CN216886422U - Shelter for ground command control system of unmanned aerial vehicle - Google Patents
Shelter for ground command control system of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN216886422U CN216886422U CN202220191527.7U CN202220191527U CN216886422U CN 216886422 U CN216886422 U CN 216886422U CN 202220191527 U CN202220191527 U CN 202220191527U CN 216886422 U CN216886422 U CN 216886422U
- Authority
- CN
- China
- Prior art keywords
- cabin
- shelter
- link
- seat
- cabin body
- 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.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a shelter for an unmanned aerial vehicle ground command control system, which comprises a cabin body, wherein the front part in the cabin body is a working cabin, the upper parts of the inner rear part in the cabin body are respectively a storage cabin and a link cabin which are arranged left and right, and the lower parts of the inner rear part in the cabin body are an oil cabin; a first flight control seat and a second flight control seat are arranged at the front end in the working cabin, and a comprehensive display seat, a task load seat and a link monitoring seat are arranged at the rear end; the left side wall of the cabin body is provided with an oil engine heat dissipation window, the right side wall of the cabin body is provided with a link cabin door, and the inside of the right side wall of the cabin body is provided with a remote control panel. According to the utility model, through the integrated design of each operation seat, each equipment cabinet, each link equipment and other equipment, the integral integration level of the shelter is higher, the functions of the ground command control system can be effectively increased, and the carriage expansibility and the equipment expansibility are strong.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle ground station design, and particularly relates to a shelter for an unmanned aerial vehicle ground command control system.
Background
With the rapid development of unmanned aerial vehicles and other related neighborhood subjects in recent years, the unmanned aerial vehicles have developed powerful weapons integrating reconnaissance and attack, and the unmanned aerial vehicles can fully and autonomously complete the attack capability of remote attack and even air combat missions in the future, particularly fixed wing unmanned aerial vehicles, and can be initially applied to the fields of surveying and mapping, geology, petroleum, agriculture and forestry and the like due to excellent functions and modularized integration of the unmanned aerial vehicles. The pod of the command and control system of the unmanned aerial vehicle generally requires that the display of the contents such as descending video, data, positioning, course and course track of the unmanned aerial vehicle is integrated in the fixed/movable pod, and the ascending of the pod has the capability of controlling the stages and processes of the unmanned aerial vehicle, such as flight attitude, flight data, take-off and landing. Specifically, an image receiving system, a flight control system antenna unit, a vehicle-mounted air conditioning unit, a mute generator unit, a mains supply access power supply system, a command display unit, a command seat unit and the like are integrated in a shelter.
At present, current unmanned aerial vehicle's operation seat and equipment rack subdivision design, and the last mounted position who does not reserve the oil machine of command and control car, link equipment also does not carry out integrated design, and these current situations all cause command and control car control unmanned aerial vehicle to use alone easily, need combine link data terminal can accomplish unmanned aerial vehicle flight task, cause to use inconveniently, and the reliability is poor.
Disclosure of Invention
The problems of poor integration of compartment equipment, limited compartment expansibility and equipment expandability and poor reliability in the prior art are solved.
In order to achieve the purpose, the utility model adopts the following technical scheme to solve the problem:
a shelter for an unmanned aerial vehicle ground command control system comprises a cabin body, wherein a working cabin is arranged at the front part in the cabin body, a storage cabin and a link cabin which are arranged on the left and right are respectively arranged above the inner rear part of the cabin body, and an oil cabin is arranged below the inner rear part of the cabin body; a first flight control seat and a second flight control seat are arranged in parallel at the front end in the working cabin, and a comprehensive display seat, a task load seat and a link monitoring seat are arranged in parallel at the rear end; an oil engine heat dissipation window is formed in the left side wall of the cabin body, a link cabin door is formed in the right side wall of the cabin body, and a remote control panel is installed inside the right side wall of the cabin body;
a manual lifting rod for mounting the U-band antenna is arranged on the outer wall of one side of the cabin body; the outer side of the top of the cabin body is respectively provided with a 4G/5G antenna, a GPS antenna, a weather instrument and a tripod head lodging device for installing a tripod head camera; the outer wall of the rear end of the cabin body is provided with an oil engine mounting door; and a top plate above the link cabin is provided with a link access.
Furthermore, a second lighting window, a power supply hole door, an air outlet and a storage bin door are arranged on the left side wall of the cabin body, a frame body used for installing interactive display equipment is arranged outside the left side wall, and the interactive display equipment is connected with the comprehensive display mat; the right side wall of the cabin body is provided with an air inlet, an access door and a first lighting window.
