Side twin-boom spreader launcher

Abstract

The utility model relates to the field of special vehicle launcher structure design, concretely is side double -arm unfolding formula launching vehicle. Side double -arm unfolding formula launching vehicle above -mentioned includes carrying vehicle, radar, side arm and missile launcher, side arm has two, sets up in carrying vehicle left and right sides and presents mirror image arrangement respectively, side arm includes arm body, connecting hinge, carrying vehicle and support hydraulic cylinder, side arm is hinged with carrying vehicle through connecting hinge, the one end fixed mounting of arm body is away from connecting hinge has support hydraulic cylinder, support hydraulic cylinder piston rod is downward, the utility model discloses through setting up side arm to carry missile launcher, makes missile launcher when the battle state can through the unfolding of side arm to be staggered with radar, combines radar and missile launcher on a car, realizes the integration of reconnaissance and attack, effectively avoids the problem that the tail flame of missile launch can cause damage to radar and radar blocks the launch of missile.

Description

Technical Field

[0001] This utility model relates to the field of special vehicle launcher structure design, specifically a side-mounted double-arm deployable launch vehicle. Background Technology

[0002] In the modern battlefield environment, the ability to conduct long-range saturation strikes has become one of the key factors determining the outcome of the battle. Missile weapon systems, with their long range, powerful firepower, and high destructive force, have become the core equipment for carrying out fire strikes and long-range deterrence. As the core vehicle of the system, the comprehensive performance of the missile launcher directly determines the mobility, stealth, survivability, and rapid response capability of the weapon system.

[0003] Due to the limitations of the vehicle's structure, only one or two launchers can usually be installed, and there is basically no place to install the guidance radar. This is because if the guidance radar is installed on the front of the launcher, it will block the missile launch; and if the guidance radar is installed on the rear of the launcher, the exhaust plume of the missile launch may damage the radar.

[0004] Therefore, in the existing technology, a vehicle is usually equipped with a guidance radar and used in conjunction with other missile launchers to form a battle group. However, forming a battle group requires at least two vehicles, one radar vehicle and one missile launcher. In this case, the target is too large and is easily detected by the enemy. It is also difficult to form a large firepower and the mobility is poor. Utility Model Content

[0005] To solve the above-mentioned technical problems, the technical solution adopted by this utility model is: a side-mounted double-arm deployable launch vehicle, including a transport vehicle, a radar, side arms and a missile launcher. There are two side arms, which are respectively set on the left and right sides of the transport vehicle and arranged in a mirror image.

[0006] The side arm includes an arm body, a connecting hinge, a transport vehicle, and a supporting hydraulic cylinder. The side arm is hinged to the transport vehicle via the connecting hinge. A supporting hydraulic cylinder is fixedly installed at the end of the arm body away from the connecting hinge, with the piston rod of the supporting hydraulic cylinder facing downward.

[0007] As a preferred embodiment of this utility model, the connecting hinge is a heavy-duty hinge.

[0008] As a preferred embodiment of this utility model, the radar is fixedly installed on the front middle of the side of the transport vehicle.

[0009] As a preferred embodiment of this utility model, the missile launcher is installed on the upper side of the arm body, and two sets of missile launchers are installed on each arm body.

[0010] As a preferred technical solution of this utility model, the transport vehicle is equipped with two ejection hydraulic cylinders. The side of the arm close to the vehicle body is hinged to the ejection hydraulic cylinder. When in combat mode, the side arm is pushed out by this hydraulic cylinder.

[0011] The beneficial effects of this utility model are as follows: First, by setting a side arm to support the missile launcher, the missile launcher can be separated from the radar by unfolding the side arm in combat mode, combining the radar and the missile launcher on one vehicle, realizing integrated reconnaissance and strike capabilities, and effectively avoiding the problem that the exhaust plume of the missile may damage the radar and the radar may block the missile launch.

[0012] Second, this utility model, through its expandable and compact design, allows for the installation of as many missile launchers as possible without mutual interference. When the side arms are retracted, the missile launchers do not interfere with each other. In combat, when the side arms are extended, each missile launcher can launch normally without interfering with each other. This design allows this utility model to become a single target when retracted, making it difficult for the enemy to detect, while in combat it can increase the firepower output by two to four times compared to traditional rocket launchers. Attached Figure Description

[0013] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0014] Figure 1 This is a front view of the present invention when it is in motion.

[0015] Figure 2 This is a right view of the present invention in combat.

[0016] Figure 3 This is a right view of the present invention when it is in motion.

[0017] In the diagram: 1. Transport vehicle; 2. Radar; 3. Side arm; 31. Arm body; 32. Connecting hinge; 33. Supporting hydraulic cylinder; 4. Missile launcher. Detailed Implementation

[0018] The embodiments of this utility model are described in detail below.

