CN204021261U - Multi-functional integrated mast installation - Google Patents
Multi-functional integrated mast installation Download PDFInfo
- Publication number
- CN204021261U CN204021261U CN201420336959.8U CN201420336959U CN204021261U CN 204021261 U CN204021261 U CN 204021261U CN 201420336959 U CN201420336959 U CN 201420336959U CN 204021261 U CN204021261 U CN 204021261U
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- output shaft
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- 238000009434 installation Methods 0.000 title claims abstract description 33
- 230000007246 mechanism Effects 0.000 claims abstract description 93
- 230000003028 elevating effect Effects 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 3
- 230000000007 visual effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
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Abstract
The utility model provides a kind of multi-functional integrated mast installation, comprise development mechanism, output frame, Yawing mechanism, antenna mechanism, luffing mechanism and phase machine mechanism, the output shaft of development mechanism is connected with output frame and can drives output frame to rotate, output frame is connected with Yawing mechanism, the output shaft of Yawing mechanism is connected with antenna mechanism and can drives antenna mechanism to rotate, the output shaft of Yawing mechanism is connected with luffing mechanism and can drives luffing mechanism to rotate, and the output shaft of luffing mechanism is connected with phase machine mechanism and can drives phase machine mechanism to rotate.Compared with prior art, the utility model by arrange three active driving mechanisms guaranteed to mediate the directional antenna at position and the pitching of the camera in top, yawing rotation and repeatedly launch, gathering demand, inner in U character form structure while meet drawing transmitting in, directional antenna and camera possess the requirement of certain altitude while organizing work, and lightweight, power consumption is little, profile envelope is little.
Description
Technical field
The utility model relates to a kind of three-dimensional for equipment such as directional antenna, cameras and launches, draws in mast installation, particularly a kind of multi-functional integrated mast installation.
Background technology
At present, satellite or deep space probe adopt a bidimensional driver train to realize pitching and the yaw angle location of directional antenna conventionally, adopt another pitching and yaw angle location that independently bidimensional driver train is realized camera.But there is following defect:
(1), owing to adopting two to overlap independently bidimensional driver train, cause that whole star weight is large, power consumption is large, and profile envelope is large;
(2) for adapting to the requirement of shaded area or low temperature storage, mast installation should meet repeatedly draws requirement in, can draw in the structure space of closed cube envelope by instruction; During operation on orbit, mast should meet directional antenna hemisphere and point to requirement to covering, and should meet the visual field requirement of four cameras, and conventional mast installation cannot be carried out inverse operation or repeatedly launch, draw in operation.
Utility model content
The utility model object is to provide a kind of multi-functional integrated mast installation, to solve mast installation of the prior art owing to adopting two to overlap independently bidimensional driver train, causes that whole star weight is large, power consumption is large, and the large technical matters of profile envelope.
The utility model object realizes by following technical scheme:
A kind of multi-functional integrated mast installation, comprise development mechanism, output frame, Yawing mechanism, antenna mechanism, luffing mechanism and phase machine mechanism, the output shaft of described development mechanism is connected with described output frame and can drives described output frame to rotate, described output frame is connected with described Yawing mechanism, the output shaft of described Yawing mechanism is connected with described antenna mechanism and can drives described antenna mechanism to rotate, the output shaft of described Yawing mechanism is connected with described luffing mechanism and can drives described luffing mechanism to rotate, the output shaft of described luffing mechanism is connected with described phase machine mechanism and can drives described phase machine mechanism to rotate.
Preferably, also comprise elevating base, described development mechanism is arranged on described elevating base.
Preferably, described development mechanism comprises drive motor I and reductor I, and the output shaft of described drive motor I is connected with described reductor I, and the output shaft of described drive motor I is fixedly connected with described output frame.
Preferably, the output shaft of described drive motor I is connected by set pin with described output frame.
Preferably, described output frame is " Z " font.
Preferably, described Yawing mechanism comprises housing II, drive motor II and reductor II, described drive motor II and described reductor II are arranged in described housing II, and described output frame is fixedly connected with described housing II, and the output shaft of described drive motor II is connected with described reductor II.
Preferably, described antenna mechanism comprises aerial bracket I, aerial bracket II and directional antenna, described directional antenna is fixedly connected with described aerial bracket I, described aerial bracket II respectively, and the output shaft of described drive motor II is fixedly connected with described aerial bracket I, described directional antenna and described aerial bracket II successively.
Preferably, described luffing mechanism comprises housing III, drive motor III and reductor III, described drive motor III and described reductor III are arranged in described housing III, the output shaft of described drive motor II is fixedly connected with described housing III, and the output shaft of described drive motor III is connected with described reductor III.