Furthermore, a coat hook is arranged on the inner wall of the left side of the cabin body.
Further, the front end of the cabin body is provided with an integrated air conditioner, a temperature and humidity clock is arranged on the inner wall of the left side of the integrated air conditioner, and the top of the cabin body is provided with an air duct connected with the integrated air conditioner.
Furthermore, the outer wall of the front end of the cabin body is provided with a boarding ladder, and the outer wall of the rear end of the cabin body is provided with a boarding ladder.
Furthermore, an electric top cover is arranged on a link access of the link cabin, and an electric lifting mechanism used for installing a link antenna is arranged in the link cabin.
Furthermore, the top of the cabin body is provided with a sunshade.
Further, still include the chassis car, the chassis car passes through the sub vehicle frame and installs cabin body below.
Furthermore, the first flight control seat and the second flight control seat are arranged in the same way, and comprise a flight operation platform, wherein a flight control computer and a matched keyboard, a mouse, an accelerator lever, a rocker and a pedal thereof are arranged on the flight operation platform; the flight control computer is provided with a plurality of displays; and the operation platforms of the comprehensive display seat, the task load seat and the link monitoring seat are all provided with a keyboard, a mouse and a plurality of displays.
Compared with the prior art, the utility model has the following technical effects:
1. the operation seat, the equipment cabinet, the link equipment and other equipment are integrated, and the oil engine room is reserved at the rear end of the shelter for installing the oil engine, so that the overall integration level of the shelter is higher, the functions of a ground command control system can be effectively increased, and the expansibility and the equipment expansibility of the carriage are high. Meanwhile, the design volume space of the shelter is effectively reduced, and the design and development cost is reduced.
2. A first flight control seat, a second flight control seat, a comprehensive display seat, a task load seat, a link monitoring seat and interactive display equipment are designed, and the reliability of the ground control unmanned aerial vehicle can be effectively improved by arranging an in-cabin control layout for multi-seat monitoring and control; the ground command control system installed in the shelter is enabled to carry out data communication in the local area network through the network switch, and hot backup can be carried out on communication among the control seats, the seats and the stations.
3. The chassis vehicle is designed at the bottom of the shelter, so that the overall maneuverability of the system is strong.
4. The link cabin is used for installing the link antenna, the electric sliding top cover is designed on the top of the link cabin and used for protecting the link antenna, and meanwhile, the automatic lifting mechanism is used for installing and controlling the lifting action of the link antenna, so that the link antenna is convenient and safe to use.
5. The holder lodging device for installing the holder camera is designed on the cabin top, so that the posture of the holder camera is convenient to install and control, and the workers can monitor the environment outside the cabin conveniently.
In conclusion, the shelter integrates and designs all parts of the ground command system, so that the system has the advantages of strong overall function, convenience in operation, strong maneuverability, smoothness in information interaction, stability in equipment operation, reasonable integrated configuration, good maintainability, strong expansion and design capability, and the unmanned aerial vehicle command control is more convenient and efficient.
Drawings
Fig. 1 is an external left side schematic view of a shelter for a ground command control system for an unmanned aerial vehicle of the present invention;
fig. 2 is an external right side schematic view of a shelter for a ground command control system for an unmanned aerial vehicle of the present invention;
figure 3 is an external rear side schematic view of a shelter for a ground command control system for an unmanned aerial vehicle of the present invention;
figure 4 is a top schematic view of a shelter for a ground command control system for an unmanned aerial vehicle of the present invention;
fig. 5 is a schematic view of the internal layout of the shelter for the ground command control system of the drone of the present invention;
FIG. 6 is a schematic layout of a first flight control agent and a second flight control agent;
FIG. 7 is a schematic diagram of a composite display agent, task load agent, and link monitor agent layout.
The reference numerals in the drawings mean:
1. a storage box; 2. an integrated air conditioner; 3. a second lighting window; 4. a power supply hole door; 5. a sunshade; 6. an air outlet; 7. an oil engine heat dissipation window; 8. a storage compartment door; 9. an interactive display device; 10. a link bay door; 11. a first lighting window; 12. an entrance and exit door; 13. an air inlet; 14. a first flight control agent; 15. a second flight control agent; 16. a comprehensive display mat; 17. a task load mat; 18. a link monitor agent; 19. an air duct; 20. a link access port; 21. a remote control panel; 22. a storage bin; 23. an oil engine compartment; 24. a link bay; 25. an air outlet; 26. a temperature and humidity clock; 27. a coat hook; 28. 4G/5G antenna; 29. a weather instrument; 30. a U-band antenna; 31. a manual lifting rod; 32. climbing a ladder; 33. an oil engine mounting door; 34. boarding a cabin ladder; 35. a GPS antenna; 36. a lodging device; 37. a motorized top cover; 38. a link antenna; 39. a cradle head lodging device; 40. cloud platform camera.
