CN110887405A - Rocket projectile vehicle-mounted and ground integrated launching vehicle - Google Patents
Rocket projectile vehicle-mounted and ground integrated launching vehicle Download PDFInfo
- Publication number
- CN110887405A CN110887405A CN201911183155.2A CN201911183155A CN110887405A CN 110887405 A CN110887405 A CN 110887405A CN 201911183155 A CN201911183155 A CN 201911183155A CN 110887405 A CN110887405 A CN 110887405A
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- China
- Prior art keywords
- vehicle
- launching
- rocket projectile
- base
- ground integrated
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention discloses a rocket projectile vehicle-mounted and ground integrated launching vehicle, and belongs to the technical field of rocket launching equipment. The fire control system comprises a chassis system, a transmitting device, a fire control system and a communication system; the launching device is movably arranged on the chassis system and comprises a base, a supporting frame, an azimuth mechanism, an undercarriage and a manual support; the supporting frame is rotatably connected with the base through an azimuth mechanism, the angle-adjustable movable mounting of the undercarriage is arranged on two sides of the supporting frame, and the manual support is arranged at the bottom of the base; the fire control system is used for controlling the launching of the rocket projectile, and the communication system is used for receiving and transmitting communication signals. The invention has the functions of quick assembly and disassembly, and has the passing capability and maneuvering capability in environments such as plains, mountainous regions, plateaus, towns, jungles and the like; possesses the vehicle-mounted or ground emission function.
Description
Technical Field
The invention belongs to the technical field of ground launching equipment, and particularly relates to a rocket projectile vehicle-mounted and ground integrated launching vehicle.
Background
Rocket weapon systems generally consist of a launching system (launch vehicle), a rocket projectile and a control system 3, and the main function of the rocket weapon system is to quickly and effectively shoot enemy cluster targets, area targets or special targets within a specified combat distance. The rocket launching system (launching vehicle) is used as an important component of a rocket weapon system and mainly has the following functions: during the transportation and marching process, the rocket bomb is born and protected; in the aiming process, the shooting direction of the rocket projectile is quickly and accurately positioned; in the launching process, the rocket projectile is reliably ignited and certain initial speed and disturbance as small as possible are provided for the rocket projectile, so that the shooting intensity is ensured. The tactical performance of rocket weapon systems is often measured in terms of range, maneuverability, and strength and concentration.
The modern war is characterized by large destruction, strong abruptness, large battlefield coverage, complex battle situation and abrupt and multi-end change, so that the military is required to have high rapid response capability and strong assault force, and the weapon system is required to have good maneuverability. The centralized use is an important principle of the application of artillery weapons of our army, and the timely maneuver is an important means for achieving the centralized use. For rocket launching systems, the requirements for maneuverability are higher due to the fact that the fire is large during launching and targets are easily exposed, and otherwise, the predetermined tasks cannot be completed.
Disclosure of Invention
The invention aims to: aiming at the existing problems, the invention provides a quick assembly and disassembly function, and the quick assembly and disassembly function has the passing capability and maneuvering capability in environments such as plains, mountainous regions, plateaus, towns, jungles and the like; the rocket projectile vehicle-mounted and ground integrated launching vehicle has a vehicle-mounted or ground launching function.
In order to achieve the above object, the present invention adopts the following technical solutions.
A rocket projectile vehicle-mounted and ground integrated launching vehicle comprises a chassis system, a launching device, a fire control system and a communication system; the launching device is movably arranged on the chassis system and comprises a base, a supporting frame, an azimuth mechanism, an undercarriage and a manual support; the supporting frame is rotatably connected with the base through an azimuth mechanism, the angle-adjustable movable mounting of the undercarriage is arranged on two sides of the supporting frame, and the manual support is arranged at the bottom of the base; the fire control system is used for controlling the launching of the rocket projectile, and the communication system is used for receiving and transmitting communication signals.
Further, the chassis system comprises an auxiliary frame, a supporting seat is arranged on the auxiliary frame, and an interface is arranged on the supporting seat and used for installing the launching device.
Furthermore, a marching fixer is arranged between the base and the supporting seat. The marching fixer has the effect of fixing the support frame.
Furthermore, trunnion seats are arranged on two sides of the support frame, and the undercarriage passes through the trunnion through a limiting bolt to be fixed on the support frame.
Further, the landing gear is fixed by a limiting bolt, and the adjusting angle of the landing gear is 0 degree, 20 degrees and 30 degrees.
Furthermore, the support frame is still installed on the base through the slewing bearing. Is beneficial to the rotation of the supporting frame.
Furthermore, the manual support comprises four supporting legs, and the supporting legs are fixed on the ground through the hoe.