Preferably, described phase machine mechanism comprises camera support and some cameras, and described some cameras are fixedly installed on described camera support, and the output shaft of described drive motor III is fixedly connected with described camera support.
Preferably, the output shaft of described drive motor III is connected by set pin with described camera support.
Compared with prior art, the utility model has following beneficial effect:
1, the utility model by arrange three active driving mechanisms guaranteed to mediate the directional antenna at position and the pitching of the camera in top, yawing rotation and repeatedly launch, gathering demand, and lightweight, power consumption is little, profile envelope is little;
2, the utility model is raised development mechanism by elevating base is set, while guaranteeing mast deployed condition, camera possesses certain height, meet the visual field requirement of camera, simultaneously, development mechanism is raised the rear range of movement that has increased development mechanism and Yawing mechanism, has guaranteed that directional antenna hemisphere points to covering;
3, the utility model reduces the position of directional antenna and camera by " Z " font output frame, thereby while guaranteeing mast rounding state, whole mast installation is drawn envelope in the U of celestial body character form structure interior volume, meet product space dimensional restriction, the demand of thermal control while realizing shaded area or low temperature storage, thus guarantee that whole mast installation meets the demand of drawing envelope in.
Certainly, implement arbitrary product of the present utility model and might not need to reach above-described all advantages simultaneously.
Accompanying drawing explanation
Fig. 1 is the rounding state lateral plan of multi-functional integrated mast installation of the present utility model;
Fig. 2 is the rounding state birds-eye view of multi-functional integrated mast installation of the present utility model;
Fig. 3 is the expansion campaign schematic diagram of multi-functional integrated mast installation of the present utility model;
Fig. 4 is the yawing rotation schematic diagram of multi-functional integrated mast installation of the present utility model;
Fig. 5 is the luffing schematic diagram of multi-functional integrated mast installation of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing, describe the utility model in detail.
Refer to Fig. 1,2, multi-functional integrated mast installation of the present utility model, comprise development mechanism 1, output frame 9, Yawing mechanism 2, antenna mechanism, luffing mechanism 3 and phase machine mechanism, the output shaft of development mechanism 1 is connected with output frame 9 and can drives output frame 9 to rotate, output frame 9 is connected with Yawing mechanism 2, the output shaft of Yawing mechanism 2 is connected with antenna mechanism and can drives antenna mechanism to rotate, the output shaft of Yawing mechanism 2 is connected with luffing mechanism 3 and can drives luffing mechanism 3 to rotate, and the output shaft of luffing mechanism 3 is connected with phase machine mechanism and can drives phase machine mechanism to rotate.The utility model by arrange three active driving mechanisms guaranteed to mediate the directional antenna at position and the pitching of the camera in top, yawing rotation and repeatedly launch, gathering demand, and lightweight, power consumption is little, profile envelope is little.
In this example, multi-functional integrated mast installation of the present utility model also comprises elevating base 10, and development mechanism 1 is arranged on elevating base 10.Elevating base 10 is fixed by screws in celestial body structure.The utility model is raised development mechanism by elevating base is set, while guaranteeing mast deployed condition, camera possesses certain height, meet the visual field requirement of camera, simultaneously, development mechanism is raised the rear range of movement that has increased development mechanism and Yawing mechanism, has guaranteed that directional antenna hemisphere points to covering.
In this example, development mechanism 1 comprises drive motor I and reductor I, the output shaft of drive motor I is connected with reductor I, and the output shaft of drive motor I is fixedly connected with by set pin with one end of output frame 9, and the output shaft of drive motor I can drive output frame 9 to rotate.
In this example, Yawing mechanism 2 comprises housing II, drive motor II and reductor II, and drive motor II and reductor II are arranged in housing II, and output frame 9 is fixedly connected with by screw with housing II, and the output shaft of drive motor II is connected with reductor II.
In this example, output frame is " Z " font.The utility model reduces the position of directional antenna and camera by " Z " font output frame, thereby while guaranteeing mast rounding state, whole mast installation is drawn envelope in the U of celestial body character form structure interior volume, meet product space dimensional restriction, the demand of thermal control while realizing shaded area or low temperature storage, thus guarantee that whole mast installation meets the demand of drawing envelope in.
In this example, antenna mechanism comprises aerial bracket I8, aerial bracket II7 and directional antenna 4, directional antenna 4 is fixedly connected with aerial bracket I8, aerial bracket II7 respectively, and the output shaft of drive motor II is fixedly connected with by screw with aerial bracket I8, directional antenna 4 and aerial bracket II7 successively.The output shaft of drive motor II can drive aerial bracket I8, directional antenna 4 and aerial bracket II7 to rotate.
