RU205040U1 - Multi-rotor salvo launch vehicle - Google Patents

Abstract

The utility model relates to transport ground vehicles for placing, transporting aircraft, in particular multicopters, as well as for launching them. The ground transport vehicle for the simultaneous launch of multicopters is made on the basis of a chassis with a cockpit and a body fixed to it for placement in the latter of multicopters on brackets and containing an operator's workplace, a control panel. The body is divided along a rigid partition to which the brackets are attached. The brackets are equipped with a mechanism for moving multicopters out of the body through openings that are made in the side rigid walls of the body and are equipped with doors. The doors open through a hinge connection from top to bottom to a horizontal position. The body is made with the possibility of placing multicopters inside N floors and M rows on the right and left along the partition. At the same time, the maximum number of multicopters launched is 2P. The useful model makes it possible to increase the efficiency of using multicopters when performing the assigned task (goal). 3 C.p. f-ly, 3 dwg

Description

The utility model relates to transport ground vehicles for placing, transporting aircraft, in particular multicopters, as well as for launching them. The utility model can be used in aerial photography, geological exploration, agriculture and forestry, and in military affairs.

Known small-sized mobile aviation system (US Pat. RF No. 2015067, publ. 30.06.1994). The system contains unmanned aerial vehicles (UAVs) with an autonomous electric drive, a mobile container and a remote control system in which the unmanned aerial vehicles are made in the form of vertically taking off platforms with rigid propfans equipped with an automatic landing system. The mobile container is based on an automobile chassis, contains a group of said aircraft and is equipped with devices for providing them with energy for flight and for the take-off and landing operating cycle. In the well-known UAV system, take-off platforms for vertical take-off and landing are launched one at a time through the sliding roof hatch, which lengthens the launch time of the UAV from the transported group.

Known ground control station based on the chassis of a special vehicle (Pat RF No. 2486078, publ. 27.06.2013), containing a van body mounted on a platform chassis, a chassis, a control system and a power supply system, a transceiver antenna. The body-van is divided by partitions inside into three compartments: operator, cargo and technological. In the cargo compartment, there are guides for placing packages with UAVs. A pneumatic system is installed in the technological compartment to power the UAV launcher. After arriving at the destination, the launcher is unloaded and installed, as well as the UAV packages are unloaded, then the UAV is installed on the launcher and the UAV is filled with fuel. An operator in the control room controls the UAV flight.

Known universal target training complex (US Pat. RF No. 2612336, publ. 03/07/2017), containing a vehicle with reusable UAVs of different types placed in it, a unified launch facility, a control point, which is configured to launch and simultaneously control several UAVs of different types. The complex can be equipped with at least 6 UAVs of different types.

Known ground vehicle equipped with a module for storage and automatic launch of the UAV (US Pat. RF No. 180861, publ. 28.06.2018), containing a module for storage and automatic launch of the UAV. The tool is made on the basis of the chassis of a special vehicle and contains a box-shaped body with a rigid frame, an engine, a transmission, a chassis, a control system and a power supply system. The UAV module is equipped with protective doors with a device for opening and closing them. The tool contains a platform for fixing the UAV, as well as a mechanism for lifting and rotating the platform with a rotary drive.

The closest technical solution to the claimed utility model is a command and staff vehicle (Pat. RF No. 195819, publ. 02/06/2020), containing a chassis with a body and a cab fixed on it, a bracket for installing a multicopter is placed inside the body, and the body is made with the ability placement of multicopters, operator's workplace, control panel and display, moreover, the front wall of the body is equipped with a swing door, on the roof of the cabin there is a platform for placing, launching and landing the multicopter, equipped with a landing sensor.

The disadvantage of the prototype is the reduced operational ability to launch multicopters placed in the body due to the use of a single launch and landing pad.

The technical result to be achieved by the claimed utility model consists in increasing the efficiency of using transported multicopters due to the simultaneous launch of several multicopters.

