CN205004523U - Satellite antenna joint design - Google Patents
Satellite antenna joint design Download PDFInfo
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- CN205004523U CN205004523U CN201520707725.4U CN201520707725U CN205004523U CN 205004523 U CN205004523 U CN 205004523U CN 201520707725 U CN201520707725 U CN 201520707725U CN 205004523 U CN205004523 U CN 205004523U
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- Prior art keywords
- satellite antenna
- joint
- water
- fixed
- nut
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Abstract
The utility model discloses a satellite antenna joint design, including fixed establishment and coupling mechanism, fixed establishment be fixed in on the satellite antenna chassis, coupling mechanism be connected with fixed establishment.
Description
Technical field
The utility model relates to a kind of jockey of satellite antenna, specifically a kind of satellite antenna joint design.
Background technology
Current structure adopts increase waterproof O shape circle in F head (F head AN connector is applicable to the connection of coaxial cable) to increase protectiveness; but what adopt between cable and joint is that screw-type close-fitting or fashion of extrusion close-fitting are to reach the effect of waterproof; service time one is long; cable sheath is easily elongated and fluffs, and loses waterproof effect and causes cable to be intake.
Utility model content
The purpose of this utility model is to provide a kind of satellite antenna joint design.
What the utility model solved is more existing adopt between cable and joints be screw-type close-fitting or fashion of extrusion close-fitting to reach the effect of waterproof, service time one is long, and cable sheath is easily elongated and fluffs, and loses waterproof effect and causes cable to enter water problem.
The technical scheme that the utility model technical solution problem adopts is: this device mainly comprises fixed mechanism and bindiny mechanism, and described fixed mechanism is fixed on satellite antenna chassis, and described bindiny mechanism is connected with fixed mechanism.
Described fixed mechanism comprises F head (F head AN connector is applicable to the connection of coaxial cable), the first nut, water joint seat and the second nut, described water joint seat is fixed on satellite antenna chassis by the first nut, it is inner that the first end of described F is placed in water joint seat, fixed by the second nut.
Pad is provided with between described water joint seat and outside, satellite antenna chassis.
Described bindiny mechanism comprises water string, attaching nut and coaxial line joint, and one end of described coaxial line joint is placed in water string one end, and described attaching nut is located at water string outside.
Sealing ring is provided with between described coaxial line joint and water string.
Described bindiny mechanism is connected with water joint seat by attaching nut, thus bindiny mechanism is connected with fixed mechanism.
Gasket seal is provided with between described coaxial line joint and water joint seat.
After described bindiny mechanism is connected with fixed mechanism, its coaxial line joint external end head and F head external end head are connected.
The beneficial effects of the utility model are: have the degree of protection that excellent water resistance linker can reach IP68, greatly extend the useful life of outdoor coaxial cable, and install and connect simply, lock-on connection is without the need to using instrument.
Accompanying drawing explanation
Fig. 1 is the decomposing schematic representation of mounting structure of the present utility model.
Fig. 2 is internal structure schematic diagram of the present utility model.
Embodiment
Below in conjunction with drawings and Examples, the utility model is described in further detail.
As shown in the figure: the utility model comprises fixed mechanism and bindiny mechanism, described fixed mechanism is fixed on satellite antenna chassis 10, and described bindiny mechanism is connected with fixed mechanism.
Described fixed mechanism comprises the connection that F head 11(F head AN connector is applicable to coaxial cable), the first nut 9, water joint seat 7 and the second nut 6, described water joint seat 7 is fixed on satellite antenna chassis 10 by the first nut 9, it is inner that F described 11 one end are placed in water joint seat 7, fixed by the second nut 6.
Pad 8 is provided with between described water joint seat 7 and outside, satellite antenna chassis 10.
Described bindiny mechanism comprises water string 1, attaching nut 3 and coaxial line joint 4, and one end of described coaxial line joint 4 is placed in water string 1 one end, and it is outside that described attaching nut 3 is located at water string 1.
Sealing ring 2 is provided with between described coaxial line joint 4 and water string 1.
Described bindiny mechanism is connected with water joint seat 7 by attaching nut 3, thus bindiny mechanism is connected with fixed mechanism.
Gasket seal 5 is provided with between described coaxial line joint 4 and water joint seat 7.
After described bindiny mechanism is connected with fixed mechanism, its coaxial line joint 4 external end head and F 11 external end heads are connected.
Claims (6)
1. a satellite antenna joint design, is characterized in that comprising fixed mechanism and bindiny mechanism, and described fixed mechanism is fixed on satellite antenna chassis, and described bindiny mechanism is connected with fixed mechanism;
Described fixed mechanism comprises F head, the first nut, water joint seat and the second nut, and described water joint seat is fixed on satellite antenna chassis by the first nut, and it is inner that the first end of described F is placed in water joint seat, fixed by the second nut;
Described bindiny mechanism comprises water string, attaching nut and coaxial line joint, and one end of described coaxial line joint is placed in water string one end, and described attaching nut is located at water string outside.
2. a kind of satellite antenna joint design according to claim 1, is characterized in that being provided with pad between described water joint seat and outside, satellite antenna chassis.
3. a kind of satellite antenna joint design according to claim 1, is characterized in that being provided with sealing ring between described coaxial line joint and water string.
4. a kind of satellite antenna joint design according to claim 1, is characterized in that described bindiny mechanism is connected with water joint seat by attaching nut, thus bindiny mechanism is connected with fixed mechanism.
5. a kind of satellite antenna joint design according to claim 1, is characterized in that being provided with gasket seal between described coaxial line joint and water joint seat.
6. a kind of satellite antenna joint design according to claim 1, after it is characterized in that described bindiny mechanism is connected with fixed mechanism, its coaxial line joint external end head and F head external end head are connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520707725.4U CN205004523U (en) | 2015-09-14 | 2015-09-14 | Satellite antenna joint design |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520707725.4U CN205004523U (en) | 2015-09-14 | 2015-09-14 | Satellite antenna joint design |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205004523U true CN205004523U (en) | 2016-01-27 |
Family
ID=55161395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520707725.4U Active CN205004523U (en) | 2015-09-14 | 2015-09-14 | Satellite antenna joint design |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205004523U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105119092A (en) * | 2015-09-14 | 2015-12-02 | 嘉兴星网通信技术有限公司 | Satellite antenna connector structure |
| CN109149050A (en) * | 2018-08-01 | 2019-01-04 | 苏州频聿精密机械有限公司 | A kind of satellite antenna joint structure |
-
2015
- 2015-09-14 CN CN201520707725.4U patent/CN205004523U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105119092A (en) * | 2015-09-14 | 2015-12-02 | 嘉兴星网通信技术有限公司 | Satellite antenna connector structure |
| CN105119092B (en) * | 2015-09-14 | 2018-01-30 | 嘉兴星网通信技术有限公司 | Satellite antenna joint design |
| CN109149050A (en) * | 2018-08-01 | 2019-01-04 | 苏州频聿精密机械有限公司 | A kind of satellite antenna joint structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |