A multi-purpose vehicle-mounted launcher for rockets and scatter bombs

Abstract

The present invention discloses a vehicle-mounted launcher for multi-purpose rockets and scatter bombs, comprising a chassis, a base frame for fixed connection to the chassis, and a launcher mounted on the base frame. The launcher comprises a scatter launcher and a rocket launcher mounted on the upper side of the scatter launcher. The scatter launcher is tilted upward, and the lower side of the rocket launcher is hingedly connected to the scatter launcher via a plurality of hinges. A drive cylinder 35 is provided at the rear of the rocket launcher for driving the rocket launcher to flip around the hinges. The base frame and the scatter launcher are rotatably connected via a slewing bearing, and the slewing bearing is provided with at least one locking mechanism for locking the rocket launcher. By combining the scatter launcher with the rocket launcher, the present invention has multi-bomb compatibility and multiple uses. This application meets the three launch requirements of universalization, modularization, and serialization, and meets existing civilian and military needs.

Description

Technical Field

[0001] The present invention relates to the technical field of launch technology, in particular to the technical field of multi-purpose vehicle-mounted launchers for rockets and scatter bombs. Background Art

[0002] Ammunition launch technology, as a crucial component of launch systems, directly impacts a system's combat capability, development costs, replenishment methods, and other aspects, and is a prerequisite for determining equipment configuration. Current platform requirements for ammunition launch include three key characteristics: universalization, modularization, and serialization; precise launch control; rapid response; lightweight launch; and rapid response. These requirements complicate the launch environment and conditions. Existing launch systems are generally designed to fire only a single type of ammunition, lacking versatility and failing to meet diverse operational requirements. Furthermore, existing launch systems are difficult to operate and generally require multiple personnel. Summary of the Invention

[0003] The purpose of the present invention is to solve the problems in the prior art and propose a multi-purpose vehicle-mounted launcher for rockets and scatter bombs, which has multi-bomb compatibility and can be used for multiple purposes. Under the premise of limited operators, it can realize more types of equipment configurations and has universal, modular and serialized launch performance.

[0004] To achieve the above objectives, the present invention provides a multi-purpose vehicle-mounted launcher for rockets and scatter bombs, comprising a chassis, a base frame fixedly connected to the chassis, and a launcher mounted on the base frame. The launcher comprises a scatter launcher and a rocket launcher mounted above the scatter launcher. The scatter launcher is arranged upwardly and tilted. The lower side of the rocket launcher is hingedly connected to the scatter launcher via a plurality of hinges. A drive cylinder 35 is provided at the rear of the rocket launcher for driving the rocket launcher to flip around the hinges. The base frame and the scatter launcher are rotatably connected via a slewing bearing. The slewing bearing is provided with at least one locking mechanism for locking the slewing bearing.

[0005] It also includes a vehicle-mounted launch control device connected to the transmitter for control, and the vehicle-mounted launch control device is arranged at a non-driving position in the passenger compartment of the chassis vehicle.

[0006] Preferably, the rocket launcher includes a plurality of directional tubes arranged in the same direction and a tube fixing frame for fixing the directional tubes. One end of the hinge is fixedly connected to the tube fixing frame, and a locking member is provided on the directional tube.

[0007] Preferably, the locking part includes a locking pin and a locking seat body, the locking seat body is fixedly arranged at the tail end of the directional tube, the locking pin can be slidably arranged in the locking seat body, and the directional tube is provided with a through hole for the end of the locking pin to pass through, and the end of the locking pin away from the directional tube is provided with an eccentric control block for cooperating with the locking seat body, the locking pin is hingedly connected to the eccentric position of the eccentric control block, and the locking seat body is provided with a locking spring for driving the locking pin to slide toward the end of the directional tube.

[0008] Preferably, the tube fixing frame is further provided with a scope seat for fixing the scope.

[0009] Preferably, the scattering and launching frame includes a scattering box arranged obliquely, the scattering box is provided with a plurality of scattering and launching ports arranged obliquely upward, and the scattering box is fixedly connected to the slewing bearing via a bracket.

[0010] Preferably, the slewing bearing comprises a slewing support inner ring and a slewing support outer ring rotatably connected to the slewing support inner ring, the lower end of the slewing support inner ring is fixedly connected to the base frame, and the scattering launch frame is fixed to the slewing support outer ring.

[0011] Preferably, the locking mechanism includes a fine-tuning direction fixer provided on the base frame, the base frame includes a first rack fixed to the outer wall of the outer ring of the rotary support, a second tooth block arranged toward the first rack, and a base fixed on the base frame, the second tooth block is slidably provided in the base, and the base is provided with a control screw for driving the second tooth block to slide back and forth in a direction away from or close to the first rack, and the control screw is threadedly connected to the base.

[0012] Preferably, the locking mechanism includes an all-angle direction fixer, and the all-angle direction fixer includes a vertically arranged pin body and a pin seat, the pin body is inserted in the pin seat and is slidably connected to the pin seat, the pin seat is fixedly connected to the scattering launch frame, and the upper side of the inner ring of the rotary support is provided with a plurality of sockets adapted to the pin body, and the pin seat is provided with a control lever for controlling the reciprocating sliding of the pin body along the pin seat, one end of the control lever is hingedly connected to the top of the pin body, and the middle part is hingedly connected to the pin seat.

[0013] Preferably, the control lever is provided with a lever arm, and a return spring is provided between the lever arm and the pin seat for driving the control lever to flip around the hinged position with the pin seat to drive the pin body to slide downward. The lever arm is also provided with a locking buckle, the middle part of the locking buckle is hingedly connected to the lever arm, and a hook is provided at one end of the locking buckle, and a hook position for engaging with the hook is provided on the pin seat. When the hook is engaged with the hook position, the pin body is in a position separated from the socket.

[0014] Preferably, the chassis vehicle is a cargo truck, an off-road vehicle, or a Class II chassis vehicle, and the power input end of the vehicle-mounted launch control device is connected to the power output end of the chassis vehicle.

[0015] The beneficial effects of the multi-purpose vehicle-mounted launcher for rockets and scatter bombs of the present invention are as follows: the present invention combines a scattering launcher with a rocket launcher. The rocket launcher is used for launching hail-prevention and rain-enhancing rockets, forest fire-extinguishing bombs, and grassland fire-extinguishing bombs. The scattering launcher is used for launching scattering ammunition life-saving bombs, scattering fire-extinguishing bombs, scattering mine-laying bombs, and scattering training bombs. It has multi-bomb compatibility and one vehicle has multiple uses. Under the premise of limited operators, more types of equipment configurations can be achieved. The launcher can be fixed on various types of vehicles through the chassis to achieve motorized launch and rapid response launch. The rocket launcher is hingedly set on the upper side of the scattering launcher, and its adjustment angle is controlled by the drive cylinder to meet various launch requirements. The direction of the launcher can be adjusted by cooperating with the rotary bearing and the locking mechanism to meet various shooting requirements. The present application meets the three launch requirements of universalization, modularization, and serialization, and meets existing civilian and military needs.

[0016] The features and advantages of the present invention will be described in detail through embodiments with reference to the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 The present invention is a schematic diagram of the three-dimensional structure of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0018] Figure 2 The present invention is a schematic diagram of the main structure of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0019] Figure 3 The present invention is a schematic diagram of the main structure of a rocket launcher of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs when the rocket launcher is in a horizontal launching state.

[0020] Figure 4 The present invention is a schematic diagram of the three-dimensional structure of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0021] Figure 5The present invention is a schematic diagram of the three-dimensional structure of a rocket launcher of a vehicle-mounted launcher for rockets and scatter bombs.

[0022] Figure 6 The present invention is a schematic diagram of the three-dimensional structure of the chassis and slewing bearing of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0023] Figure 7 The present invention is a schematic diagram of the top view of the chassis structure of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0024] Figure 8 The present invention is a schematic diagram of the three-dimensional structure of a locking part of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0025] Figure 9 The present invention is a schematic diagram of the internal structure of a locking part of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0026] Figure 10 The present invention is a schematic diagram of the three-dimensional structure of an all-angle direction fixer of a multi-purpose vehicle-mounted launcher for rockets and scatter bombs.

[0027] in:

[0028] 1-vehicle-mounted launch control device; 2-chassis vehicle; 3-launcher; 4-chassis; 31-rocket launcher; 311-directional tube; 312-fixing frame; 314-sighting mirror base; 315-locking piece; 3151-locking latch; 3152-locking base; 3153-eccentric control block; 3154-locking spring; 32-dispensing launcher; 321-dispensing box; 322-bracket; 41-slewing bearing; 411- Rotary support inner ring; 412 - slewing support outer ring; 4111 - socket; 44 - fine-tuning direction fixer; 441 - first rack; 442 - second gear block; 443 - base; 444 - control screw; 45 - full-angle direction fixer; 451 - pin body; 452 - pin seat; 453 - lever; 454 - return spring; 455 - locking buckle; 4521 - hook position; 4531 - lever arm; 4551 - hook head Implementation Method

[0029] To make the objectives, technical solutions, and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and examples. However, it should be understood that the specific embodiments described herein are merely illustrative of the present invention and are not intended to limit the scope of the present invention. In addition, in the following description, descriptions of well-known structures and technologies are omitted to avoid unnecessary confusion of the present invention.

[0030] In the description of the present invention, it should be noted that when an element is referred to as being "fixed to" or "disposed on" another element, it may be directly on the other element or indirectly on the other element. When an element is referred to as being "connected to" another element, it may be directly connected to the other element or indirectly connected to the other element.

[0031] In the description of the present invention, it should be noted that the terms "center", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, or the orientations or positional relationships in which the inventive product is usually placed when in use. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", "third" and the like are only used to distinguish the description and cannot be understood as indicating or implying relative importance. Therefore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of such features. In the description of the present invention, "multiple" means two or more, unless otherwise clearly and specifically defined. "Several" means one or more, unless otherwise clearly and specifically defined.

[0032] In the description of the present invention, it should also be noted that, unless otherwise expressly specified or limited, the terms "disposed," "installed," "connected," and "connected" should be understood in a broad sense. For example, they may refer to fixed connections, detachable connections, or integral connections; they may refer to mechanical connections or electrical connections; they may refer to direct connections or indirect connections through an intermediate medium; and they may refer to internal communication between two components. Those skilled in the art will understand the specific meanings of the above terms in the present invention based on the specific circumstances. Example

[0033] See Figures 1-10 The present invention provides a multi-purpose vehicle-mounted launcher for rockets and scatter bombs, comprising a chassis 2, a base frame 4 for fixedly connecting to the chassis 2, and a launcher 3 provided on the base frame 4. The launcher 3 comprises a scattering launcher 32 and a rocket launcher 31 provided on the upper side of the scattering launcher 32. The scattering launcher 32 is arranged to face upward at an angle. The lower side of the rocket launcher 31 is hingedly connected to the scattering launcher 32 through two hinges 34. A driving cylinder 35 is provided at the rear of the rocket launcher 31 for driving it to flip around the hinge 34. The base frame 4 and the scattering launcher 32 are rotatably connected through a slewing bearing 41. The slewing bearing 41 is provided with two locking mechanisms for locking it.

[0034] The vehicle-mounted launch control device 1 is further included and is connected to the launcher 3 . The vehicle-mounted launch control device 1 is located at the co-pilot position of the chassis vehicle 2 . In this embodiment, the scattering launcher 32 is combined with the rocket launcher 31. The rocket launcher 31 is used for launching hail-proof and rain-enhancing rockets, forest fire-extinguishing bombs, and grassland fire-extinguishing bombs. The scattering launcher 32 is used to launch scattering ammunition life-saving bombs, scattering fire-extinguishing bombs, scattering mine-laying bombs, and scattering training bombs. It has multi-bomb compatibility and one vehicle has multiple uses. Under the premise of limited operators, more types of equipment configurations can be achieved. The launcher in this embodiment can be fixed on various vehicles through the chassis 4 to achieve motorized launch and rapid response launch. Furthermore, in this embodiment, considering that there is generally no need to adjust the launch angle when launching scattering ammunition, the angle of the scattering launcher 32 is set to be fixed, and when launching rocket-type ammunition, the launch angle of the rocket-type ammunition needs to be adjusted in response to various launch requirements. Therefore, the rocket launcher 31 is hingedly set on the upper side of the scattering launcher 32, and its adjustment angle is controlled by the drive cylinder 35 to meet various launch requirements. The slewing bearing 41 cooperates with the locking mechanism to adjust the orientation of the launcher 3 to meet various shooting requirements.

