CN204088548U - A kind of Portable satellite aerial - Google Patents
A kind of Portable satellite aerial Download PDFInfo
- Publication number
- CN204088548U CN204088548U CN201420610498.9U CN201420610498U CN204088548U CN 204088548 U CN204088548 U CN 204088548U CN 201420610498 U CN201420610498 U CN 201420610498U CN 204088548 U CN204088548 U CN 204088548U
- Authority
- CN
- China
- Prior art keywords
- feed
- adjusting mechanism
- portable satellite
- strut
- fixed head
- 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 discloses a kind of Portable satellite aerial, the reflecting surface comprising base and be made up of multiple dismountable reflecting plate, base comprises chassis, pitching adjusting mechanism position adjusting mechanism and fixed head; Chassis is made up of upper and lower two pieces of disks, lower disc is connected with bracing or strutting arrangement, in the middle of upper and lower two disks, gear train and ball are installed, upper disk is provided with position adjusting mechanism, the pinion engaged with gear train is installed below position adjusting mechanism, upper disk is provided with fixed head, reflecting surface is all connected by rotating shaft with fixed head with feed strut, feed strut is connected with feed, pitching adjusting mechanism one end is slidably connected on feed strut, one end can be automatically connected on disk, is connected between reflecting surface with feed strut by feed brace.This Portable satellite aerial, it adopts Split type structure, compact conformation, stablizes, removes and installs conveniently, and volume is little, lightweight, easy to carry.
Description
Technical field
The utility model belongs to technical field of satellite communication, relates to a kind of Portable satellite aerial.
Background technology
In the epoch of communication globalization, satellite communication is large and communication efficiency high with its wide coverage, message capacity, occupies irreplaceable critical role in the communications field.In the area that the existing satellite communication networks such as outlying mountain area can't cover at present, if during burst major event, when original GCF ground communication facility is seriously damaged and paralyses, unimpeded in order to ensure the commander that effectively speedily carries out rescue work, news collection or other important communication, portable satellite communication system arises at the historic moment, and is used widely.Wherein Portable satellite communication antenna is exactly the core of system.So-called portable, namely to be convenient to dismounting, install and transport.These factors are to the structure of antenna, and integrated level is had higher requirement.
Utility model content
The utility model, in order to solve the problems of the technologies described above, provides a kind of portable Portable satellite aerial, installs under being convenient to dismounting and heeling condition.
The utility model is achieved through the following technical solutions:
A kind of Portable satellite aerial, the reflecting surface comprising base, feed, bracing or strutting arrangement, feed strut, feed brace and be made up of multiple dismountable reflecting plate, described base comprises chassis, pitching adjusting mechanism position adjusting mechanism and fixed head; Chassis is made up of upper and lower two pieces of disks, lower disc is connected with bracing or strutting arrangement, in the middle of upper and lower two disks, gear train and ball are installed, upper disk is provided with position adjusting mechanism, the pinion engaged with gear train is installed below position adjusting mechanism, upper disk is provided with fixed head, reflecting surface is all connected by rotating shaft with fixed head with feed strut, feed strut is connected with feed, pitching adjusting mechanism one end is slidably connected on feed strut, one end can be automatically connected on disk, is connected between reflecting surface with feed strut by feed brace.
Described base is also provided with level meter and compass.
Described bracing or strutting arrangement comprises support leg, and described support leg one end and the lower disc of base are bolted, and the other end has screwed hole, is provided with screw rod in screwed hole.
Described reflecting surface comprises six reflecting plates, and a slice reflecting plate back side is provided with backrest, and connected by snap close between other reflecting plate, backrest is connected by rotating shaft with fixed head.
Its front of reflecting plate that the back side is provided with backrest is fixed with bearing pin plate, and feed strut is also provided with bearing pin plate, and feed brace is connected with the bearing pin plate on reflecting plate and feed strut.
Have groove in the middle of feed strut, pitching adjusting mechanism one end is connected in groove by pin slide.
Pitching dial is flexibly connected with fixed head by rotating shaft.
Compared with prior art, the utility model has following useful technique effect:
The Portable satellite aerial that the utility model provides, it adopts Split type structure, and compact conformation, stable, integrated level is high, and remove and install conveniently, volume is little, lightweight, easy to carry.
Accompanying drawing explanation
The Portable satellite aerial structural representation one that Fig. 1 provides for the utility model;
The Portable satellite aerial structural representation two that Fig. 2 provides for the utility model;
The reflecting surface structure schematic diagram of the Portable satellite aerial that Fig. 3 provides for the utility model;
The Portable satellite aerial structural representation three that Fig. 4 provides for the utility model.
Wherein: 1 is base; 2 is reflecting surface; 3 is support leg; 4 is feed strut; 5 is feed brace; 6 is feed; 7 is pitching adjusting mechanism; 8 is position adjusting mechanism; 9 is fixed head; 10 is level meter; 11 is compass; 12 is backrest; 13 is snap close; 14 is rotating shaft; 15 is bearing pin plate; 16 is screw rod; 17 is groove; 18 is bearing pin; 19 is pitching dial; 20 is chassis.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail:
See Fig. 1 to Fig. 4, a kind of Portable satellite aerial, the reflecting surface 2 comprising base 1, feed 6, bracing or strutting arrangement, feed strut 4, feed brace 5 and be made up of multiple dismountable reflecting plate, described base 1 comprises chassis 20, pitching adjusting mechanism 7, position adjusting mechanism 8 and fixed head 9, chassis 20 is made up of upper and lower two pieces of disks, lower disc is connected with support leg 3 one end by bolt, support leg 3 other end has screwed hole, screw rod 16 is installed in screwed hole, in the middle of upper and lower two disks, gear train and ball are installed, upper disk is provided with position adjusting mechanism 8, position adjusting mechanism 8 is provided with the pinion engaged with gear train below, upper disk is provided with fixed head 9, reflecting surface 2, pitching dial 19 and feed strut 4 are all movably connected by rotating shaft 14 with fixed head 9, feed strut 4 is connected with feed 6, groove 17 is had in the middle of feed strut 4, pitching adjusting mechanism 7 one end is slidably connected in the groove 17 of feed strut 4 by bearing pin 18, one end can be automatically connected on disk, be connected by feed brace 5 between reflecting surface 2 with feed strut 4, described base 1 is also provided with level meter 10 and compass 11.
