CN115801105B - One-vehicle one-stop type high-integration maneuvering measurement and control station - Google Patents
One-vehicle one-stop type high-integration maneuvering measurement and control station Download PDFInfo
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- CN115801105B CN115801105B CN202211641360.0A CN202211641360A CN115801105B CN 115801105 B CN115801105 B CN 115801105B CN 202211641360 A CN202211641360 A CN 202211641360A CN 115801105 B CN115801105 B CN 115801105B
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Abstract
The invention relates to the field of aerospace measurement and control, in particular to a one-vehicle one-stop type high-integration maneuvering measurement and control station. The measurement and control station integrates measurement and control, guard, network, navigation and power supply functions, and the measurement and control shelter can be divided into a working area, a measurement and control antenna area, a guard antenna area and a power station area according to the functional area. The invention has the beneficial effects that the functions of four vehicles of the traditional measurement and control station are integrated into one vehicle through a high-integration design, and a one-vehicle one-stop maneuvering measurement and control station capable of loading multi-domain equipment and independently executing tasks is innovatively developed. Through reasonable arrangement and careful design, each region of the measurement and control station can be effectively utilized, and the system has the advantages of multi-domain synthesis, high integration, high automation, capability of being deployed anywhere, quick response and the like, and meets the urgent demands of the current market.
Description
Technical Field
The invention belongs to the technical field of aerospace measurement and control, and particularly relates to a one-vehicle one-stop type high-integration maneuvering measurement and control station.
Background
The vehicle-mounted shelter measurement and control station is widely applied due to good maneuverability, high flexibility and convenience in quick deployment. However, the existing motor measurement and control station, especially the motor station loaded with large-scale measurement and control antenna, is limited by the traditional loading mode and vehicle space, the integration level is generally low, a multi-vehicle one-station mode is generally adopted, namely, a set of measurement and control station with complete functions is formed by a plurality of vehicles with different functions, each vehicle can only realize a single function, and the set of station is generally divided into a plurality of vehicles such as antenna vehicles, equipment vehicles, power station vehicles, satellite communication vehicles and the like. The method has the advantages of low integration level, poor concealment, low automation degree and low response speed, and particularly seriously influences the emergency response capability of the motor station when facing emergency tasks and emergencies. With the rapid development of aerospace industry and the requirement for maneuvering measurement and control in recent years, the defects of the traditional maneuvering measurement and control station are more remarkable, and the one-stop measurement and control station which has high integration level, maneuvering flexibility, can be deployed at any time and any place and can respond rapidly becomes an urgent market demand.
Disclosure of Invention
The invention aims to solve the defects of the traditional multi-vehicle one-stop type maneuvering measurement and control station, and provides a design method of the one-vehicle one-stop type high-integration maneuvering measurement and control station.
In order to achieve the above purpose, the present invention adopts the following technical scheme:
A highly integrated maneuvering measurement and control station can realize all functions of a complete measurement and control station, including measurement and control, communication, navigation, power supply and the like, and a whole vehicle space comprises loading of a measurement and control antenna and a satellite antenna, installation of related equipment and a cabinet, operation space of personnel, an operation desk and a display console, whole vehicle power supply equipment, calibration equipment, a measurement and gesture positioning system and the like. All functions of the measurement and control station are integrated in a vehicle and a shelter, and the system can be divided into two parts of the vehicle and the shelter according to the structure, wherein the shelter can be divided into a working area, a measurement and control antenna area, a guard antenna area and a power station area according to the functions;
The vehicle is a vehicle of the measurement and control station;
The shelter integrates all functions of the measurement and control station, and the bottom of the shelter is provided with a standard twist lock interface, so that the shelter can be mounted on a vehicle or a ship and is flexible and motorized to install;
The working area is used for integrating equipment such as personnel operation facilities, indoor measurement and control communication network navigation and other supporting facilities. The measurement and control equipment is arranged on the equipment cabinet in a centralized way, and the personnel operation facilities comprise an operation seat, an aviation seat, a large-sized liquid crystal display screen and a work table. Other supporting facilities comprise UPS uninterrupted power supply equipment, environmental control equipment, warm air blower, comprehensive distribution box, storage cabinet and the like;