[0035] See Figure 4 、 Figure 5 The rocket launcher 31 comprises ten directional tubes 311 arranged in the same direction, a tube mounting bracket 312 for securing the tubes 311, and one end of the hinged member 34 fixedly connected to the tube mounting bracket 312. Locking members 315 are provided on the directional tubes 311. There are ten directional tubes in total, arranged in two rows and five columns. Arrangements can be designed based on the vehicle's load capacity and actual requirements, including but not limited to three rows and five columns or four rows and five columns. The directional tubes 311 are used to launch rockets, and the locking members 315 secure the rockets within the directional tubes 311, ensuring safe and secure retention before launch and during movement with the rockets, and reliable separation during launch.

[0036] See Figure 4 、 Figure 8 and Figure 9The locking member 315 includes a locking pin 3151 and a locking seat 3152. The locking seat 3152 is fixed to the rear end of the directional tube 311. The locking pin 3151 is slidably mounted within the locking seat 3152. The directional tube 311 is provided with a through hole for the end of the locking pin 3151 to pass through. An eccentric control block 3153 is provided on the end of the locking pin 3151, distal from the directional tube 311, for engaging with the locking seat 3152. The locking pin 3151 is hingedly connected to the eccentric control block 3153 at an eccentric position. A locking spring 3154 is housed within the locking seat 3152 for driving the locking pin 3151 toward the end of the directional tube 311. When the locking pin 3151 is inserted into the directional tube 311, it engages with the rocket within the directional tube 311, securing it.

[0037] See Figure 4 , a sighting mirror seat 314 for fixing the sighting mirror is also provided on the tube fixing frame 312. The sighting mirror seat 314 is used to install the sighting mirror, and the sighting mirror can be selected as a standard mechanical telescope or an electronic sighting device.

[0038] See Figure 2 、 Figure 4 The scatter launcher 32 includes an inclined scatter box 321 with 24 upwardly inclined scatter launch ports 311. The scatter box 321 is fixedly connected to the slewing bearing 41 via a bracket 322. The bracket 322 is used to fix the tilt angle of the scatter box 321. The scatter launch ports 311 can be designed based on the load capacity of the chassis and actual requirements, including but not limited to arrangements such as 6 rows and 6 columns or 8 rows and 6 columns. The scatter launch ports 311 are used to load scatter bombs.

[0039] Preferably, the scatter box 321 is tilted at 45°. Example

[0040] See Figure 6 、 Figure 7 The slewing bearing 41 includes an inner slewing ring 411 and an outer slewing ring 412 rotatably connected to the inner slewing ring 411. The lower end of the inner slewing ring 411 is fixedly connected to the chassis 4, and the scatter launcher 32 is fixed to the outer slewing ring 412. The slewing bearing 41 serves as the base of the scatter launcher 32, connecting it to the chassis 4. Secondly, it is rotatable, facilitating ammunition loading and orientation adjustment.

[0041] See Figure 4 、 Figure 6The locking mechanism includes a fine-tuning direction fixer 44 provided on the base frame 4, and the base frame 4 includes a first rack 441 fixed to the outer wall of the rotary support outer ring 412, a second tooth block 442 arranged toward the first rack 441, and a base 443 fixed on the base frame 4, the second tooth block 442 is slidably provided in the base 443, and the base 443 is provided with a control screw 444 for driving the second tooth block 442 to slide back and forth in a direction away from or close to the first rack 441, and the control screw 444 is threadedly connected to the base 443. The fine-tuning direction holder 44 is used for fine-tuning the direction of the transmitter 3. When it is used, the second tooth block 442 is controlled to move away from the first rack 441 by rotating the control screw 444, so that it is separated from the second tooth block 442, and the slewing support outer ring 412 can rotate relative to the slewing support inner ring 411 to fine-tune the direction of the transmitter 3. After the adjustment is completed, the second tooth block 442 is controlled to move toward the first rack 441 by rotating the control screw 444, so that it is engaged with the second tooth block 442, thereby locking the slewing support outer ring 412 and the slewing support inner ring 411, making adjustment more convenient, and the direction is fixed more firmly and not easy to loosen.