Concrete, described reflecting surface 2 comprises six reflecting plates, a slice reflecting plate back side is provided with backrest 12, front is fixed with bearing pin plate 15, connected by snap close 13 between other reflecting plate, backrest 12 is connected by rotating shaft 14 with the fixed head 9 of base, simultaneously, feed strut is also provided with bearing pin plate 15, and feed brace 5 is connected with the bearing pin plate 15 on reflecting plate and feed strut 4.
Wherein, because chassis 20 is made up of upper and lower two pieces of disks, below that disk with support leg be connected.In the middle of upper and lower two disks, gear train and ball are installed, a pinion is installed below position adjusting mechanism, so in time turning position adjusting mechanism 8, the bull gear drive in pinion driven gear group, disk above will rotate, and just can regulate the rotational angle of disk.
The utility model is installed under being convenient to dismounting and heeling condition, and is easy to carry.
More than show and describe general principle of the present utility model and principal character and advantage of the present utility model.The technical staff of the industry should understand; the utility model is not restricted to the described embodiments; what describe in above-described embodiment and specification just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (7)
1. a Portable satellite aerial, it is characterized in that, the reflecting surface (2) comprising base (1), feed (6), bracing or strutting arrangement, feed strut (4), feed brace (5) and be made up of multiple dismountable reflecting plate, described base (1) comprises chassis (20), pitching adjusting mechanism (7), position adjusting mechanism (8) and fixed head (9), chassis (20) is made up of upper and lower two pieces of disks, lower disc is connected with bracing or strutting arrangement, in the middle of upper and lower two disks, gear train and ball are installed, upper disk is provided with position adjusting mechanism (8), position adjusting mechanism (8) is provided with the pinion engaged with gear train below, upper disk is provided with fixed head (9), reflecting surface (2) is all connected by rotating shaft (14) with fixed head (9) with feed strut (4), feed strut (4) is connected with feed (6), pitching adjusting mechanism (7) one end is slidably connected on feed strut (4), one end can be automatically connected on disk, be connected by feed brace (5) between reflecting surface (2) with feed strut (4).
2. Portable satellite aerial according to claim 1, is characterized in that, described base (1) is also provided with level meter (10) and compass (11).
3. Portable satellite aerial according to claim 1, it is characterized in that, described bracing or strutting arrangement comprises support leg (3), described support leg (3) one end and the lower disc of base are bolted, the other end has screwed hole, is provided with screw rod (16) in screwed hole.
4. Portable satellite aerial according to claim 1, it is characterized in that, described reflecting surface (2) comprises six reflecting plates, a slice reflecting plate back side is provided with backrest (12), connected by snap close (13) between other reflecting plate, backrest (12) is connected by rotating shaft (14) with fixed head (9).
5. Portable satellite aerial according to claim 1, it is characterized in that, its front of reflecting plate that the back side is provided with backrest (12) is fixed with bearing pin plate (15), feed strut is also provided with bearing pin plate (15), feed brace (5) is connected with the bearing pin plate (15) on reflecting plate and feed strut (4).
6. Portable satellite aerial according to claim 1, it is characterized in that, have groove (17) in the middle of feed strut (4), pitching adjusting mechanism (7) one end is slidably connected in groove (17) by bearing pin (18).
7. Portable satellite aerial according to claim 1, is characterized in that, pitching dial (19) is flexibly connected with fixed head (9) by rotating shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420610498.9U CN204088548U (en) | 2014-10-21 | 2014-10-21 | A kind of Portable satellite aerial |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420610498.9U CN204088548U (en) | 2014-10-21 | 2014-10-21 | A kind of Portable satellite aerial |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204088548U true CN204088548U (en) | 2015-01-07 |
Family
ID=52181223
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420610498.9U Expired - Fee Related CN204088548U (en) | 2014-10-21 | 2014-10-21 | A kind of Portable satellite aerial |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204088548U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104802690A (en) * | 2015-04-17 | 2015-07-29 | 苏州携旅网络技术有限公司 | Mobile emergency communication device |
| CN105305012A (en) * | 2015-12-02 | 2016-02-03 | 湖南创智数码科技股份有限公司 | Satellite portable station |
| CN112397871A (en) * | 2020-10-22 | 2021-02-23 | 广东盛路通信科技股份有限公司 | Microwave antenna structure capable of controlling and adjusting |
-
2014
- 2014-10-21 CN CN201420610498.9U patent/CN204088548U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104802690A (en) * | 2015-04-17 | 2015-07-29 | 苏州携旅网络技术有限公司 | Mobile emergency communication device |
| CN105305012A (en) * | 2015-12-02 | 2016-02-03 | 湖南创智数码科技股份有限公司 | Satellite portable station |
| CN112397871A (en) * | 2020-10-22 | 2021-02-23 | 广东盛路通信科技股份有限公司 | Microwave antenna structure capable of controlling and adjusting |
| CN112397871B (en) * | 2020-10-22 | 2023-12-01 | 广东盛路通信科技股份有限公司 | Microwave antenna structure capable of being controlled and adjusted |
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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 |
Granted publication date: 20150107 Termination date: 20151021 |
|
| EXPY | Termination of patent right or utility model |