An unmanned aerial vehicle emergency command unit system

Abstract

This invention discloses an unmanned aerial vehicle (UAV) emergency command unit system. The UAV emergency command unit system includes: a container and an environmental control subsystem and an electronic power supply system (i.e., a data processing subsystem) inside the container; the container subsystem has one or more of the following: a conference table, a display console, a folding chair, storage cabinets, equipment cabinets, fire extinguishers, a whiteboard, a water dispenser, and fixed emergency lights; the environmental control subsystem has one or more of the following: a split-type air conditioner, wall-mounted lighting, and an exhaust fan assembly; the data processing subsystem has one or more of the following: a telephone, a computer, a monitor, a printer, a large display screen, a switch, a router, a ruggedized laptop, and a keyboard and mouse. The beneficial effects of this invention are: it requires no deployment or collection, can be used directly, provides a comfortable environment for field meetings, command, and UAV monitoring, and improves operational efficiency.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicles (UAVs), and in particular, to an UAV emergency command unit system. Background Technology

[0002] Ensuring the normal operation of drones typically involves remote areas. Therefore, operators need to carry a significant amount of research equipment (such as laptops, UPS systems, batteries, folding tables and chairs) to the site. Deployment and recovery operations alone consume a substantial amount of the operators' time and energy. Summary of the Invention

[0003] The technical problem to be solved by this invention is that on-site deployment and collection occupy a lot of time and energy of operators, and provides an emergency command unit system for unmanned aerial vehicles.

[0004] To address the aforementioned technical problems, the present invention provides a technical solution: Compared with the prior art, the beneficial effects of the present invention are at least as follows: it can be used directly without deployment or collection, providing a comfortable support environment for field meetings, command and control, drone monitoring, etc., and improving operational efficiency.

[0005] In addition to the technical problems solved by the present invention, the technical features constituting the technical solutions, and the beneficial effects brought about by the technical features of these technical solutions as described above, other technical problems that the present invention can solve, other technical features contained in the technical solutions, and the beneficial effects brought about by these technical features will be further described in detail with reference to the accompanying drawings. Attached Figure Description

[0006] Figure 1 This is a top view of the unit system in an embodiment of the present invention.

[0007] Figure 2 This is a left wall view of the unit system in an embodiment of the present invention.

[0008] Figure 3 This is a right wall view of the unit system in an embodiment of the present invention.

[0009] Figure 4 This is a front wall view of the unit system in an embodiment of the present invention.

[0010] Figure 5 This is a rear wall view of the unit system in an embodiment of the present invention.

[0011] Figure 6 This is an internal top view of the unit system in an embodiment of the present invention.

[0012] Figure 7 This is an internal right view of the unit system in an embodiment of the present invention.

[0013] Figure 8This is an internal left-side view of the unit system in an embodiment of the present invention.

[0014] Figure 9 This is an internal top view of the unit system in an embodiment of the present invention.

[0015] Figure 10 This is an internal front view of the unit system in an embodiment of the present invention.

[0016] Figure 11 This is an internal rear view of the unit system in an embodiment of the present invention.

[0017] Figure 12 It is an adapter board inside the power / signal port in an embodiment of the present invention.

[0018] Figure 13 This is a crosslinking diagram of an embodiment of the present invention. Detailed Implementation

[0019] The present invention will now be described in further detail with reference to specific embodiments and accompanying drawings. It should be noted that these descriptions of embodiments are intended to aid in understanding the invention and do not constitute a limitation thereof. Furthermore, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other.

[0020] This embodiment is designed based on an 8m container body 1, without a chassis, and uses a standard semi-trailer for transportation. The container body dimensions are 8000×2500×2200mm.

[0021] Figures 1-5 For the external layout of the container. Figure 1 This is a top view of the container. A pair of handles 101 are arranged diagonally on the top of the container. Figure 2 This is a view of the left side of the container. The left side of the container has one light-transmitting window 102, one exhaust fan, and two air inlets. The net dimensions (width × height) are 160 × 160 mm. Four sets of folding ramps 104 are located at the rear. Figure 3 This is a view of the right side of the container. Four sets of folding ramps 104 are arranged at the front, followed by one skylight 102 and one main access door 105, with net dimensions (width × height): 800 × 1800 mm. A cabinet maintenance door 103 with net dimensions (width × height): 485 × 1800 mm is installed at the rear. Figure 4 This is a view of the front wall of the container. Two air conditioner outdoor units 301 are fixed above by brackets. Figure 5This is a view of the rear wall of the container. An exhaust fan with two outlets is installed at the upper left, with net dimensions (width × height): 160 × 160 mm. There is a rear access door 106 in the middle. A power / signal port 107 is installed at the lower right, containing a power / signal adapter board with aviation connectors and lightning protection devices, with net dimensions (width × height): 400 × 400 mm.