[0042] See Figure 4 、 Figure 6 and Figure 10 The locking mechanism also includes a full-angle direction fixer 45, which includes a vertically arranged pin body 451 and a pin seat 452, the pin body 451 is inserted into the pin seat 452 and is slidably connected to the pin seat 452, the pin seat 452 is fixedly connected to the scattering launcher 32, and a plurality of sockets 4111 adapted to the pin body 451 are provided on the upper side of the slewing support inner ring 411, and a control lever 453 for controlling the reciprocating sliding of the pin body 451 along the pin seat 452 is provided on the pin seat 452, one end of the control lever 453 is hingedly connected to the top of the pin body 451, and the middle part is hingedly connected to the pin seat 452. The full-angle direction fixer 45 meets the circumferential adjustment requirements of the slewing bearing 41. When adjustment is required, the pin body 451 is controlled to rise by controlling the lever 453 to separate it from the socket 4111, thereby releasing the lock. The slewing support inner ring 411 and the slewing support outer ring 412 can rotate relative to each other, thereby adjusting the direction of the launcher 3, which makes it easier to load the launcher 3 and also allows real-time adjustment of the launch direction.

[0043] See Figure 10A lever arm 4531 is provided on the control lever 453, and a return spring 454 is provided between the lever arm 4531 and the pin seat 452 for driving the control lever 453 to flip around the hinged position with the pin seat 452 to drive the pin body 451 to slide downward. A locking buckle 455 is also provided on the lever arm 4531, and the middle part of the locking buckle 455 is hingedly connected to the lever arm 4531. A hook head 4551 is provided at one end of the locking buckle 455, and a hook position 4521 that is engaged with the hook head 4551 is provided on the pin seat 452. When the hook head 4551 is engaged with the hook position 4521, the pin body 451 is in a position separated from the socket 4111. The return spring 454 is used to make the pin body 451 slide downward automatically, so that it remains in cooperation with the socket 4111, to prevent the pin body 451 from being separated from the socket 4111 due to vibration during driving. When the hook head 4551 and the hook position 4521 cooperate, the pin body 451 can be kept on the upper side of the pin seat 452, so that the pin body 451 remains separated from the socket 4111, which is convenient for adjusting the direction of the transmitter 3.

[0044] Preferably, in this embodiment, the slewing bearing 41 has both a fine-tuning direction fixer 44 and a full-angle direction fixer 45. When adjusting the direction, both direction fixers need to be unlocked.

[0045] Preferably, the chassis 2 is a cargo truck, an off-road vehicle, or a Class II chassis, and the power input of the vehicle-mounted launch control device 1 is connected to the power output of the chassis 2. Furthermore, the number of launch racks can be increased depending on the load capacity and rear compartment size of the chassis 2.

[0046] Preferably, the underframe 4 is a well-shaped beam structure welded from profiles and steel plates. As shown in the figure, it is mainly composed of basic components such as a long and short crossbeam that are symmetrical to each other, and a slewing bearing 41 that are orthogonally welded into an integral frame. It serves as the connection between the chassis 2 and the scatter launcher 32. A pad is installed between the long crossbeam of the underframe and the upper surface of the vehicle beam. The long crossbeam of the underframe is fixed to the chassis beam by bolts, ensuring a reliable connection between the underframe and the vehicle beam.

[0047] Preferably, in this embodiment, the driving cylinder 35 can adopt a standard manual or electric telescopic cylinder to control the launching angle of the launcher 3.

[0048] Preferably, it further comprises a remote control launch control device 5 wirelessly connected to the launcher 3. The remote control launch device 5 can be installed to enable personnel to control the launch of the launch vehicle within a range of 50 meters from the launch rack.