The measurement and control antenna area is used for loading a large measurement and control antenna, and the antenna is provided with an intelligent lodging mechanism and can be completely contained in the cabin in a collection state;
The guard antenna area is used for loading a guard antenna and an antenna housing, and the guard antenna is provided with an intelligent lifting system;
the power station area is used for loading 2 high-power oil machines, and the two oil machines are mutually backed up to provide reliable electric power support for the whole set of measurement and control system;
The antenna of the measurement and control antenna area is connected with measurement and control equipment of the working area through a cable; the guard antenna of the guard antenna area is connected with communication equipment of the working area through a cable; the oil engine of the power station area is connected with the comprehensive distribution box of the working area through a power cable, and is connected with an upper computer of the working area through a control cable, so that intelligent control of power supply and fault reporting of the oil engine are realized;
preferably, an electric sliding cabin top cover is arranged at the top of the measurement and control antenna area, so that the concealment and protection of the antenna in a storage state can be ensured;
Preferably, a movable unmanned aerial vehicle packaging box and an accessory box are arranged below a rear antenna in the measurement and control antenna area, and the unmanned aerial vehicle can be used for mounting calibration equipment during calibration in areas such as offshore or desert and the like;
Preferably, an oil machine and a cabinet are arranged below the tail antenna of the measurement and control antenna area, so that grid connection of the oil machine and the mains supply and parallel operation between the two oil machines can be realized, namely, thermal switching can be realized between the mains supply and the oil machine and between the two oil machines, and uninterrupted power supply of equipment can be ensured even if the mains supply is suddenly powered off or one of the oil machines fails;
Preferably, a UPS host and a battery cabinet are arranged in a working area, so that uninterrupted power supply of key equipment of the whole system is ensured;
preferably, a maintenance door is arranged at the joint of the oil engine and the cabinet and the square bulkhead, and a power aviation plug is arranged on a control panel of the cabinet and is used as a power port of the whole vehicle;
Preferably, a bracket is arranged at the rear part of the cab of the tractor, an electric lifting rod is arranged on the bracket, and the top of the lifting rod is used for installing calibration equipment and lightning protection equipment.
Preferably, an electric leveling support leg is arranged at the bottom of the semitrailer and used for supporting and leveling the chassis in a vehicle-mounted parking state;
Preferably, the cable channel department of working cabin to outside all adopts the pyrogram stopper gram shielding module, and the ventilation window in the working cabin adopts the shielding window, and air conditioner air intake and air outlet department adopts waveguide ventilation window, and the inside and outside covering of shelter wallboard, roof, bottom plate adopts whole aluminum plate, above shielding measure guarantees the good shielding nature of working cabin, protects cabin staff to avoid electromagnetic radiation injury.
The invention provides a design method of a one-vehicle one-stop type high-integration maneuvering measurement and control station, which has the beneficial effects that:
by means of high integration design, functions of 4 vehicles are integrated into 1 vehicle, and compared with multiple vehicles and one station, the integration level of the maneuvering measurement and control station can be greatly improved, and the method is suitable for urgent requirements of the current aerospace measurement and control field on quick deployment of maneuvering stations;
By concentrating all functions of the measurement and control station on the design of a shelter and the design of a twist lock device at the bottom of the shelter, which accords with related standards, the measurement and control station can adapt to various mounting platforms of vehicles and ships, and compared with a plurality of vehicles and one station, the flexibility of the measurement and control station is greatly improved;
The electric sliding cover mechanism is arranged at the top of the shelter, so that the large measurement and control antenna is accommodated in the whole shelter, and the concealment of the measurement and control station can be remarkably improved;
The large measurement and control antenna is accommodated in the whole shelter, so that damage to the antenna by severe weather such as wind, sand, rain, snow, hail and the like can be reduced, the environmental adaptability of the antenna is remarkably improved, and the service life of the antenna is prolonged;
1 by high power station: 1, the heat backup and mains supply grid connection design can obviously improve the reliability of the whole system power supply and the adaptability to severe environments such as a plateau;
The uninterrupted power supply equipment of the UPS provides double guarantees for uninterrupted power supply of other important equipment except the driving motor.