In this example, luffing mechanism 3 comprises housing III, drive motor III and reductor III, drive motor III and reductor III are arranged in housing III, and the output shaft of drive motor II is fixedly connected with by screw with housing III, and the output shaft of drive motor III is connected with reductor III.
In this example, phase machine mechanism comprises camera support 6 and some cameras 5, and some cameras 5 are fixedly installed on camera support 6 by screw, and the output shaft of drive motor III is fixedly connected with by set pin with camera support 6.
When in off working state, multi-functional integrated mast installation of the present utility model is in rounding state, as shown in Figure 1.In the time will carrying out work, first by drive motor I, make the output shaft rotation of drive motor I, thereby drive 9 rotations of output frame to make to export frame 9 and turn to suitable position, thereby drive directional antenna to realize the motion positions of-112 °～+ 90 ° of pitch orientation, as shown in Figure 3; By drive motor II, make again the output shaft rotation of drive motor II, thereby driving directional antenna 4 to rotate makes directional antenna 4 turn to suitable position, thereby drive directional antenna to realize the motion positions of-178.5 °～+ 178.5 ° of yaw directions, thereby realize the bidimensional driving control that directional antenna refers to ground communication transfer, as shown in Figure 4; Finally by drive motor III, make the output shaft rotation of drive motor III, thereby driving camera support 6 to rotate makes camera support 6 turn to suitable position, thereby drive camera to realize the motion positions of-78 °～+ 90 ° of pitch orientation, thereby driving, the bidimensional of realizing camera imaging controls, as shown in Figure 5.When not working, reversing sense drives each drive motor can make multi-functional integrated mast installation in rounding state.
Disclosed is above only several specific embodiments of the application, but the application is not limited thereto, and the changes that any person skilled in the art can think of, all should drop in the application's protection domain.
Claims (10)
1. a multi-functional integrated mast installation, it is characterized in that, comprise development mechanism, output frame, Yawing mechanism, antenna mechanism, luffing mechanism and phase machine mechanism, the output shaft of described development mechanism is connected with described output frame and can drives described output frame to rotate, described output frame is connected with described Yawing mechanism, the output shaft of described Yawing mechanism is connected with described antenna mechanism and can drives described antenna mechanism to rotate, the output shaft of described Yawing mechanism is connected with described luffing mechanism and can drives described luffing mechanism to rotate, the output shaft of described luffing mechanism is connected with described phase machine mechanism and can drives described phase machine mechanism to rotate.
2. multi-functional integrated mast installation as claimed in claim 1, is characterized in that, also comprise elevating base, described development mechanism is arranged on described elevating base.
3. multi-functional integrated mast installation as claimed in claim 1 or 2, it is characterized in that, described development mechanism comprises drive motor I and reductor I, and the output shaft of described drive motor I is connected with described reductor I, and the output shaft of described drive motor I is fixedly connected with described output frame.
4. multi-functional integrated mast installation as claimed in claim 3, is characterized in that, the output shaft of described drive motor I is connected by set pin with described output frame.
5. multi-functional integrated mast installation as claimed in claim 1, is characterized in that, described output frame is " Z " font.
6. multi-functional integrated mast installation as claimed in claim 1, it is characterized in that, described Yawing mechanism comprises housing II, drive motor II and reductor II, described drive motor II and described reductor II are arranged in described housing II, described output frame is fixedly connected with described housing II, and the output shaft of described drive motor II is connected with described reductor II.
7. multi-functional integrated mast installation as claimed in claim 6, it is characterized in that, described antenna mechanism comprises aerial bracket I, aerial bracket II and directional antenna, described directional antenna is fixedly connected with described aerial bracket I, described aerial bracket II respectively, and the output shaft of described drive motor II is fixedly connected with described aerial bracket I, described directional antenna and described aerial bracket II successively.
8. multi-functional integrated mast installation as claimed in claim 6, it is characterized in that, described luffing mechanism comprises housing III, drive motor III and reductor III, described drive motor III and described reductor III are arranged in described housing III, the output shaft of described drive motor II is fixedly connected with described housing III, and the output shaft of described drive motor III is connected with described reductor III.
9. multi-functional integrated mast installation as claimed in claim 8, it is characterized in that, described phase machine mechanism comprises camera support and some cameras, and described some cameras are fixedly installed on described camera support, and the output shaft of described drive motor III is fixedly connected with described camera support.
