CN218772740U - Satellite measurement and control ground detector in random mode - Google Patents
Satellite measurement and control ground detector in random mode Download PDFInfo
- Publication number
- CN218772740U CN218772740U CN202222139695.4U CN202222139695U CN218772740U CN 218772740 U CN218772740 U CN 218772740U CN 202222139695 U CN202222139695 U CN 202222139695U CN 218772740 U CN218772740 U CN 218772740U
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- China
- Prior art keywords
- wall
- circuit board
- ground detector
- satellite measurement
- control ground
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- 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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- 238000005259 measurement Methods 0.000 title claims abstract description 18
- 238000009434 installation Methods 0.000 claims abstract description 9
- 230000000694 effects Effects 0.000 abstract description 7
- 238000006073 displacement reaction Methods 0.000 abstract description 2
- 238000001514 detection method Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
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Abstract
The utility model discloses a meet satellite measurement and control ground detector of mode at will, including organism and panel, the panel bolt fastening is at the opening end outer wall of organism: the inner wall of organism is provided with the installation pole, and is equipped with the spout on the installation pole, the inner wall both sides of spout all are provided with elastic component, and the activity is provided with the circuit board between two elastic component, be provided with main control unit, tuner and demodulator on the circuit board respectively. The utility model discloses in, this detector can provide the elastic expansion space on the transverse position for the circuit board through two elastic component that set up for the circuit board can be in certain extent elastic displacement when receiving impact action, thereby plays the cushioning effect to the impact force, avoids violent impact force and leads to the circuit board to take place to drop or even the phenomenon of damage, the effectual installation safety in utilization that improves the circuit board.
Description
Technical Field
The utility model relates to a satellite observes and controls technical field, especially relates to a satellite observes and controls ground detection appearance of chance mode.
Background
In a conventional satellite measurement and control system, various analog quantity signals and digital quantity signals are required to be collected and processed correspondingly. For example, there are many analog quantity signals and digital quantity signals to be acquired in the distributor equipment, and the relay in the distributor equipment needs to be correspondingly opened and closed, so as to complete the power-on and power-off functions of the load.
The circuit board is required to be installed in the existing satellite measurement and control ground detector, corresponding components are arranged on the circuit board for measurement and control detection, the installation structure of the circuit board generally adopts a fixed mode, the circuit board cannot flexibly move within a certain range, when the satellite measurement and control ground detector is severely impacted, the circuit board can be impacted, the phenomenon of easy fault damage is caused, and the using effect of the satellite measurement and control ground detector is reduced.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a can play the buffer protection to handle to the circuit board, avoid the circuit board to take place to acutely rock and the satellite observing and controlling ground detector of fault damage along with meet the mode.
In order to achieve the above object, the present invention provides the following technical solutions: the utility model provides a satellite of chance mode observes and controls ground detection appearance, includes organism and panel, the panel bolt fastening is at the open end outer wall of organism:
the inner wall of the machine body is provided with an installation rod, and the installation rod is provided with a sliding chute;
elastic components are arranged on two sides of the inner wall of the sliding chute, and a circuit board is movably arranged between the two elastic components;
and the circuit board is respectively provided with a main controller, a tuner and a demodulator.
As a further description of the above technical solution:
the elastic component comprises a jacket arranged in the sliding groove, an oil body is filled in the jacket, a push rod is arranged on the outer side of the oil body, and a sliding seat is arranged at the end part of the push rod.
As a further description of the above technical solution:
the inner wall of the jacket is provided with an air bag.
As a further description of the above technical solution:
the two jackets are connected through a conduction pipe.
As a further description of the above technical solution:
the outer wall of the panel is provided with a display screen and a control button respectively.
As a further description of the above technical solution:
and the outer wall of the machine body is respectively provided with a data connector and a power supply interface.
As a further description of the above technical solution:
the outer wall spiral connection of data connector has flexible pipe, and the open end inner wall of flexible pipe is provided with flexible rubber packing.