The utility model is further explained below with reference to the drawings and the detailed description.
Detailed Description
As shown in fig. 1 to 5, the shelter for the ground command control system of the unmanned aerial vehicle provided by the utility model comprises a cabin body, wherein the front part in the cabin body is a working cabin, the storage cabin 22 and the link cabin 24 which are arranged on the left and right are respectively arranged above the rear part in the cabin body, and the oil cabin 23 is arranged below the rear part. Wherein, install the oil engine in the oil engine cabin 23, the oil engine is used for commander control system's emergency power supply to use, installs the link antenna in the link cabin 24, and the storing cabin 22 is used for storing article annex.
A first flight control seat 14 and a second flight control seat 15 are arranged in parallel at the front end in the working cabin, and a comprehensive display seat 16, a task load seat 17 and a link monitoring seat 18 are arranged in parallel at the rear end; the left side wall of the cabin body is provided with an oil engine heat dissipation window 7, the right side wall of the cabin body is provided with a link cabin door 10, and a remote control panel 21 is arranged in the right side wall of the cabin body.
The outer wall of one side of the cabin body is provided with a manual lifting rod 31 for installing the U-band antenna 30; the outer side of the top of the cabin body is respectively provided with a 4G/5G antenna 28, a GPS antenna, a weather instrument 29 and a tripod head lodging device 39 for installing a tripod head camera 40; the outer wall of the rear end of the cabin body is provided with an oil engine mounting door 33. The top plate above the link cabin 24 is provided with a link access opening 20.
In the scheme, a first flight control seat 14 and a second flight control seat 15 are used for operating the unmanned aerial vehicle and monitoring various parameters and instructions of the unmanned aerial vehicle, a comprehensive display seat 16 is used for displaying display pictures of all other seats (namely the first flight control seat 14, the second flight control seat 15, a mission load seat 17 and a link monitoring seat 18) in the cabin body through an interactive display device 9, the interactive display device 9 is used for enabling personnel outside the cabin body to better monitor various parameters of the unmanned aerial vehicle, the mission load seat 17 is used for monitoring parameters and instructions of load equipment hung on an aircraft platform and operating the load equipment when the unmanned aerial vehicle carries out a mission, and the link monitoring seat 18 is used for monitoring the communication quality of a link; the oil engine heat dissipation window 7 is used for quickly dissipating heat generated in the working process of the oil engine; the link cabin door 10 is used for facilitating the opening of the link cabin 24 for operation; the remote control panel 21 is used for facilitating the control of the power supply of each power supply device in the cabin body by the working personnel; the manual lifting rod 31 is used for installing and controlling the U-band antenna 30 to lift; the GPS antenna 35 is used for communication between the differential device and a satellite, and the 4G/5G antenna 28 is used for communication between a control system applied by the utility model and a 4G/5G wireless network of an external environment; cloud platform camera 40 is convenient for under-deck staff to observe outside unmanned aerial vehicle runway situation. The link gateway 20 is used for data interaction between link equipment in the cabin and the link cabin 24.
Preferably, the left side wall of the cabin body is provided with a second lighting window 3, a power supply hole door 4, an air outlet 25 and a storage bin door 8, a frame body for installing interactive display equipment 9 is arranged outside the left side wall, and the interactive display equipment 9 is connected with the comprehensive display mat 16 and used for displaying the content of the interactive display equipment; the right side wall of the cabin body is provided with an air inlet 13, an access door 12 and a first lighting window 11. The first lighting window 11 and the second lighting window 3 are used for providing light rays for the working cabin, the power supply hole door 4 is used for conveniently providing power distribution for all electric equipment in the cabin, and the air outlet 25 and the air inlet 13 are used for keeping air in the cabin smooth; the access door 12 is used to facilitate opening of the working compartment for operation.
Preferably, the inner wall of the left side of the cabin body is provided with a hat and coat hook 27, so that the use by workers is facilitated.
Preferably, the integrated air conditioner 2 is arranged at the front end of the cabin body, the inner wall of the left side of the cabin body is provided with a temperature and humidity clock 26, and the top of the cabin body is provided with an air duct 19 connected with the integrated air conditioner 2, which are jointly used for controlling the environment in the cabin body.
Preferably, the outer wall of the front end of the cabin body is provided with a boarding ladder 34, the outer wall of the rear end of the cabin body is provided with a top climbing ladder 32, the boarding ladder 34 is convenient for workers to enter the shelter, and the top climbing ladder 32 is used for facilitating the workers to climb the cabin top for operation.
Preferably, an electric top cover 37 is provided on the link entrance 20 of the link compartment 24, and an electric lifting mechanism for installing a link antenna 38 is provided in the link compartment 24. In this manner, the link antenna 38 can be raised and lowered by the motorized lift mechanism by opening the motorized top cover 37.
Preferably, the top of the cabin is provided with a sunshade for shielding all components on the top of the cabin.
Preferably, the utility model further comprises a chassis truck, wherein the chassis truck is arranged below the cabin body through the auxiliary frame and used for realizing that the cabin body freely moves to a proper working place, and the maneuvering performance of the ground command control system is effectively improved. And a storage box is also arranged on the auxiliary frame.
Specifically, as shown in fig. 6, the first flight control agent 14 and the second flight control agent 15 are provided in the same manner, specifically as follows: the flight control device comprises a flight operation platform with the size of 1100mm multiplied by 825mm multiplied by 1689mm, and a flight control computer and a matched keyboard, a mouse, an accelerator lever, a rocker and a pedal thereof are arranged on the flight operation platform; the flight control computer is provided with 2 24-inch displays and 3 21.5-inch displays; a first flight control computer of the first flight control seat 14 and a second flight control computer of the second flight control seat 15 form a rack-mounted server to form an internally closed data operation system; as shown in fig. 7, the console sizes of the integrated display agent 16, the task load agent 17 and the link monitor agent 18 are 2100mm × 850m × 1758, and a keyboard, a mouse and three 24-inch displays are all mounted on the console sizes; the link monitor agent 16 is also equipped with a picture splitter; a link computer of the comprehensive display position 16, a task load computer of the task load position 17 and an application server of the link monitoring position 18 form a rack server to form an internally closed data operation system; the shock pad and the channel-section steel are all installed to the below all around of operation panel, conveniently dismantle and maintain, and such design makes the cabin body install also can not influence its whole operating efficiency and performance on moving platform.
Claims (9)
1. The shelter for the ground command control system of the unmanned aerial vehicle comprises a cabin body and is characterized in that a working cabin is arranged at the front part in the cabin body, a storage cabin (22) and a link cabin (24) which are arranged on the left and right are respectively arranged above the rear part in the cabin body, and an oil cabin (23) is arranged below the rear part in the cabin body; a first flight control seat (14) and a second flight control seat (15) are arranged at the front end in the working cabin in parallel, and a comprehensive display seat (16), a task load seat (17) and a link monitoring seat (18) are arranged at the rear end in parallel; the left side wall of the cabin body is provided with an oil engine heat dissipation window (7), the right side wall of the cabin body is provided with a link cabin door (10), and a remote control panel (21) is arranged in the right side wall of the cabin body;
a manual lifting rod (31) for installing a U-band antenna (30) is arranged on the outer wall of one side of the cabin body; the outer side of the top of the cabin body is respectively provided with a 4G/5G antenna (28), a GPS antenna (35), a weather instrument (29) and a tripod head lodging device (39) for installing a tripod head camera (40); the outer wall of the rear end of the cabin body is provided with an oil engine mounting door (33); and a link access (20) is arranged on the top plate above the link cabin (24).
2. The shelter for the ground command and control system of the unmanned aerial vehicle according to claim 1, wherein a second lighting window (3), a power supply hole door (4), an air outlet (25) and a storage bin door (8) are formed on the left side wall of the shelter body, a frame body for installing interactive display equipment (9) is arranged outside the left side wall, and the interactive display equipment (9) is connected with the comprehensive display seat (16); the right side wall of the cabin body is provided with an air inlet (13), an access door (12) and a first lighting window (11).
3. The shelter for ground command and control system of unmanned aerial vehicle according to claim 1, wherein the inner wall of the left side of the shelter body is provided with a coat hook (27).