[0049] Working process of the present invention:

[0050] During operation, a multi-purpose vehicle-mounted launcher for rockets and scatter bombs of the present invention selects a chassis 2 of a suitable model and is fixed on the chassis 2 through the chassis 4. The scattering launcher 32 is filled with scattering ammunition life-saving bombs, scattering fire-extinguishing bombs, scattering mine-laying bombs, and scattering training bombs. The rocket launcher 31 is filled with hail-proof and rain-enhancing rockets, forest fire-extinguishing bombs, and grassland fire-extinguishing bombs. The vehicle-mounted launch control device 1 is arranged at a non-driving position in the passenger compartment of the chassis 2. The launch is controlled by the vehicle-mounted launch control device 1. The rocket launcher 31 is hingedly arranged on the upper side of the scattering launcher 32, and its adjustment angle is controlled by the drive cylinder 35 to meet various shooting requirements. When the direction of the launcher 3 needs to be adjusted, the locking mechanism is unlocked, and then the direction of the launcher 3 is adjusted by the slewing bearing 41. After the adjustment is completed, the slewing bearing 41 is locked again by the locking mechanism.

[0051] The rocket launcher 31 is used for launching hail-proof and rain-enhancing rockets, forest fire-extinguishing bombs, and grassland fire-extinguishing bombs. The scattering launcher 32 is used for launching scattering ammunition such as life-saving bombs, fire-extinguishing bombs, mine-laying bombs, and training bombs. It has multi-bomb compatibility and one vehicle can be used for multiple purposes. Under the premise of limited operators, more types of equipment configurations can be achieved. The launcher of this embodiment can be fixed on various vehicles through the chassis 4 to achieve motorized launch and rapid response launch. Furthermore, this embodiment takes into account that there is generally no need to adjust the launch angle when launching scattering ammunition, so the angle of the scattering launcher 32 is set to be fixed, and when launching rocket-type ammunition, the launch angle of the rocket-type ammunition needs to be adjusted in response to various launch requirements. Therefore, the rocket launcher 31 is hingedly set on the upper side of the scattering launcher 32, and its adjustment angle is controlled by the drive cylinder 35 to meet various launch requirements. The direction of the launcher 3 can be adjusted by cooperating with the slewing bearing 41 and the locking mechanism to meet various shooting requirements.

[0052] The standard parts used in this application document can all be purchased from the market, and the specific connection methods of each part adopt conventional means such as mature bolts, rivets, welding, etc. in the existing technology. The electric slide rail slide, cylinder, welding machine, electric telescopic rod and internal components of the controller all adopt conventional models in the existing technology, and their internal structure belongs to the existing technology structure. Workers can complete normal operation of them according to the existing technical manual. In addition, the circuit connection adopts the conventional connection method in the existing technology, and no detailed description is given here.

[0053] It should be noted that although the above embodiments have been described herein, this does not limit the scope of patent protection of the present invention. Therefore, based on the innovative concept of the present invention, changes and modifications to the embodiments described herein, or equivalent structural or equivalent process transformations made using the contents of the present invention's description and drawings, and direct or indirect application of the above technical solutions to other related technical fields, are all included in the scope of protection of the present invention's patent.