In the technical scheme, the utility model provides a pair of satellite measurement and control ground detector of chance mode has following beneficial effect:
this detector can provide the flexible space of elasticity on the transverse position for the circuit board through two elastic component that set up for the circuit board can be in certain extent elastic displacement when receiving impact effect, thereby plays the cushioning effect to the impact force, avoids violent impact force and leads to the circuit board to take place to drop the phenomenon of damaging even, the effectual installation safety in utilization who improves the circuit board.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments described in the present invention, and other drawings can be obtained by those skilled in the art according to these drawings.
Fig. 1 is a schematic structural diagram of a satellite measurement and control ground detector in a encounter mode according to an embodiment of the present invention;
fig. 2 is a schematic view of an internal structure of a machine body according to an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a mounting rod according to an embodiment of the present invention;
fig. 4 is a schematic view of an internal structure of an elastic component according to an embodiment of the present invention;
fig. 5 is a schematic structural diagram of a data connector according to an embodiment of the present invention.
Description of reference numerals:
1. a body; 11. a circuit board; 12. a main controller; 13. mounting a rod; 131. a chute; 132. an elastic component; 1321. a jacket; 1322. a top rod; 1323. a conduction pipe; 1324. an air bag; 1325. an oil body; 133. a slide base; 14. a tuner; 15. a demodulator; 2. a panel; 3. a display screen; 4. a data connector; 41. a telescopic pipe; 42. a rubber gasket; 5. a power interface; 6. and a control button.
Detailed Description
In order to make those skilled in the art better understand the technical solution of the present invention, the present invention will be further described in detail with reference to the attached drawings.
As shown in fig. 1-5, a satellite measurement and control ground detector in a random mode includes a machine body 1 and a panel 2, the panel 2 is bolted to an outer wall of an open end of the machine body 1:
the inner wall of the machine body 1 is provided with a mounting rod 13, and the mounting rod 13 is provided with a sliding chute 131;
the two elastic components 132 are respectively arranged on two sides of the inner wall of the chute 131, the circuit board 11 is movably arranged between the two elastic components 132, and the two elastic components 132 can provide an elastic telescopic space at a transverse position for the circuit board 11, so that the circuit board 11 can elastically displace in a certain range when being impacted, thereby buffering the impact force and avoiding the phenomenon that the circuit board 11 falls off or is damaged due to violent impact force;
a main controller 12, a tuner 14 and a demodulator 15 are respectively arranged on the circuit board 11, the tuner 14 and the demodulator 15 (the structure and the working principle are the same as those of the conventional tuner 14 and demodulator 15, and are not described herein) are mutually connected in a conductive manner, a signal input end of the tuner 14 is connected with the data connector 4, a signal output end of the demodulator 15 is connected with the main controller 12 in a conductive manner, and the data connector 4 is used for connecting satellite antenna signals;
the outer wall of panel 2 is provided with display screen 3 and control button 6 respectively, and the outer wall of organism 1 is provided with data connector 4 and power source 5 respectively for the measurement and control data on the circuit board 11 can show on display screen 3, and carry out corresponding controlling through control button 6.
The elastic component 132 includes a jacket 1321 disposed in the chute 131, the jacket 1321 is filled with an oil body 1325, the outside of the oil body 1325 is provided with a mandrel 1322, the end of the mandrel 1322 is provided with a slide seat 133, the inner wall of the jacket 1321 is provided with an air bag 1324, the two jackets 1321 are connected through a conducting pipe 1323, when the detector falls on the ground or is impacted by a large external force, an impact force is transmitted to the circuit board 11, at this time, the circuit board 11 drives the slide seat 133 to move in the chute 131, and the slide seat 133 presses the mandrel 1322 on one side, so that the mandrel 1322 on the side enters the corresponding jacket 1321, and presses the oil body 1325 in the jacket 1321 to enter the conducting pipe 1323, and finally flows into another jacket 1321, thereby the elastic buffer effect is achieved on the moving process of the slide seat 133, the impact influence on the circuit board 11 is reduced, when the mandrel moves to press the air bag 1324 to deform, the air bag 132133 can be further buffered, and the slide seat 1324 loses pressure, and the slide seat 1324 can be reset to drive the slide seat 131 to be reset to move in the chute 11, and the circuit board 11 can be reset automatically, and the circuit board can be restored to be moved.
The outer wall screwed connection of data joint 4 has flexible pipe 41, and the open end inner wall of flexible pipe 41 is provided with flexible rubber gasket 42, after data joint 4 goes up the cover and establishes connecting wire, rotate flexible pipe 41 and make it remove connecting wire's the outside, and make rubber gasket 42 can contact with connecting wire's outer wall, thereby play sealed parcel's effect between connecting wire and the data joint 4, also play outside flexible guard action to connecting wire simultaneously, prevent that connecting wire from taking place excessive wearing and tearing cracked phenomenon even when the atress is crooked, the wiring stability of data joint 4 has been improved.
Certain exemplary embodiments of the present invention have been described above by way of illustration only, and it will be apparent to those of ordinary skill in the art that the described embodiments may be modified in various different ways without departing from the spirit and scope of the present invention. Accordingly, the drawings and description are illustrative in nature and should not be construed as limiting the scope of the invention.
Claims (7)
1. The utility model provides a satellite of mode is observed and controled ground detector along with meeting, includes organism (1) and panel (2), panel (2) bolt fastening is at the opening end outer wall of organism (1), its characterized in that:
the inner wall of the machine body (1) is provided with an installation rod (13), and the installation rod (13) is provided with a sliding chute (131);
elastic components (132) are arranged on two sides of the inner wall of the sliding groove (131), and a circuit board (11) is movably arranged between the two elastic components (132);
the circuit board (11) is provided with a main controller (12), a tuner (14) and a demodulator (15) respectively.
2. The satellite measurement and control ground detector in the opportunistic mode according to claim 1, characterized in that: the elastic component (132) comprises a jacket (1321) arranged in the sliding groove (131), an oil body (1325) is filled in the jacket (1321), a push rod (1322) is arranged on the outer side of the oil body (1325), and a sliding seat (133) is arranged at the end part of the push rod (1322).
3. The satellite measurement and control ground detector in the opportunistic mode according to claim 2, characterized in that: an air bag (1324) is arranged on the inner wall of the jacket (1321).
4. The satellite measurement and control ground detector in the opportunistic mode according to claim 2, characterized in that: the two jackets (1321) are connected through a conducting pipe (1323).
5. The satellite measurement and control ground detector in the opportunistic mode according to claim 1, characterized in that: the outer wall of the panel (2) is respectively provided with a display screen (3) and a control button (6).
6. The satellite measurement and control ground detector in the opportunistic mode according to claim 1, characterized in that: the outer wall of the machine body (1) is respectively provided with a data connector (4) and a power interface (5).
7. The satellite measurement and control ground detector of the opportunistic mode according to claim 6, characterized in that: the outer wall of the data joint (4) is spirally connected with a telescopic pipe (41), and the inner wall of the opening end of the telescopic pipe (41) is provided with a flexible rubber gasket (42).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222139695.4U CN218772740U (en) | 2022-08-15 | 2022-08-15 | Satellite measurement and control ground detector in random mode |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222139695.4U CN218772740U (en) | 2022-08-15 | 2022-08-15 | Satellite measurement and control ground detector in random mode |
Publications (1)
Publication Number | Publication Date |
---|---|
CN218772740U true CN218772740U (en) | 2023-03-28 |
Family
ID=85690654
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202222139695.4U Expired - Fee Related CN218772740U (en) | 2022-08-15 | 2022-08-15 | Satellite measurement and control ground detector in random mode |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN218772740U (en) |
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2022
- 2022-08-15 CN CN202222139695.4U patent/CN218772740U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20230328 |
|
CF01 | Termination of patent right due to non-payment of annual fee |