Drawings
FIG. 1 is an overall external view of the measuring and control station of the present invention.
Fig. 2 is a layout of the right wall of the cabin according to the invention.
Fig. 3 is a top view of the interior of the capsule of the present invention.
Fig. 4 is a layout of the left wall in the cabin according to the invention.
Fig. 5 is an a-direction view of fig. 2 in accordance with the present invention.
Fig. 6 is a B-B view of fig. 2 of the present invention.
Fig. 7 is a view in the direction C of fig. 2 of the present invention.
Fig. 8 is a schematic view of the entire structure of the sliding top cover in fig. 2.
Fig. 9 is a schematic structural view of the sliding plate of fig. 8.
Fig. 10 is a schematic structural view of the driving device of fig. 8.
Fig. 11 is a schematic structural view of the impact mechanism of fig. 8.
Fig. 12 is a schematic view of the rack and guide wheel of fig. 8.
Fig. 13 is a bottom view of fig. 8.
In the figure:
1. A tractor; 2. a semi-trailer; 3. an electric lifting rod; 4. electrically leveling the support legs; 5. a box-type cabin; 6. a working area; 7. measuring and controlling an antenna area; 8. a guard antenna area; 9. a power station area; 10. a counter; 11. a counter maintenance door; 12. a storage box; 13. an aeronautical seat; 14. a compartment plate; 15. a cabinet; 16. a left maintenance door of the cabinet; 17. a right maintenance door of the cabinet; 18. a pyroxak shielding module; 19. a battery and a storage cabinet; 20. an integral air conditioner; 21. a U-shaped air duct; 22. a large liquid crystal display; 23. a turnover plate table; 24. shielding the observation window; 25. a temperature and humidity clock; 26. a signal aperture door; 27. a comprehensive distribution box; 28. a cabin door; 29. an illumination panel switch; 30. an air conditioner controller; 31. a warm-air drier; 32. a large measurement and control antenna; 33. measuring and controlling an antenna lodging mechanism; 34. sliding the top cover; 35. an antenna left maintenance door; 36. an antenna right maintenance door; 37. a lodging mechanism control box; 38. sliding the top cover control box; 39. unmanned aerial vehicle containing box; 40. unmanned aerial vehicle accessory box; 41. the oil machine is combined with the cabinet; 42. a power port door; 43. a satellite antenna and an antenna housing; 44. a toilet antenna lifting mechanism; 45. an oil engine No. 1; 46. a No. 2 oil machine; 101. a fixing plate; 102. a multi-stage sliding plate; 103. a driving device; 104. a collision mechanism; 105. a rack; 106. a guide wheel; 107. an automatic wire winding mechanism; 108. a limit switch; 109. a sealing strip; 201. a load-bearing frame; 202. a skin; 301. a motor; 302. a speed reducer; 303. a first drive shaft; 304. a first gear; 305. a second gear; 306. a second drive shaft; 307. a third gear; 401. a front bump; 402. a rear bump; 501. a reverse hanging rack; 502. and a rack mount.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments.
As shown in fig. 1 to 13, the highly integrated mobile measurement and control station according to the present invention includes a tractor 1 and a semitrailer 2, where the tractor 1 and the semitrailer 2 are vehicles of the measurement and control station, and two kinds of chassis or other types of chassis may be used according to actual use requirements. In this embodiment, electric lift pole 3 is installed at tractor 1 driver's cabin rear portion, and electric lift pole 3 top is used for installing calibration equipment and lightning-arrest equipment, and electric lift pole 3's the highest stroke is 15m, can satisfy calibration user demand and lightning-arrest demand. And an electric leveling supporting leg 4 is arranged at the bottom of the semitrailer 2 and is used for supporting and leveling the chassis in a vehicle-mounted parking state. In this embodiment, a box-shaped cabin 5 is loaded on the semitrailer 2, and the box-shaped cabin 5 can be a box-shaped cabin 5 with a step at the bottom, or can be a cabin with other shapes according to the actual chassis type and the use environment. In this embodiment, the maximum external dimensions of the box-shaped enclosure 5 are 12000mm×2438mm×3100mm (length×width×height). The box-type cabin body 5 is divided into a working area 6, a measurement and control antenna area 7, a satellite antenna area 8 and a power station area 9 according to functions.