4. The shelter for the ground command and control system of the unmanned aerial vehicle according to claim 1, wherein the front end of the shelter body is provided with an integrated air conditioner (2), the inner wall of the left side of the shelter body is provided with a temperature and humidity clock (26), and the top of the shelter body is provided with an air duct (19) connected with the integrated air conditioner (2).
5. The shelter for the ground command and control system of the unmanned aerial vehicle as claimed in claim 1, wherein the outer wall of the front end of the shelter body is provided with a boarding ladder (34), and the outer wall of the rear end of the shelter body is provided with a boarding ladder (32).
6. The shelter for the ground command and control system of the unmanned aerial vehicle as claimed in claim 1, wherein an electric top cover (37) is arranged on the link access opening (20) of the link cabin (24), and an electric lifting mechanism for installing a link antenna (38) is arranged in the link cabin (24).
7. The shelter of claim 1, wherein a sunshade is provided on the top of the shelter.
8. The shelter of claim 1, further comprising a chassis mounted below the shelter via a sub-frame.
9. The shelter for the ground command control system of unmanned aerial vehicle according to claim 1, wherein the first flight control seat (14) and the second flight control seat (15) are arranged identically, comprising a flight console on which a flight control computer and its associated keyboard, mouse, throttle lever, rocker and pedal are arranged; the flight control computer is provided with a plurality of displays; and the operation platforms of the comprehensive display seat (16), the task load seat (17) and the link monitoring seat (18) are all provided with a keyboard, a mouse and a plurality of displays.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220191527.7U CN216886422U (en) | 2022-01-24 | 2022-01-24 | Shelter for ground command control system of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220191527.7U CN216886422U (en) | 2022-01-24 | 2022-01-24 | Shelter for ground command control system of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216886422U true CN216886422U (en) | 2022-07-05 |
Family
ID=82180723
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220191527.7U Active CN216886422U (en) | 2022-01-24 | 2022-01-24 | Shelter for ground command control system of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216886422U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443302A (en) * | 2023-06-16 | 2023-07-18 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
-
2022
- 2022-01-24 CN CN202220191527.7U patent/CN216886422U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443302A (en) * | 2023-06-16 | 2023-07-18 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
| CN116443302B (en) * | 2023-06-16 | 2023-09-05 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle comprehensive guarantee vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106060451B (en) | Sea area unmanned aerial vehicle monitoring mobile platform | |
| CN105223958A (en) | A kind of emergency communication based on captive unmanned plane and support system and method | |
| US8127333B2 (en) | Device for imaging an aircraft cabin | |
| CN216886422U (en) | Shelter for ground command control system of unmanned aerial vehicle | |
| CN103072693A (en) | Cockpit of an aircraft comprising a folding seat | |
| CN217099804U (en) | Convenient vehicle-mounted unmanned aerial vehicle platform and unmanned aerial vehicle system | |
| CN206107055U (en) | Field operations shelter arsenal | |
| CN217099805U (en) | Vehicle-mounted take-off and landing system of unmanned aerial vehicle | |
| CN106274618A (en) | Car is dispersed in patrol | |
| CN214823680U (en) | Fire engine based on unmanned aerial vehicle | |
| CN113200093A (en) | Fire engine based on unmanned aerial vehicle | |
| CN107672503A (en) | Unmanned aerial vehicle remote sensing emergency monitoring and commanding vehicle | |
| CN114363391A (en) | Unmanned aerial vehicle ground command control system | |
| CN115801105B (en) | One-vehicle one-stop type high-integration maneuvering measurement and control station | |
| CN219918930U (en) | One-vehicle one-stop type high-integration maneuvering measurement and control station | |
| CN210363538U (en) | Open-air removal telemetry station | |
| CN213109143U (en) | Unmanned aerial vehicle command vehicle supporting storage and retraction of multiple unmanned aerial vehicles | |
| CN110884677A (en) | A winding and unwinding devices for mooring unmanned aerial vehicle | |
| CN216186130U (en) | Parking apron and parking system | |
| CN209640707U (en) | A kind of vehicle-mounted unmanned aerial vehicle ground control system | |
| CN209224072U (en) | A kind of security patrol robot mobile command center | |
| CN221256271U (en) | Unmanned aerial vehicle middle-range ground station suitable for helicopter air transport | |
| CN112428908A (en) | Portable intelligent inspection vehicle of transmission line unmanned aerial vehicle | |
| CN217706334U (en) | System for refitting upper single-wing aircraft into unmanned aerial vehicle | |
| CN115258190B (en) | Design method and system for refitting unmanned aerial vehicle system by upper single-wing aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |