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CN-122015573-A - Sliding rail type missile launching device

CN122015573ACN 122015573 ACN122015573 ACN 122015573ACN-122015573-A

Abstract

The invention provides a sliding rail type missile launching device which comprises a mounting seat, a supporting frame, a supporting plate, a missile fixing seat, an angle adjusting mechanism and a height adjusting mechanism, wherein the mounting seat is used for being fixed on a carrier, the height adjusting mechanism is arranged on the mounting seat and used for adjusting the height of the supporting frame, the angle adjusting mechanism is arranged on the supporting frame and used for adjusting the angle of the supporting plate, the missile fixing seat is arranged on the supporting plate and used for fixing a launcher, a stress wheel is arranged at the bottom of the supporting frame, and a supporting table used for supporting the upper part of the supporting plate is arranged on the supporting frame. The bearing wheel at the bottom of the supporting plate translates on the ground when the angle adjusting mechanism is adjusted, and the back of the supporting plate is always supported on the supporting table. The missile on the supporting plate can be supported on the ground no matter what angle the missile on the supporting plate is positioned, and the back of the supporting plate can be supported on the supporting table. The missile can be adjusted to any inclination angle on the premise of meeting the stress condition.

Inventors

  • ZHANG XIAOYU
  • ZHANG SHUAI
  • WEN JIAN

Assignees

  • 北京中航天佑科技有限公司

Dates

Publication Date
20260512
Application Date
20260330

Claims (7)

  1. 1. The sliding rail type missile launching device is characterized by comprising a mounting seat (1), a supporting frame (2), a supporting plate (3), a missile fixing seat (4), an angle adjusting mechanism (5) and a height adjusting mechanism (6), wherein the mounting seat (1) is used for being fixed on a carrier, the height adjusting mechanism (6) is arranged on the mounting seat (1) and used for adjusting the height of the supporting frame (2), the angle adjusting mechanism (5) is arranged on the supporting frame (2) and used for adjusting the angle of the supporting plate (3), the missile fixing seat (4) is arranged on the supporting plate (3) and used for fixing a launcher, a stress wheel (7) is arranged at the bottom of the supporting frame (2), and a supporting table (12) used for supporting the upper portion of the supporting plate (3) is arranged on the supporting frame (2).
  2. 2. The sliding rail type missile launching device according to claim 1, wherein the angle adjusting mechanism (5) comprises a sliding rail (51), a first connecting rod (53), a second connecting rod (54), a mechanism frame (56), a worm (58) and a worm wheel (57), the sliding rail (51) is arranged on the supporting frame (2) and is distributed along the length direction of the supporting frame (2), a pulley (52) is rotatably arranged on the supporting plate (3), the pulley (52) is slidably matched with the sliding rail (51), the mechanism frame (56) is fixed on the supporting frame (2), the worm (58) is pivoted on the mechanism frame (56), the worm wheel (57) is rotatably arranged on the mechanism frame (56) and meshed with the worm (58), the first connecting rod (53) is hinged with the second connecting rod (54) through a rotating shaft (55), the other end of the second connecting rod (54) is hinged on the supporting plate (3), and the other end of the first connecting rod (53) is hinged on the worm wheel (57).
  3. 3. The sliding rail type missile launching device according to claim 1 is characterized in that a rotating arm (9) is rotatably arranged on the mounting seat (1), the rotating arm (9) is connected with the supporting frame (2) through a height adjusting mechanism (6), and a motor I (10) connected with a rotating shaft of the rotating arm (9) is arranged on the mounting seat (1).
  4. 4. A sliding rail type missile launching device according to claim 3 is characterized in that the height adjusting mechanism (6) comprises a rotating frame (61), a sliding rod (62), a sliding sleeve (63) sleeved on the sliding rod (62) in a sliding mode, a screw rod (64), a nut (65) sleeved on the screw rod (64) in a threaded mode and a motor II (66), the rotating frame (61) is arranged on the rotating arm (9), the screw rod (64) and the sliding rod (62) are arranged on the rotating frame (61), the sliding sleeve (63) and the nut (65) are fixed on the supporting frame (2), and the motor II (66) is arranged on the rotating frame (61) and is coaxially connected with the screw rod (64).
  5. 5. A sliding track type missile launcher according to claim 2, characterized in that the worm (58) is coaxially connected with a rocking wheel (59).
  6. 6. The sliding rail type missile launching device according to claim 2 is characterized by further comprising a positioning mechanism (8), wherein the positioning mechanism (8) comprises a positioning plate (81), the positioning plate (81) is pivoted on the pulley (52), positioning holes (82) are formed in the sliding rail (51) at equal intervals along the length direction of the sliding rail, and positioning bolts (83) corresponding to the positioning holes (82) are connected to the positioning plate (81) in a threaded mode.
  7. 7. The sliding rail type missile launcher according to claim 1 is characterized in that the mounting base (1) is provided with a connecting hole (11) for connecting a carrier.

Description

Sliding rail type missile launching device Technical Field The invention relates to the technical field of artificial rainfall missile launching devices, in particular to a sliding rail type missile launching device. Background According to the physical characteristics of different cloud layers, the artificial rainfall is realized by selecting a proper time to scatter catalysts such as dry ice, silver iodide, salt powder and the like into the cloud by using an airplane and a rocket gun, so that the cloud layers are subjected to precipitation or precipitation amount is increased, drought in farmlands is relieved, the irrigation water amount or water supply capacity of reservoirs is increased, and because the airplane is limited by flight conditions, flight strokes and the like, the artificial rainfall is realized by adopting rocket-launched in county and city in a plurality of counties, and at present, a mobile vehicle-mounted launching device is conventionally adopted, so that the rainfall probability is improved by launching a plurality of shells at one time. However, because the launching device is arranged on the vehicle, the stress points are all on the vehicle during launching, and the shells can generate larger recoil during launching, the launching device without better supporting points is easily damaged by the larger recoil, and the serious problem is that the vehicle head tilts forward, so that safety accidents are easy to occur. Disclosure of Invention Aiming at the defects of the prior art, the invention provides a sliding rail type missile launching device, which solves the problems in the background art. The sliding rail type missile launching device comprises a mounting seat, a supporting frame, a supporting plate, a missile fixing seat, an angle adjusting mechanism and a height adjusting mechanism, wherein the mounting seat is used for being fixed on a carrier, the height adjusting mechanism is arranged on the mounting seat and used for adjusting the height of the supporting frame, the angle adjusting mechanism is arranged on the supporting frame and used for adjusting the angle of the supporting plate, the missile fixing seat is arranged on the supporting plate and used for fixing a launcher, a stress wheel is arranged at the bottom of the supporting frame, and a supporting table used for supporting the upper portion of the supporting plate is arranged on the supporting frame. Preferably, the angle adjusting mechanism comprises a sliding rail, a first connecting rod, a second connecting rod, a mechanism frame, a worm and a worm wheel, wherein the sliding rail is arranged on the supporting frame and is arranged along the length direction of the supporting frame, a pulley is rotatably arranged on the supporting plate, the pulley is slidably matched with the sliding rail, the mechanism frame is fixed on the supporting frame, the worm is pivoted on the mechanism frame, the worm wheel is rotatably arranged on the mechanism frame and is meshed with the worm, the first connecting rod is hinged with the second connecting rod through a rotating shaft, the other end of the second connecting rod is hinged on the supporting plate, and the other end of the first connecting rod is hinged on the worm wheel. Preferably, the mounting seat is rotatably provided with a rotating arm, the rotating arm is connected with the supporting frame through a height adjusting mechanism, and the mounting seat is provided with a motor I connected with a rotating shaft of the rotating arm. Preferably, the height adjusting mechanism comprises a rotating frame, a sliding rod, a sliding sleeve sleeved on the sliding rod in a sliding mode, a screw rod, a nut sleeved on the screw rod in a threaded mode and a second motor, the rotating frame is arranged on the rotating arm, the screw rod and the sliding rod are arranged on the rotating frame, the sliding sleeve and the nut are fixed on the supporting frame, and the second motor is arranged on the rotating frame and is coaxially connected with the screw rod. Preferably, the worm is coaxially connected with a rocking wheel. Preferably, the positioning mechanism further comprises a positioning plate, the positioning plate is pivoted on the pulley, positioning holes are formed in the sliding rail at equal intervals along the length direction of the sliding rail, and positioning bolts corresponding to the positioning holes are connected to the positioning plate through threads. Preferably, the mounting seat is provided with a connecting hole for connecting the carrier. The invention provides a sliding rail type missile launching device. The beneficial effects are as follows: 1. This slide rail formula guided missile emitter, when angle adjustment mechanism drives, through rocking wheel drive worm rotation, worm drive worm wheel anticlockwise rotation, worm wheel rotation drive connecting rod one around its anticlockwise rotation, connecting rod one drive connecting rod two backward pr