The working area 6 is positioned at the front part of the box-type cabin 5, and three operation seats 9 are arranged on the front wall of the working area 6. The bottom of the operation seat 9 is provided with 4 19-inch cabinets 10 with the height of 13U, and the front wall of the working area 6 is provided with two cabinet maintenance doors 11, so that equipment in the cabinets 10 can be maintained from the rear part. The top of the operating seat 9 is provided with a storage cabinet 12. The operation seat 9 rear side sets up 3 aviation seat 13, and the design of aviation seat 13 satisfies ergonomic requirement, can provide comfortable safe operation environment for operating personnel. The space cabin plate 14 is arranged between the working area 6 and the measurement and control antenna area 7, 419 inch cabinets 15 with the height of 36U are arranged at the rear part of the working area 6, a gap of 500mm is reserved between the cabinets 15 and the space cabin plate 14 to serve as a rear maintenance space of the cabinet 13, and the left and right sides of the space cabin plate 14 are provided with cabinet left maintenance doors 16 and cabinet right maintenance doors 17, so that personnel can conveniently enter the working area 6 from the measurement and control antenna area 7, and equipment in the cabinets 15 can be repaired from the rear part. A set of pyroxak shielding modules 18 are respectively arranged below the left and right cabinet maintenance doors 16 and 17 and used for accessing cables entering the working cabin from other cabins, so that the shielding performance of the working cabin is ensured. The clearance department of rack 15 and the left side wall of workspace 6 still is equipped with battery and locker 19, and battery and locker 19 first half is the storage tank, forms sufficient storing space together with locker 12, satisfies operating personnel's storing demand. The battery and the back half part of the storage cabinet 19 are provided with UPS battery packs, the cabinet 15 is provided with a UPS host, and the UPS battery packs and the UPS host form an uninterruptible power supply system together, so that uninterruptible power supply of important equipment of the measurement and control station is ensured. The cabinet 15 forms a sufficient installation space for the equipment together with the cabinet 10 to meet the installation requirements of the whole system equipment. An integrated air conditioner 20 is hung outside the front wall of the working area 6, an air inlet and an air return opening are formed in the joint of the front wall of the working area 6 and the integrated air conditioner 20, a U-shaped air duct 21 is arranged on the periphery of the top surface inside the working area 6, and a plurality of groups of air balls are uniformly distributed on the U-shaped air duct 21. The left side wall of the working area 6 is provided with a large-sized liquid crystal display 22, a turnover table 23, a shielding observation window 24 and a temperature and humidity clock 25. The right side wall of the working area 6 is provided with a signal hole door 26, a comprehensive distribution box 27, a cabin door 28, a lighting panel switch 29 and an air conditioner controller 30. The integrated air conditioner 20, the air inlet, the air return opening, the U-shaped air duct 21 and the air conditioner controller 30 form a complete environmental control system together, and effective temperature and humidity guarantee is provided for the working area 6. The lower part of the left side wall of the working area 6, which is close to the aviation seat, is also provided with a warm air blower 31 for auxiliary heating measures when the air temperature is low.