[0022] Figures 6-11 The internal layout of the container. Figure 6 This is a top view of the container interior. Ten wall-mounted lights 4 are symmetrically and evenly arranged on the top, with net dimensions (length × width): 600 × 200 mm and a thickness of 13 mm. The wall-mounted lights 4 are controlled by a lighting switch 401 on the side of the main access door. Figure 7 This is a right-hand view of the container interior. The front section is a meeting area, with a wall-mounted air conditioner unit 302 installed in the upper left corner; the main access door 105 is in the middle, with two fire extinguishers 5 installed on the door, and a telephone 6 and a lighting switch 401 installed in front of the door frame; behind the door is a set of 5-seat display consoles 11, with 10 monitors 9, 5 sets of keyboards and mice 7, and 5 computers 11 integrated on each seat; below the seats is storage space for folding chairs 10, with straps and hanging points for the folding chairs; above the seats is a row of shelves 8, which can temporarily store documents and miscellaneous items; behind the seats is an equipment cabinet 13; the cabinet houses routers 21, switches 22, power distribution boxes 23, UPS main units 24, and UPS batteries 25, among other equipment. Figure 8 This is a left-side view of the container interior. The upper part shows the air duct 108 connecting the outdoor and indoor units of the air conditioner. At the rear is a storage cabinet 17 (No. 2) for storing cable reels 109 and other miscellaneous items. Above the storage cabinet is a printer 16; in the upper corner is an indoor air conditioner unit 302; in the middle is a five-seat control console 12, integrating ten monitors 9, five sets of keyboards and mice 7, and five computers 11; below the seats is storage space for folding chairs 10; above the seats is a row of shelves 8; the overall frame of the control console 12 is welded from Q235 square tubing, with a cold-rolled steel sheet covering the surface. The monitors 9 are arranged with upper and lower screens. The mouse is embedded in the desktop. A cover is placed above the base; when the mouse is needed, it can be opened directly through a hole in the cover to remove it. When the mouse is in use, the cover is lowered to form a flat surface with the desktop for easy use. The keyboard lies flat on the table, secured by a frame that uses stainless steel countersunk screws. The keycaps are exposed for easy access and to maintain keyboard stability during vibrations and impacts. A shelf 8, made of MDF, is mounted above the seating area and secured to the bulkhead with a tripod. A computer 11 is mounted below the table using brackets. A water dispenser 15 and a wall socket 16 are located in the center; a whiteboard 14 is mounted on the bulkhead; and the meeting area is at the front.

[0023] Figure 9 This is a top-down view of the container's interior. The interior is divided into a meeting area and an operating area. The meeting area is located at the front, while the operating areas are located at the rear on the left and right sides. At the front of the meeting area is a large display screen 18, below which is storage cabinet 19 (No. 1). In the center is a conference table 20, measuring (length × width × height): 2000 × 800 × 760 mm, used to house ruggedized laptops 19 for convenient work by staff. The tabletop 20 is made of cold-rolled steel sheet, bent and formed, with a powder-coated surface. Two sockets are located in the center of the table, providing 220V power outlets for ruggedized laptops and other peripherals, as well as an RJ45 network interface. The operating area includes two five-seat control consoles 12 and ten folding chairs 10. Equipment cabinets 13 are located at the rear. Figure 10 This is a front view of the container's interior. A 75-inch display screen is installed in the center of the front wall, and below the screen is storage locker #1. Figure 11 This is a view of the rear interior of the container. A rear access door (106) is located in the center of the rear, with two fire extinguishers (5) hanging on it.

[0024] Figure 12 This diagram shows the layout of the adapter board within the power / signal ports, including two network ports, one telephone port (red and black terminals), one AC220V critical power input, one AC220V auxiliary power input, and one grounding terminal. The AC220V critical power supply primarily powers devices such as computers, monitors, printers, large display screens, routers, switches, and ruggedized laptops. The AC220V auxiliary power supply powers wall-mounted lights, exhaust fan assemblies, spare sockets, and air conditioners.

[0025] Figure 13 This is the system interconnection diagram. Two mains power lines are introduced externally to the enclosure: one for critical equipment and one for auxiliary equipment. The critical equipment mains power line supplies power to the critical equipment via the distribution box and UPS. If the external power supply suddenly fails, the UPS main unit and UPS battery will operate to supply power to the critical equipment. The auxiliary equipment mains power line supplies power to auxiliary equipment, mainly exhaust fan assemblies, wall-mounted lights, wall sockets, and air conditioners, via the distribution box. External signals are transmitted to the telephone inside the enclosure via the red and black terminals on the adapter board. The external network is connected to the large display screen, printer, ruggedized laptop, and computer inside the enclosure via a router and switch. Operators use ruggedized laptops and computers for work, and can project images onto the large display screen via the switch, or connect to the printer to print field mission content. Each computer is equipped with two monitors for UAV attitude and intelligence display.

[0026] The above description merely illustrates embodiments of the present invention and is quite specific and detailed; however, it should not be construed as limiting the scope of the invention. It should be noted that those skilled in the art can make various modifications and improvements without departing from the inventive concept, and these all fall within the scope of protection of the present invention. Therefore, the scope of protection of this invention should be determined by the appended claims.

Claims

1. A drone emergency command unit system, characterized in that, include: The container and its internal environmental control subsystem, power supply system, and data processing subsystem; the container subsystem includes one or more of the following: conference table, display console, folding chair, storage cabinet, equipment cabinet, fire extinguisher, whiteboard, water dispenser, and fixed emergency light; the environmental control subsystem includes one or more of the following: split-type air conditioner, wall-mounted lighting, and exhaust fan assembly; the data processing subsystem includes one or more of the following: telephone, computer, monitor, printer, large display screen, switch, router, ruggedized laptop, and keyboard and mouse.

2. The UAV emergency command unit system of claim 1, wherein, The container adopts a right-angled corrugated plate structure, which is assembled and welded from the front, back, left, right, top and bottom plates, corner pieces and beams.

3. The UAV emergency command unit system of claim 1, wherein, The container's interior is divided into a meeting area and an operating area, accommodating multiple people working simultaneously. The front features a large display screen, with storage cabinets below for ruggedized laptops. The meeting table is equipped with folding chairs for impromptu meetings and command and control. The control console features a five-seat integrated design, symmetrically arranged within the container and secured to the bulkhead using E-type shock-absorbing pads. Each five-seat control console integrates a monitor, keyboard, mouse, and computer. Below the seats is storage space for folding chairs; above the seats are shelves; the rear features equipment cabinets and storage cabinets; fire extinguishers are fixed to the entrance / exit doors; a whiteboard is installed opposite the main entrance / exit door for daily record-keeping; a water dispenser is located next to the whiteboard for daily drinking water; and a fixed emergency light is installed above the rear entrance / exit door.

4. The UAV emergency command unit system of claim 1, wherein, The split-type air conditioner uses a commercial inverter air conditioner. The outdoor unit is fixed to the front bulkhead, with a ring-shaped vibration damping pad in the middle to reduce vibration transmitted from the air conditioner to the container. A set of drain pipes is installed on each side of the air conditioner. The indoor units are arranged diagonally to regulate the temperature inside the container. Wall-mounted lights are installed side by side on the top to provide lighting for work inside the container. The exhaust fan inlet is located in the middle of the left side of the container, and the exhaust fan outlet is located at the top rear of the container.

5. The UAV emergency command unit system of claim 1, wherein, The main power supply adopts an external mains power supply method, with two 220V mains power lines at a frequency of 50Hz. The mains power is supplied to the distribution box through the enclosure adapter plate. After distribution by the distribution box, the power supply to each device is provided. The power distribution system is the basic platform for normal and stable operation. The power supply and distribution system consists of an external power supply enclosure adapter plate, distribution box, UPS, grounding system and supporting cables. The adapter plate has two external power input interfaces. The system power supply adopts a single-phase three-wire power supply. One line is the power supply line for critical equipment, mainly including computers, monitors, printers, large display screens, routers, switches, and ruggedized laptops. The other line is the power supply line for auxiliary equipment, including wall-mounted lights, exhaust fan assemblies, spare sockets, and air conditioners.

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