To achieve the specified technical result, the vehicle is a ground vehicle for simultaneous launching of multicopters, made on the basis of a chassis with a cabin and a body fixed on it for placement in the latter on brackets and containing an operator's workplace, a control panel, the body is divided along a rigid partition to which the brackets are attached, equipped with a mechanism for extending multicopters from the body through openings made in the side rigid walls of the body and equipped with doors that open from top to bottom to a horizontal position, the body is designed to accommodate multicopters inside N floors and M rows to the right and left along the bulkhead, while the maximum number is simultaneously launched multicopters is 2P, where P is the number of multicopters in a row.

The proposed land vehicle for simultaneous launch of multicopters is illustrated by the drawings shown in FIG. 1-3.

FIG. 1 shows a general view; in fig. 2 - rear view in working position; in fig. 3 is a top view in working position.

The ground transport vehicle for the simultaneous launch of multicopters is made on the basis of chassis 1 with a cabin 2 and a body 3 fixed to chassis 1 (Figs. 1, 2, 3). The body 3 is divided along a rigid partition 4. Brackets 5 are attached to the partition 4, on which the multicopters are located 6. The brackets 5 are equipped with a mechanism 7 for extending the multicopters 6 from the body 3. The extension mechanism 7 can be made in telescopic, rail ways. In the side rigid walls 8 of the body 3, openings 9 are made, through which the multicopters 6 are extended from the body 3. The openings 9 are equipped with doors 10, which automatically open through a hinge connection from top to bottom to a horizontal position. The body 3 is made with the possibility of placing multicopters 6 inside on brackets 5 N floors, the number of floors N (in Fig. 1, 2, 3 N = 3) and M rows in the number (in Fig. 1, 2, 3 M = 6 - total number of rows), in each row the number of multicopters 6 is P (in this useful model it is equal to P = 5). The number of N floors, the number of M rows, the number of P multicopters in a row depends on the weight and dimensions of the multicopters used 6. The operator's workplace with a remote control panel is located in the cabin 2 of the ground vehicle.

When the estimated number of multicopters 6 is brought to the starting position, at the command of the operator, the doors 10 are automatically opened from top to bottom to a horizontal position, and multicopters 6 are removed from the body 3 through the openings 9 using the extension mechanism 7. the number of launched multicopters 6 is 10. Moreover, the launch of multicopters 6 can be carried out either by a full floor of 2P multicopters, or combined from multicopters from any of the floors, provided that only one multicopter 6 is located vertically to the right and left of the partition 4, or single-group , in storeyed or combined. After starting, the mechanisms 7 for extending the multicopters 6 and the doors 10 return to their original position, freeing up space for use below or above the located floor according to a similar algorithm. When launching and in flight, multicopters 6 receive information from a remote control panel from an operator who is in cockpit 2 or, if necessary, who has left the cockpit, in a place convenient for control. Thus, the useful model makes it possible to increase the efficiency of the use of multicopters 6 when performing the assigned task (goal).

Claims (4)

1. Transport ground vehicle for simultaneous launch of multicopters, made on the basis of a chassis with a cockpit and a body fixed to it for placement in the latter multicopters on brackets and containing an operator's workplace, a control panel, characterized in that the body is divided along a rigid partition to which the brackets are attached equipped with a mechanism for extending multicopters from the body through openings made in the side rigid walls of the body and equipped with doors that open from top to bottom to a horizontal position, the body is designed to accommodate multicopters inside N floors and M rows to the right and left along the bulkhead, while the maximum number simultaneously launched multicopters is 2P, where P is the number of multicopters in a row. 2. The vehicle according to claim 1, characterized in that the operator's workplace with a remote control panel is located in the cab. 3. A vehicle according to claim 1, characterized in that the number of N floors, M rows, the number of P multicopters in a row depends on the weight and dimensions of the multicopter used. 4. The vehicle according to claim 1, characterized in that the mechanism for extending the multicopter from the body can be made in a telescopic, rail way.

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