And the measurement and control antenna area 7 is positioned in the middle of the box-type cabin 5. And a large measurement and control antenna 32 and a measurement and control antenna lodging mechanism 33 are arranged in the measurement and control antenna area 7. The main reflecting surface of the large measurement and control antenna 32 adopts a two-side folding structure, and the total width is smaller than the internal net width of the bulkhead of the measurement and control antenna area 7 in the storage state, so that the smooth storage of the antenna is ensured. The top of the measurement and control antenna area 7 is of a large opening structure, and a sliding top cover 34 capable of being automatically opened and closed is arranged to meet the cabin entering and exiting requirements, the hiding requirements and the protection requirements of the large antenna. The left side wall of the measurement and control antenna area 7 is provided with an antenna left maintenance door 35, and the right side wall is provided with an antenna right maintenance door 36, so that the maintenance requirements of the internal equipment are met. The right side wall hanging antenna lodging mechanism control box 37 and the sliding top cover control box 38 of the measurement and control antenna area 7 are respectively provided with a plurality of illuminating lamps on the left side wall, the right side wall and the rear wall, so that the illumination requirement of the measurement and control antenna area 7 is met. The unmanned aerial vehicle storage box 39 and the unmanned aerial vehicle accessory box 40 are arranged below the rear antenna in the measurement and control antenna area 7, and the loaded unmanned aerial vehicle can be used for loading calibration equipment in calibration of areas such as offshore or deserts. And an oil machine and cabinet 41 is arranged below the tail antenna of the measurement and control antenna area 7, and a control panel of the oil machine and cabinet 41 is arranged on the end face of the control panel close to the right bulkhead of the measurement and control antenna area 7. And a power hole door 42 is formed at the joint of the right side wall of the measurement and control antenna area 7 and the control panel of the cabinet for maintaining the cabinet. The control panel of the oil engine and cabinet 41 is provided with a power input aviation plug of the whole vehicle as a power orifice of the whole vehicle.
In this embodiment, the measurement and control antenna lodging mechanism 33 is electrically interlocked with the sliding top cover 34, after the sliding top cover 34 is completely opened, the measurement and control antenna lodging mechanism 33 can lodge, and after the measurement and control antenna lodging mechanism 33 is collected in place, the sliding top cover 34 can be closed.
The structure of the sliding roof in this embodiment is specifically as follows:
the device is covered at the position of the shelter opening and comprises a multi-stage sliding plate set 102, a driving device 103 and a collision mechanism 104, wherein a plurality of sliding plates of the multi-stage sliding plate set are arranged in a stacked mode, and the sliding plate at the lowest layer is a fixed plate which is fixedly arranged at one side of the shelter opening;
The driving device is positioned on the lower surface of the sliding plate at the uppermost layer; the driving device comprises a motor and a transmission shaft; third gears 307 are arranged at the two ends of the second transmission shaft 306, racks are arranged at the tops of the two side walls of the square cabin opening, and the third gears are meshed with the corresponding racks; the motor drives the third gear to move along the rack through the second transmission shaft.
The driving device 103 further comprises a speed reducer 302, a first transmission shaft 303, a first gear 304 and a second gear 305; the middle part of the first transmission shaft is fixedly connected with the output end of the speed reducer; the two first gears are respectively positioned at two ends of the first transmission shaft; the first drive shaft rotates the second drive shaft by engagement of the second gear 305 on the second drive shaft with the first gear.
Further, the collision mechanism 104 includes a front striker 401 and a rear striker 402. One end of the near driving device on the lower surface of each sliding plate is provided with the front collision block 401, and the front collision block and the sliding plate on the lower layer are positioned on the same plane; the rear collision block 402 is arranged at one end of the far driving device on the lower surface of each sliding plate, and a limiting block is arranged at one end of the near driving device on the upper surface of each sliding plate; and in the shelter sealing state, the rear stop block is tightly attached to the limiting block.
Each sliding plate consists of a bearing frame 201 and a skin 202; the skin is located on top of the load-bearing frame.
The third gear 307 and the rack 105 adopt an inverted engagement structure.
The rack 105 is provided with a sliding guide rail integrated with the rack; the lower surface of each sliding plate is provided with a guide wheel 106, and the guide groove of each guide wheel 106 is restrained in the sliding guide rail of the rack 105.
An automatic winding mechanism 107 is attached to an end portion of the fixed plate 101 near the driving device 103, and a cable led out from the control box is connected to the motor 301 after passing through the automatic winding mechanism 107.
A limit switch 108 is further arranged at the end part of the sliding plate at the topmost layer, and a stop block corresponding to the limit switch is arranged on the side wall of the shelter; when the multistage sliding plate group is unfolded to be extremely limited, the stop block is abutted against the limit switch. The skin 202 of each sliding plate 102 adopts a multi-fold structure, and a sealing strip 109 is arranged at the end edge of each sliding plate 102.
In this embodiment, the large measurement and control antenna 32 is electrically interlocked with the measurement and control antenna lodging mechanism 33, after the measurement and control antenna lodging mechanism 33 is lifted in place, the large measurement and control antenna 32 can be unfolded and posture adjusted, and after the large measurement and control antenna 32 is folded and azimuth and pitching angles are adjusted in place, the measurement and control antenna lodging mechanism 33 can lodge.
The guard antenna area 8 is positioned at the rear part of the box-shaped cabin body 5, and the area is not provided with a bulkhead and is of an open design. The guard antenna area 8 is provided with a guard antenna and an antenna housing 43 and a guard antenna lifting mechanism 44. The guard antenna lifting mechanism 44 can automatically lift and lock the guard antenna at any position.
The utility model discloses a power station district 9 is located the bottom in the antenna district 8 that defends, and power station district 9 left and right sides is equipped with No. 1 oil engine 45, no. 2 oil engines 46 respectively, and the capacity and the function of two oil engines are the same completely, are symmetrical design structurally, set up the operation maintenance panel at the lateral surface respectively to the maintenance operation of oil engine is convenient for.
In this embodiment, the power supply system of the measurement and control station is jointly formed by the comprehensive distribution box 27, the oil engine parallel cabinet 41, the oil engine No. 1 45, the oil engine No. 2 46, the UPS host and the UPS battery pack, wherein the oil engine parallel cabinet 41 can realize the parallel connection of the oil engine and the mains supply and the parallel connection between the two oil engines, namely, the heat switching between the mains supply and the oil engine and between the two oil engines can be realized, even if the mains supply is suddenly powered off or one of the oil engines fails, uninterrupted power supply of the equipment can be ensured, and the two oil engines can be combined for use, thereby obviously improving the power supply. The UPS host and the UPS battery pack are used as uninterruptible power supply components, and dual power supply guarantee is provided for important electronic equipment (except for a driving motor in general) of the measurement and control station.
The working procedure of this embodiment is: taking the field work in the vehicle-mounted state as an example, firstly arranging a measurement and control station to a designated place, opening a power hole door 42, operating a control panel of a cabinet 41 to start an oil engine, enabling a worker to enter a working area 6, opening a comprehensive distribution box 27 to power up all equipment, and leveling by using an electric supporting leg 4. After the sliding top cover 34 is opened in place, the measurement and control antenna lodging mechanism 33 is started, after the measurement and control antenna lodging mechanism 33 is lifted in place, the posture of the measurement and control antenna is unlocked, the main reflecting surface folding panel is opened, and the system monitors and issues parameters according to task requirements, so that measurement and control and communication tasks are completed.
The foregoing is only a preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art, who is within the scope of the present invention, should make equivalent substitutions or modifications according to the technical scheme of the present invention and the inventive concept thereof, and should be covered by the scope of the present invention.
Claims (1)
1. A one-vehicle one-stop type high-integration maneuvering measurement and control station is characterized in that: the measurement and control station includes: the vehicle and shelter; the vehicle comprises a tractor (1) and a semitrailer (2), and the shelter is a box-type shelter body (5); the box-type cabin body (5) is divided into a working area (6), a measurement and control antenna area (7), a satellite antenna area (8) and a power station area (9) according to functions;
the tractor (1) and the semitrailer (2) are vehicles, the tractor (1) drives the semitrailer (2) to move, and the box-shaped cabin (5) integrates the function of a measurement and control station and is positioned at the top of the semitrailer (2);
The working area (6) is used for operating and controlling the measurement and control station and deploying tasks by operators;
The measurement and control antenna area (7) is a loading platform of a large measurement and control antenna (32) and a lodging mechanism (33);
the guard antenna area (8) is a loading platform of a guard antenna, an antenna cover (43) and a guard antenna lifting mechanism (44);
The power station area (9) is a loading platform of the high-power oil engine and is used for providing field power supply for the measurement and control station;
A sliding top cover (34) capable of being automatically opened and closed is arranged at the top of the measurement and control antenna area (7);
The sliding top cover (34) covers the shelter opening and comprises a multistage sliding plate set (102), a driving device (103) and a collision mechanism (104), wherein a plurality of sliding plates of the multistage sliding plate set are arranged in a stacked mode, and the sliding plate at the lowest layer is a fixed plate and is fixedly arranged on one side of the shelter opening;
The driving device is positioned on the lower surface of the sliding plate at the uppermost layer; the driving device comprises a motor and a transmission shaft; third gears (307) are arranged at two ends of the second transmission shaft (306), racks are arranged at the tops of two side walls of the square cabin opening, and the third gears are meshed with the corresponding racks; the motor drives the third gear to move along the rack through the second transmission shaft;
The driving device (103) further comprises a speed reducer (302), a first transmission shaft (303), a first gear (304) and a second gear (305); the middle part of the first transmission shaft is fixedly connected with the output end of the speed reducer; the first gears are arranged at two ends of the first transmission shaft respectively; the first transmission shaft drives the second transmission shaft to rotate through the engagement of a second gear (305) on the second transmission shaft and the first gear;
The collision mechanism (104) comprises a front collision block (401) and a rear collision block (402); one end of the near driving device on the lower surface of each sliding plate is provided with a front collision block (401), and the front collision block and the sliding plate on the lower layer are positioned on the same plane; one end of the far driving device on the lower surface of each sliding plate is provided with a rear collision block (402), and one end of the near driving device on the upper surface of each sliding plate is provided with a limiting block; in the sealed state of the shelter, the rear stop block is tightly attached to the limiting block;
each sliding plate consists of a bearing frame (201) and a skin (202); the skin is positioned at the top of the bearing frame;
the third gear (307) and the rack (105) adopt a reverse engagement structure;
the rack (105) is provided with a sliding guide rail integrated with the rack; the lower surface of each sliding plate is provided with a guide wheel (106), and the guide groove of each guide wheel (106) is restrained in the sliding guide rail of the rack (105);
An automatic winding mechanism (107) is arranged at one end part of the fixed plate (101) close to the driving device (103), and a cable led out from the control box is connected to the motor (301) after passing through the automatic winding mechanism (107);
A limit switch (108) is further arranged at the end part of the sliding plate at the topmost layer, and a stop block corresponding to the limit switch is arranged on the side wall of the shelter; when the multistage sliding plate group is unfolded to be extremely limited, the stop block is propped against the limit switch; the skin (202) of each sliding plate (102) adopts a multi-bending structure, and a sealing strip (109) is arranged at the edge of the end part of each sliding plate (102).
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| CN116519020B (en) * | 2023-06-01 | 2025-03-11 | 中国电子科技集团公司第五十四研究所 | Inertial navigation calibration device and method for maneuvering measurement and control platform |
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| US6847892B2 (en) * | 2001-10-29 | 2005-01-25 | Digital Angel Corporation | System for localizing and sensing objects and providing alerts |
| CN104494503A (en) * | 2014-11-25 | 2015-04-08 | 中国兵器工业计算机应用技术研究所 | Comprehensive shelter system of unmanned aerial vehicle |
| CN210101442U (en) * | 2019-06-11 | 2020-02-21 | 龙岩市海德馨汽车有限公司 | Mobile base station vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN210363538U (en) * | 2019-08-14 | 2020-04-21 | 中航天元防务技术（北京）有限公司 | Open-air removal telemetry station |
| CN219918930U (en) * | 2022-12-20 | 2023-10-27 | 中国电子科技集团公司第五十四研究所 | One-vehicle one-stop type high-integration maneuvering measurement and control station |
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