Unmanned aerial vehicle command and control square cabin working unit

Abstract

The utility model discloses an unmanned aerial vehicle command and control shelter working unit. The unmanned aerial vehicle command and control shelter working unit comprises a shelter body, and a flight control seat, an emergency monitoring seat and a situation display and control temporary seat which are arranged in the shelter body. The flight control seat is located at one end of the shelter body, the emergency monitoring seat is located at the other opposite end of the shelter body, and the situation display and control temporary seat is located in the middle of the shelter body. The top wall of the shelter body above the flight control seat and the emergency monitoring seat is an integrated ceiling, and the integrated ceiling is provided with a seat panel light, a seat camera and a seat air-conditioning port. The seat panel lamp has the advantages that the seat panel lamp, the seat camera and the seat air-conditioning port are integrated together, so that the seat panel lamp is compact in layout, convenient to install and beneficial to later maintenance.

Description

Technical Field

[0001] The utility model relates to a command and control shelter, and in particular to a working unit of an unmanned aerial vehicle (UAV) command and control shelter. Background Art

[0002] The working unit of the UAV command and control station is the working area where operators achieve long-endurance control of UAVs. The current disadvantages of the existing working unit of the UAV command and control station are as follows: the layouts of the top monitoring and top lighting are relatively scattered, and the installation is inconvenient. Summary of the Invention

[0003] The purpose of the utility model is to provide a new working unit of an unmanned aerial vehicle command and control shelter.

[0004] To achieve the above purpose, a technical solution provided by the utility model is: a working unit of an unmanned aerial vehicle command and control shelter, including: a shelter body and a flight control seat, an emergency monitoring seat and a situation display and control temporary seat inside the shelter body; the flight control seat is at one end of the shelter body, the emergency monitoring seat is at the opposite end of the shelter body, and the situation display and control temporary seat is at the middle position of the shelter body; the top wall of the shelter body above the flight control seat and the emergency monitoring seat is an integrated ceiling, and the integrated ceiling is provided with a seat flat lamp, a seat camera and a seat air-conditioning outlet.

[0005] As a preferred scheme of the working unit of the unmanned aerial vehicle command and control shelter, the seat air-conditioning outlet includes: an air outlet, and the air outlet adopts an inclined air outlet design.

[0006] As a preferred scheme of the working unit of the unmanned aerial vehicle command and control shelter, it further includes: a fisheye camera inside the shelter body, and the fisheye camera is at the middle position of the top wall of the shelter body.

[0007] As a preferred scheme of the working unit of the unmanned aerial vehicle command and control shelter, it further includes: a smoke detector and a warning lamp inside the shelter body, the smoke detector is at the middle position of the top wall of the shelter body, the warning lamp is on the side wall of the shelter body, and the smoke detector is communicatively connected with the warning lamp.

[0008] As a preferred scheme of the working unit of the unmanned aerial vehicle command and control shelter, the flight control seat and the emergency monitoring seat have the same hardware configuration, and the hardware configuration includes: an aviation seat and a movable display and control console.

[0009] Compared with the prior art, the beneficial effects of the utility model are at least that: the flight control seat, the emergency monitoring seat and the temporary seat for situation display and control are designed at the position of the cabin body, in order to ensure that the center of gravity of the cabin body is centrally distributed and the hoisting is safer. The seat flat panel light, the seat camera and the seat air conditioning port are integrated together, in order to achieve a compact layout, convenient installation, and facilitate later maintenance. The air outlet of the seat air conditioning port adopts an oblique air outlet design, in order to avoid direct blowing of the flight control seat or the emergency monitoring seat below. The smoke alarm and the warning light alarm can be linked to ensure the safety inside the cabin body. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Figure 1 It is a top view of the working unit of the embodiment of the utility model.

[0011] Figure 2 It is a left side view of the working unit of the embodiment of the utility model.

[0012] Figure 3 It is a right side view of the working unit of the embodiment of the utility model.

[0013] Figure 4 It is a front side view of the working unit of the embodiment of the utility model.

[0014] Figure 5 It is a top view of the working unit of an embodiment of the utility model.

[0015] Figure 6 It is a lighting and alarm cross-linking diagram of an embodiment of the utility model. DETAILED DESCRIPTION

[0016] The present invention is further described in detail below through specific implementations in combination with the accompanying drawings. It should be noted that the description of these implementations is used to help understand the present invention, but does not constitute a limitation of the present invention. In addition, the technical features involved in each implementation of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0017] See also Figures 1 to 5 , the figure shows a UAV command and control cabin work unit. The UAV command and control cabin work unit is the working area for operators to control the UAV.

[0018] The command ruler control shelter work unit includes: a shelter body and a flight control seat 1, an emergency monitoring seat 2, a situation display and control temporary seat 3, a lighting and warning module 4, an integrated ceiling 5, a seat camera 6, a fish-eye camera 7, an air conditioner 8, a ventilation device 9, a daylighting window 10, a double-leaf door of the work unit 11, a fire extinguisher 12, a wall socket 13, a mooring ring 14, and a floor drain 15 inside the shelter body.

[0019] The flight control seat 1 and the emergency monitoring seat 2 are symmetrically arranged. The flight control seat 1 is at one end of the shelter body. The emergency monitoring seat 2 is at the opposite end of the shelter body. The flight control seat 1 and the emergency monitoring seat 2 have the same hardware configuration. The hardware configuration includes: a curved screen 101, a touch screen 102, an instruction control box 103, a ruggedized tablet computer 104, a control stick 105, a throttle lever 106, a keyboard and mouse assembly 107, an aviation seat 108, a movable display and control console 109, and a seat computer 110.

[0020] During specific implementation, the curved screen 101 is a 37.5-inch ruggedized curved screen, and the maximum resolution supports 3840×1600. The touch screen 102 is a 21.5-inch ruggedized touch display, and the maximum resolution supports 1920×1080. The instruction control box 103 is configured with 10 function buttons and supports OLED display. The ruggedized tablet computer 104 is a multi-touch capacitive screen and uses anti-glare AG glass. The control stick 105 has two groups of independent continuous quantity outputs for pitch and roll, and the total stroke of the joystick for roll and pitch is ±10°. The throttle lever 106 supports two operation modes of single-engine and twin-engine, and the number of buttons is no more than 6. The keyboard in the keyboard and mouse assembly 107 selects a blue switch keyboard, and the mouse selects an optical mouse. The aviation seat 108 is modified from an e-sports seat, and the backrest angle, handrest angle, height, seat height, front-back, and left-right positions are adjustable. The movable display and control console 109 is configured with mobile wheels and a locking mechanism and supports short-distance self-propelled movement. The seat computer 110 is installed on the right side of the bottom leg of the movable display and control console 109, facilitating the operator to turn on and off the machine normally.

[0021] The situation display and control temporary seat 3 is in the middle of the shelter body. The hardware configuration of the situation display and control temporary seat 3 includes: a keyboard and mouse assembly 301, a folding table 302, a situation display large screen 303, and a situation computer.

[0022] In specific implementation, the keyboard in the keyboard and mouse assembly 301 uses a blue-axis keyboard, and the mouse uses an optical mouse. The folding table 302 adopts a sheet metal structure, which can accommodate the keyboard and mouse assembly 301 and has self-locking function. The situation display large screen 303 is a 32-inch touch display with a maximum resolution of 1920×1080 and a power consumption of no more than 600W. The situation computer is installed in the equipment compartment and is connected to the situation display large screen via HDMI and USB cables.

[0023] The lighting and warning module 4 includes a seat panel light 401, an aisle panel light 402, a smoke alarm 403, a sound system 404, a warning light 405, a door limiter 406 and a control host.

[0024] During the specific implementation, the seat flat panel lamp 401 and the aisle flat panel lamp 402 both use cold, warm and blue three-channel lighting flat panel lamps, taking into account the emergency function. The size of the seat flat panel lamp 401 (length × width × thickness): 600 × 300 × 13mm, which is used to illuminate the seat. The size of the aisle flat panel lamp 402 (length × width × thickness): 600 × 600 × 13mm, which is used to illuminate the aisle. The lamp is fixed to the groove of the interior ceiling panel and is fixed by the structural parts of the interior panel, so that the interior surface is flush with the light-emitting surface. The smoke alarm 403 is powered by DC24V. The audio 404 is installed in a ceiling-mounted manner, and the power of the amplifier does not exceed 80W. The light emission direction of the warning light 405 is parallel to the bulkhead and is equipped with a sunshade. The warning light halo is soft, achieving the effect of seeing the light but not the lamp. The warning light is configured in red and yellow. The color of the 1st level alarm is red, and the flashing frequency is 2Hz (the duty ratio of light and dark is 0.5 each); the color of the 2nd level alarm is yellow, and the flashing frequency is 2Hz (the duty ratio of light and dark is 0.5 each). Both alarm modes flash continuously until the alarm is eliminated. The control host is installed on the equipment compartment cabinet and does not occupy the work unit space.

[0025] The top wall of the cabin body is provided with the seat camera 6 at the position of the flight control seat 1 and the emergency monitoring seat 2. The seat camera 6 is a camera with zoom and sound pickup functions. The monitoring range of the seat camera 6 covers the lower position.

[0026] A fisheye camera 7 is provided in the middle area of the top wall of the square cabin body. The fisheye camera 7 is a camera with a sound pickup function. The monitoring range of the fisheye camera 7 covers all positions inside the square cabin body.

[0027] In specific implementation, the seat camera 6 and the fisheye camera 7 are connected to a hard disk video recorder via a Category 6 shielded network cable, and can be accessed through the seat computer 110 to obtain monitoring audio and video information.

[0028] The top wall of the shelter body is equipped with a ceiling-mounted air conditioner, which is selected according to the space size of the working unit. The ceiling-mounted air conditioner has an outdoor unit, an air return opening 801 and an air outlet 802. The air outlet 802 adopts an oblique air outlet design to prevent the air conditioner from blowing directly at the operators.

[0029] During specific implementation, 2 ceiling-mounted air conditioners are selected, and the cooling capacity of a single unit is 4500W.

[0030] The side wall of the shelter body is equipped with a ventilation device 9, which has an axial flow fan, a ventilation window and a waveguide plate.

[0031] During specific implementation, the waveguide plate is shielded to ensure that the electromagnetic shielding efficiency of the shelter can reach 0.15MHz - 10GHz and is not less than 40dB.

[0032] The side wall of the shelter body is equipped with daylighting windows 10, which are symmetrically arranged. The side wall of the shelter body has an access door. The access door 11 is selected as a double-leaf door.

[0033] During specific implementation, the net size (width × height) of the access door 11 is 1400×1800mm to ensure that the entire movable display and control console can smoothly enter and exit the cabin. 2 fire extinguishers 12 are installed on the door. 3 groups of mooring rings 14 and 1 floor drain 15 are arranged at the bottom of the working unit cabin.

[0034] There are wall sockets 13 on the side wall of the shelter body at the positions of the flight control seat 1, the emergency monitoring seat 2 and the situation display and control temporary seat 3.

[0035] During specific implementation, the wall socket 13 is selected as 10A AC220V.

[0036] Figure 1 This is a top view of the working unit. The lighting and warning module 4 and the suspended ceiling 5 are symmetrically arranged. 4 speakers 404 are respectively installed at the four corners of the working unit. An integrated suspended ceiling 5 is set above the unilateral seat, integrating an air return opening 801, an air outlet 802, 2 seat cameras and 2 seat flat lights. 1 aisle flat light 402, 1 fisheye camera 7 and 1 smoke detector 403 are set above the aisle of the working unit.

[0037] Figure 2 This is a left side view of the working unit. The seats are symmetrically arranged. 1 daylighting window 10 and 1 wall socket 13 are set beside each seat. 1 ventilation window is set above the rear side of the working unit for air outlet. 1 situation display and control temporary seat 3 is set in the middle of the left wall.

[0038] Figure 3It is the right side view of the working unit. The seats are symmetrically arranged. One lighting window 10 and one wall socket 13 are set beside each seat. One ventilation window is set at the lower front side of the working unit for air intake. One double-door 11 is set on the right wall of the working unit, and two fire extinguishers 12 are installed on the cabin door.

[0039] Figure 4 It is the front side view of the working unit. Two warning lights are embedded in the single-side bulkhead, and the light-emitting direction is parallel to the bulkhead.

[0040] Figure 5 It is the top view of the working unit. The seats are symmetrically arranged to ensure that the center of gravity of the working unit is centered. Three pairs of mooring rings 14 and one floor drain 15 are set at the bottom. Temporary cable reels and sundry boxes can be fixed to the mooring rings 14 through straps.

[0041] Figure 6 It is the cross-linking diagram of lighting and warning. The central control host controls the parameters such as luminous flux and light color of the seat flat lights 401 and aisle flat lights 402 in the working unit, realizes the multi-mode intelligent control function of the lights, and meets the diverse lighting requirements inside the working unit, including working mode, emergency mode, air defense mode, and warning mode, etc. The emergency lighting is integrated in the aisle flat lights and is powered by an emergency power supply. The control panel realizes the opening and closing of the emergency lighting through the main controller. When the lighting control panel is in the air defense mode and the cabin door limit 406 is opened, the power supply of the blue light lighting circuit is connected, and the seat flat lights 401 and aisle flat lights 402 in the working unit emit uniform blue light at the same time; when the cabin door is closed, the circuit power supply is connected, and the lighting inside the cabin returns to the white light working state. In the warning control mode, mainly four warning lights 405, four sounders 404 and one smoke detector 403 are used for linkage operation. The seat computer and the central control host are connected to the switch through network cables. The operator can control the sound and light alarm of the warning lights 405 and sounders 404 through the upper computer software of the seat computer 110. When there is thick smoke in the working unit, the smoke detector 403 gives a sound and light prompt and links the four warning lights 405 on the bulkhead to realize the alarm.

[0042] The above only expresses the implementation modes of the present utility model, and its description is relatively specific and detailed, but it cannot be understood as a limitation to the scope of the utility model patent. It should be noted that for those of ordinary skill in the art, without departing from the concept of the present utility model, several deformations and improvements can still be made, and these all belong to the protection scope of the present utility model. Therefore, the protection scope of the present utility model patent shall be subject to the appended claims.

Claims

1. A working unit of a UAV command and control shelter, characterized in that Including: A shelter body, a flight control seat, an emergency monitoring seat and a situation display and control temporary seat inside the shelter body; the flight control seat is at one end of the shelter body, the emergency monitoring seat is at the opposite end of the shelter body, and the situation display and control temporary seat is in the middle position of the shelter body; the top wall of the shelter body above the flight control seat and the emergency monitoring seat is an integrated ceiling, and the integrated ceiling is equipped with seat flat lights, seat cameras and seat air-conditioning outlets.

2. The working unit of the UAV command and control shelter according to claim 1, wherein The seat air-conditioning outlet includes: an air outlet, and the air outlet adopts an inclined air outlet design.

3. The working unit of the UAV command and control shelter according to claim 1, characterized in that, It also includes: A fish-eye camera inside the shelter body, and the fish-eye camera is in the middle position of the top wall of the shelter body.

4. The working unit of the UAV command and control shelter according to claim 1, characterized in that, It also includes: A smoke detector and an alarm lamp inside the shelter body, the smoke detector is in the middle position of the top wall of the shelter body, the alarm lamp is on the side wall of the shelter body, and the smoke detector is communicatively connected to the alarm lamp.

5. The working unit of the UAV command and control shelter according to claim 1, characterized in that The flight control seat and the emergency monitoring seat have the same hardware configuration, and the hardware configuration includes: an aviation seat and a movable display and control console.

Images