10. multi-functional integrated mast installation as claimed in claim 9, is characterized in that, the output shaft of described drive motor III is connected by set pin with described camera support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420336959.8U CN204021261U (en) | 2014-06-23 | 2014-06-23 | Multi-functional integrated mast installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420336959.8U CN204021261U (en) | 2014-06-23 | 2014-06-23 | Multi-functional integrated mast installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204021261U true CN204021261U (en) | 2014-12-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420336959.8U Expired - Lifetime CN204021261U (en) | 2014-06-23 | 2014-06-23 | Multi-functional integrated mast installation |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105406193A (en) * | 2015-11-25 | 2016-03-16 | 中国电子科技集团公司第三十八研究所 | Large radar antenna with pitching dual-motor synchronous driving mechanism |
| CN112606979A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Power-off self-locking method for turnover type underwater mast |
| CN112606978A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Comprehensive mast system |
| CN112606982A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Communication system based on underwater mast |
| CN112623166A (en) * | 2020-12-24 | 2021-04-09 | 北京华航无线电测量研究所 | Output shaft transmission system with retractable invisible mast |
| CN112623167A (en) * | 2020-12-24 | 2021-04-09 | 北京华航无线电测量研究所 | Pitching shaft body connecting structure capable of containing invisible mast |
| CN112660350A (en) * | 2020-12-24 | 2021-04-16 | 北京华航无线电测量研究所 | Submersible vehicle hidden monitoring method based on retractable mast |
| CN112678114A (en) * | 2020-12-24 | 2021-04-20 | 北京华航无线电测量研究所 | Sealing structure of underwater mast |
| CN112678135A (en) * | 2020-12-24 | 2021-04-20 | 北京华航无线电测量研究所 | Underwater mast structure |
| CN112693584A (en) * | 2020-12-24 | 2021-04-23 | 北京华航无线电测量研究所 | Optical monitoring system based on underwater mast |
| CN112722223A (en) * | 2020-12-24 | 2021-04-30 | 北京华航无线电测量研究所 | Double-shaft servo system capable of containing invisible mast |
| CN112829905A (en) * | 2020-12-29 | 2021-05-25 | 中国船舶重工集团有限公司第七一0研究所 | Double-mast integrated module for underwater unmanned vehicle |
| CN113911394A (en) * | 2021-09-30 | 2022-01-11 | 北京空间飞行器总体设计部 | Light-weight large-bearing extraterrestrial planet detection pointing mechanism |
-
2014
- 2014-06-23 CN CN201420336959.8U patent/CN204021261U/en not_active Expired - Lifetime
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105406193A (en) * | 2015-11-25 | 2016-03-16 | 中国电子科技集团公司第三十八研究所 | Large radar antenna with pitching dual-motor synchronous driving mechanism |
| CN105406193B (en) * | 2015-11-25 | 2018-07-13 | 中国电子科技集团公司第三十八研究所 | A kind of Large Radar Antenna with pitching two-shipper synchronous drive mechanism |
| CN112606979A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Power-off self-locking method for turnover type underwater mast |
| CN112606978A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Comprehensive mast system |
| CN112606982A (en) * | 2020-12-24 | 2021-04-06 | 北京华航无线电测量研究所 | Communication system based on underwater mast |
| CN112623166A (en) * | 2020-12-24 | 2021-04-09 | 北京华航无线电测量研究所 | Output shaft transmission system with retractable invisible mast |
| CN112623167A (en) * | 2020-12-24 | 2021-04-09 | 北京华航无线电测量研究所 | Pitching shaft body connecting structure capable of containing invisible mast |
| CN112660350A (en) * | 2020-12-24 | 2021-04-16 | 北京华航无线电测量研究所 | Submersible vehicle hidden monitoring method based on retractable mast |
| CN112678114A (en) * | 2020-12-24 | 2021-04-20 | 北京华航无线电测量研究所 | Sealing structure of underwater mast |
| CN112678135A (en) * | 2020-12-24 | 2021-04-20 | 北京华航无线电测量研究所 | Underwater mast structure |
| CN112693584A (en) * | 2020-12-24 | 2021-04-23 | 北京华航无线电测量研究所 | Optical monitoring system based on underwater mast |
| CN112722223A (en) * | 2020-12-24 | 2021-04-30 | 北京华航无线电测量研究所 | Double-shaft servo system capable of containing invisible mast |
| CN112829905A (en) * | 2020-12-29 | 2021-05-25 | 中国船舶重工集团有限公司第七一0研究所 | Double-mast integrated module for underwater unmanned vehicle |
| CN113911394A (en) * | 2021-09-30 | 2022-01-11 | 北京空间飞行器总体设计部 | Light-weight large-bearing extraterrestrial planet detection pointing mechanism |
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| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |