite communication antenna boards |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011201902048U CN202103157U (en) | 2011-06-08 | 2011-06-08 | Fastener for reinforcing carbon fiber satellite communication antenna boards |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202103157U true CN202103157U (en) | 2012-01-04 |
Family
ID=45389157
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011201902048U Expired - Fee Related CN202103157U (en) | 2011-06-08 | 2011-06-08 | Fastener for reinforcing carbon fiber satellite communication antenna boards |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202103157U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105020217A (en) * | 2015-07-27 | 2015-11-04 | 湖州佳宁印刷有限公司 | Rapid connection device |
| CN109139633A (en) * | 2018-09-04 | 2019-01-04 | 王付华 | It is a kind of for space flight, the snap close piece of aviation field |
-
2011
- 2011-06-08 CN CN2011201902048U patent/CN202103157U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105020217A (en) * | 2015-07-27 | 2015-11-04 | 湖州佳宁印刷有限公司 | Rapid connection device |
| CN109139633A (en) * | 2018-09-04 | 2019-01-04 | 王付华 | It is a kind of for space flight, the snap close piece of aviation field |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20120104 Termination date: 20180608 |