Claims

1. A multi-purpose vehicle-mounted launcher for rockets and scatter bombs, comprising a chassis vehicle (2), a base frame (4) for fixedly connecting to the chassis vehicle (2), and a launcher (3) arranged on the base frame (4), characterized in that: The launcher (3) includes a scattering launcher (32) and a rocket launcher (31) arranged on the upper side of the scattering launcher (32), the scattering launcher (32) is arranged to be tilted upward, the lower side of the rocket launcher (31) is hingedly connected to the scattering launcher (32) through a plurality of hinges (34), the tail of the rocket launcher (31) is provided with a driving cylinder (35) for driving it to flip around the hinge (34), the base frame (4) and the scattering launcher (32) are rotatably connected through a slewing bearing (41), and the slewing bearing (41) is provided with at least one locking mechanism for locking it; the slewing bearing (41) ) includes a slewing support inner ring (411) and a slewing support outer ring (412) rotatably connected to the slewing support inner ring (411), the lower end of the slewing support inner ring (411) is fixedly connected to the chassis (4), and the scattering launcher (32) is fixed to the slewing support outer ring (412); and also includes a vehicle-mounted launch control device (1) connected to the launcher (3) for control, the vehicle-mounted launch control device (1) is provided at a non-driving position in the passenger compartment of the chassis vehicle (2), the locking mechanism includes a fine-tuning direction fixer (44) provided on the chassis (4), the fine-tuning direction fixer (44) includes a fixed device provided on the slewing support A first rack (441) on the outer wall of the outer ring (412), a second tooth block (442) arranged toward the first rack (441), and a base (443) fixed on the base frame (4), wherein the second tooth block (442) is slidably arranged in the base (443), and a control screw (444) is provided on the base (443) for driving the second tooth block (442) to slide back and forth in a direction away from or close to the first rack (441), wherein the control screw (444) is threadedly connected to the base (443), and the locking mechanism includes a full-angle direction fixer (45), and the full-angle direction fixer (45) includes a vertical A pin body (451) and a pin seat (452) are provided, wherein the pin body (451) is inserted into the pin seat (452) and is slidably connected to the pin seat (452), the pin seat (452) is fixedly connected to the scattering launch frame (32), a plurality of jacks (4111) adapted to the pin body (451) are provided on the upper side of the slewing support inner ring (411), and a control lever (453) for controlling the pin body (451) to slide back and forth along the pin seat (452) is provided on the pin seat (452), one end of the control lever (453) is hingedly connected to the top of the pin body (451), and the middle part is hingedly connected to the pin seat (452).

2. A vehicle-mounted launcher for rockets and scatter bombs as claimed in claim 1, characterized in that: The rocket launcher (31) includes a plurality of directional tubes (311) arranged in the same direction, a tube fixing frame (312) for fixing the directional tubes (311), one end of the hinge (34) is fixedly connected to the tube fixing frame (312), a locking member (315) is provided on the directional tube (311), and the locking member (315) includes a locking pin (3151) and a locking seat (3152), the locking seat (3152) is fixedly arranged at the tail of the directional tube (311), and the locking pin (3151) is slidably arranged on the locking seat (3152). 152), and a through hole is provided on the directional tube (311) for the end of the locking pin (3151) to pass through, an eccentric control block (3153) for cooperating with the locking seat (3152) is provided on the end of the locking pin (3151) away from the directional tube (311), the locking pin (3151) and the eccentric control block (3153) are hingedly connected at an eccentric position, and a locking spring (3154) is provided in the locking seat (3152) for driving the locking pin (3151) to slide toward the end of the directional tube (311).

3. A vehicle-mounted launcher for rockets and scatter bombs as claimed in claim 2, characterized in that: The tube fixing frame (312) is also provided with a sighting mirror seat (314) for fixing the sighting mirror.

4. The multi-purpose vehicle-mounted launcher for rockets and scatter bombs according to claim 1, characterized in that: The scattering launch frame (32) comprises a scattering box (321) arranged obliquely, the scattering box (321) being provided with a plurality of scattering launch ports (3211) arranged obliquely upward, and the scattering box (321) being fixedly connected to the slewing bearing (41) via a bracket (322).

5. The multi-purpose vehicle-mounted launcher for rockets and scatter bombs according to claim 1, characterized in that: The control lever (453) is provided with a lever arm (4531), and a return spring (454) is provided between the lever arm (4531) and the pin seat (452) for driving the control lever (453) to flip around the hinged position with the pin seat (452) to drive the pin body (451) to slide downward. The lever arm (4531) is also provided with a locking buckle (455), and the middle part of the locking buckle (455) is hingedly connected to the lever arm (4531). One end of the locking buckle (455) is provided with a hook (4551). The pin seat (452) is provided with a locking buckle (455) for locking the control lever (453) around the hinged position with the pin seat (452). The hook head (4551) is engaged with the hook position (4521), and when the hook head (4551) is engaged with the hook position (4521), the pin body (451) is in a position separated from the insertion hole (4111).

6. The multi-purpose vehicle-mounted launcher for rockets and scatter bombs according to claim 1, characterized in that: The chassis vehicle (2) is a cargo truck, an off-road vehicle, or a second-class chassis vehicle, and the power input end of the vehicle-mounted emission control device (1) is connected to the power output end of the chassis vehicle (2).

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