[0019] See Figures 1-3 The side-mounted double-arm launch vehicle includes a carrier vehicle 1, a radar 2, side arms 3, and a missile launcher 4. There are two side arms 3, which are respectively set on the left and right sides of the carrier vehicle 1 and arranged in a mirror image. Each side arm 3 includes an arm body 31, a connecting hinge 32, a carrier vehicle 1, and a supporting hydraulic cylinder 33. The side arm 3 is hinged to the carrier vehicle 1 through the connecting hinge 32. The supporting hydraulic cylinder 33 is fixedly installed at the end of the arm body 31 away from the connecting hinge 32, with the piston rod of the supporting hydraulic cylinder 33 facing downward. The radar 2 is fixedly installed on the upper side of the carrier vehicle 1, in the middle of the front position.

[0020] This utility model uses a side arm 3 to support the missile launcher 4, so that the missile launcher 4 can be separated from the radar 2 by unfolding the side arm 3 in combat mode. This integrates the radar 2 and the missile launcher 4 on a single vehicle, achieving integrated reconnaissance and strike capabilities while effectively avoiding the problem that the missile's exhaust plume may damage the radar 2 or that the radar 2 may obstruct the missile's launch.

[0021] See Figures 1-3 The connecting hinge 32 is a heavy-duty hinge; the missile launcher 4 is installed on the upper side of the arm 31, and two sets of missile launchers 4 are installed on each arm 31; the transport vehicle 1 is equipped with two ejection hydraulic cylinders, and the side of the arm 31 near the vehicle body is hinged to the ejection hydraulic cylinder. When in combat, the side arm 3 is pushed out by this hydraulic cylinder.

[0022] This invention features a compact, deployable design that allows for the installation of as many missile launchers 4 as possible without mutual interference. When the side arms 3 are retracted, the missile launchers 4 do not interfere with each other. In combat, when the side arms 3 are extended, each missile launcher 4 can be launched normally without mutual interference. This design allows the invention to become a single target when retracted, making it difficult for the enemy to detect, while in combat it can increase firepower output by two to four times compared to traditional rocket launchers.

[0023] Specifically, when movement is required, the side arm 3 and the supporting hydraulic cylinder 33 retract and lock, allowing the transport vehicle 1 to be started to complete the transfer. A diagram illustrating the movement state of this utility model can be found here. Figure 1 , Figure 3 When combat is required, after the transport vehicle 1 stops, the operators control the ejection hydraulic cylinder to eject the side arm 3. The ejection distance is determined according to the target position. After ejection to the target position, the operators control the support hydraulic cylinder 33 to extend. The piston rod of the support hydraulic cylinder 33 pushes against the ground to assist the ejection hydraulic cylinder in resisting the huge impact force during missile launch. Furthermore, multiple missile launchers 4 enable this utility model to increase firepower output by two to four times compared to traditional rocket launchers. A combat status diagram of this utility model can be found in the attached diagram. Figure 2 .

[0024] Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and should not be construed as limiting the present invention. Those skilled in the art can make changes, modifications, substitutions and variations to the above embodiments within the scope of the present invention, which are still covered by the protection scope of the present invention.

Claims

1. A side-mounted, double-arm deployable launch vehicle, characterized in that: It includes a transport vehicle (1), a radar (2), a side arm (3) and a missile launcher (4). There are two side arms (3), which are respectively set on the left and right sides of the transport vehicle (1) and arranged in a mirror image. The side arm (3) includes an arm body (31), a connecting hinge (32), a carrier vehicle (1) and a supporting hydraulic cylinder (33). The side arm (3) is hinged to the carrier vehicle (1) through the connecting hinge (32). The supporting hydraulic cylinder (33) is fixedly installed at the end of the arm body (31) away from the connecting hinge (32), and the piston rod of the supporting hydraulic cylinder (33) faces downward.

2. The side-mounted dual-arm deployable launch vehicle according to claim 1, characterized in that, The connecting hinge (32) is a heavy-duty hinge.

3. The side-mounted dual-arm deployable launch vehicle according to claim 1, characterized in that, The radar (2) is fixedly installed on the upper side of the transport vehicle (1) at the front center.

4. The side-mounted dual-arm deployable launch vehicle according to claim 1, characterized in that, The missile launchers (4) are mounted on the upper side of the arm body (31), and two sets of missile launchers (4) are mounted on each arm body (31).

5. The side-mounted dual-arm deployable launch vehicle according to claim 1, characterized in that, The transport vehicle (1) is equipped with two ejection hydraulic cylinders. The side arm (31) close to the vehicle body is hinged to the ejection hydraulic cylinder. When in combat, the side arm (3) is pushed out by this hydraulic cylinder.

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