Furthermore, the supporting legs are telescopic supporting legs.
Further, the landing gear is arranged in two layers.
The invention has the beneficial effects that:
the invention has the functions of quick assembly and disassembly, and has the passing capability and maneuvering capability in environments such as plains, mountainous regions, plateaus, towns, jungles and the like; the device has a vehicle-mounted or ground launching function, and meets the requirement on shooting precision; the device has the functions of loading and locking the cartridge guided rocket projectile; the device has the functions of shooting, shooting angle adjustment and measurement; wherein the fire control system has the functions of launching control and pre-shooting inspection of the rocket projectile,
drawings
FIG. 1 is a schematic view of the vehicle launch configuration of the present invention;
FIG. 2 is a side view of the vehicle launch structure of the present invention;
fig. 3 is a schematic view of the ground support launching structure of the present invention.
In the figure, 1-support frame; 2-a base; 3-manual support; 4-auxiliary frame; 5-a chassis; 6-undercarriage; 7-a communication system; 8-a fire control system; 9-marching fixation device; 10-an orientation mechanism; 11-cable.
Detailed Description
The technical solution of the present invention is further described below, but the scope of the claimed invention is not limited to the described.
As shown in fig. 1-3, a rocket projectile vehicle-mounted and ground integrated launching vehicle comprises a chassis 5 system, a launching device, a fire control system 8 and a communication system 7; the launching device is movably arranged on a chassis 5 system and comprises a base 2, a support frame 1, an azimuth mechanism 10, an undercarriage 6 and a manual support 3; the supporting frame 1 is rotationally connected with the base 2 through an azimuth mechanism 10, the undercarriage 6 is movably arranged on two sides of the supporting frame 1 in an angle-adjustable manner, and the manual support 3 is arranged at the bottom of the base 2; the fire control system 8 is used for controlling the launching of the rocket projectile, and the communication system 7 is used for receiving and transmitting communication signals.
The chassis 5 system includes sub vehicle frame 4, is equipped with the supporting seat on the sub vehicle frame 4, is equipped with the interface on the supporting seat and is used for installing emitter.
A marching fixer 9 is arranged between the base 2 and the supporting seat. The marching fixation device 9 has the function of fixing the support frame 1.
Trunnion seats are arranged on two sides of the support frame 1, and the undercarriage 6 penetrates through the trunnion through a limiting bolt to be fixed on the support frame 1.
The landing gear 6 is fixed by a limit bolt, and the angle of adjustment is 0 degree, 20 degrees and 30 degrees.
The supporting frame 1 is also arranged on the base 2 through a turntable bearing. Facilitating the rotation of the support 1.
The manual support 3 comprises four supporting legs, and the supporting legs are fixed on the ground through the hoe.
The supporting legs are telescopic supporting legs.
The landing gear 6 is arranged in two levels.
In conclusion, when the vehicle-mounted launcher is used for vehicle-mounted launching, the interface is arranged on the supporting seat of the auxiliary frame 4 of the chassis 5 and used for installing the launcher, and the launcher can be detached to facilitate manual carrying. The launching device comprises a base 2, a support frame 1, an azimuth mechanism 10, a landing gear 6 and a manual support 3. Base 2 direct mount is on the supporting seat, and support frame 1 passes through the slewing bearing and installs on base 2. The two sides of the support frame 1 are provided with trunnion seats which are connected with the undercarriage 6 through trunnions, and the undercarriage 6 is lifted up and down manually and is fixed at several angles of 0 degree, 20 degrees and 30 degrees by using a limiting bolt. The azimuth mechanism 10 is arranged in the base 2, the gear is arranged at the bottom of the support frame 1, and under the drive of the gear, the whole launching device can rotate relative to the base 2 through the gear to finish the azimuth aiming function. The undercarriage 6 is used as a fixed base body of the cartridge bomb, is provided with an installation interface and an electrical interface with the launching cartridge, is fixed for adapting to cartridge bomb loading, and is designed into an upper layer frame and a lower layer frame. The azimuth mechanism 10 mainly comprises a crank handle, a cover plate, a bearing, a rack, a screw rod and a gear, adopts a structural form that a sliding screw pair drives the rack to drive the gear, has the characteristics of stable operation, self-locking at any position, posture keeping and the like, can ensure that an upper mounting part is quickly adjusted to a transmitting position, and finally ensures that an azimuth shooting angle is adjusted within the range of +/-10 DEG
When the ground support is launched, the whole launching device part without the cartridge is detached from the vehicle and divided into two parts, then the launching device is transported to a designated fighting position, four supporting legs of the manual support 3 are adjusted to enable the launching device to be in a horizontal state, the supporting legs are fixed firmly by the hoe, then the cartridge is installed on the undercarriage 6, the launching device is manually adjusted to a specified altitude angle and azimuth angle according to a fire control instruction, the communication system 7 transmits signals to the launching device through the cable 11, and the fire control system 8 controls ignition to complete rocket projectile launching.
Claims (9)
1. The utility model provides a rocket projectile is on-vehicle, ground integration launch vehicle which characterized in that: comprises a chassis (5) system, a transmitting device, a fire control system (8) and a communication system (7); the launching device is movably arranged on a chassis (5) system and comprises a base (2), a support frame (1), an azimuth mechanism (10), an undercarriage (6) and a manual support (3); the supporting frame (1) is rotationally connected with the base (2) through an azimuth mechanism (10), the undercarriage (6) is movably arranged on two sides of the supporting frame (1) in an angle-adjustable manner, and the manual support (3) is arranged at the bottom of the base (2); the fire control system (8) is used for controlling the launching of the rocket projectile, and the communication system (7) is used for receiving and transmitting communication signals.
2. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 1, wherein: the chassis (5) system comprises an auxiliary frame (4), a supporting seat is arranged on the auxiliary frame (4), and an interface is arranged on the supporting seat and used for installing the launching device.
3. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 2, wherein: and a marching fixer (9) is also arranged between the base (2) and the supporting seat.
4. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 1, wherein: trunnion seats are arranged on two sides of the support frame (1), and the undercarriage (6) penetrates through the trunnion through a limiting bolt to be fixed on the support frame (1).
5. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 4, wherein: the landing gear (6) is fixed by a limiting bolt, and the adjusting angle is 0 degree, 20 degrees and 30 degrees.
6. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 1, wherein: the supporting frame (1) is also arranged on the base (2) through a turntable bearing.
7. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 1, wherein: the manual support (3) comprises four supporting legs, and the supporting legs are fixed on the ground through the hoe.
8. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 7, wherein: the supporting legs are telescopic supporting legs.
9. The rocket projectile vehicle-mounted and ground integrated launching vehicle as claimed in claim 1, wherein: the landing gear (6) is arranged in two layers.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911183155.2A CN110887405A (en) | 2019-11-27 | 2019-11-27 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911183155.2A CN110887405A (en) | 2019-11-27 | 2019-11-27 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110887405A true CN110887405A (en) | 2020-03-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911183155.2A Pending CN110887405A (en) | 2019-11-27 | 2019-11-27 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111998729A (en) * | 2020-09-11 | 2020-11-27 | 无锡聚锋防务科技有限公司 | Vehicle-mounted weapon station with protection shield |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2014550A6 (en) * | 1988-12-20 | 1990-07-16 | Nacional Santa Barbara De Ind | Bar for installation of a Milan missile-firing post on a light field (campaign) vehicle |
| CN2316624Y (en) * | 1998-03-11 | 1999-04-28 | 中国航天工业总公司第四研究院第四十一研究所 | Raining hail-suppression rocket launching device |
| JP2003336998A (en) * | 2002-05-21 | 2003-11-28 | Komatsu Ltd | Vehicle mounted gun launching mechanism |
| CN103884236A (en) * | 2014-03-03 | 2014-06-25 | 浙江海洋学院 | Movable precipitation cannonball firing frame |
| CN206479091U (en) * | 2017-01-20 | 2017-09-08 | 中国航天科工集团上海浦东开发中心 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
-
2019
- 2019-11-27 CN CN201911183155.2A patent/CN110887405A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2014550A6 (en) * | 1988-12-20 | 1990-07-16 | Nacional Santa Barbara De Ind | Bar for installation of a Milan missile-firing post on a light field (campaign) vehicle |
| CN2316624Y (en) * | 1998-03-11 | 1999-04-28 | 中国航天工业总公司第四研究院第四十一研究所 | Raining hail-suppression rocket launching device |
| JP2003336998A (en) * | 2002-05-21 | 2003-11-28 | Komatsu Ltd | Vehicle mounted gun launching mechanism |
| CN103884236A (en) * | 2014-03-03 | 2014-06-25 | 浙江海洋学院 | Movable precipitation cannonball firing frame |
| CN206479091U (en) * | 2017-01-20 | 2017-09-08 | 中国航天科工集团上海浦东开发中心 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111998729A (en) * | 2020-09-11 | 2020-11-27 | 无锡聚锋防务科技有限公司 | Vehicle-mounted weapon station with protection shield |
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Application publication date: 20200317 |
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| RJ01 | Rejection of invention patent application after publication |