CN113928586B - Multifunctional bullet hanging vehicle capable of collecting, storing, carrying, hanging and preventing collection and fight and high efficiency - Google Patents
Multifunctional bullet hanging vehicle capable of collecting, storing, carrying, hanging and preventing collection and fight and high efficiency Download PDFInfo
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- CN113928586B CN113928586B CN202111182684.8A CN202111182684A CN113928586B CN 113928586 B CN113928586 B CN 113928586B CN 202111182684 A CN202111182684 A CN 202111182684A CN 113928586 B CN113928586 B CN 113928586B
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- 230000007246 mechanism Effects 0.000 claims abstract description 93
- 230000005540 biological transmission Effects 0.000 claims description 30
- 238000010008 shearing Methods 0.000 claims description 24
- 230000003028 elevating effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 3
- 230000006378 damage Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 241000237536 Mytilus edulis Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000020638 mussel Nutrition 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
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- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Warehouses Or Storage Devices (AREA)
Abstract
The invention discloses a multifunctional bullet hanging vehicle integrating storage, carrying, hanging and anti-trapping and high efficiency, belonging to the technical field of bullet hanging vehicles. The missile taking and hanging device comprises a frame, a missile storage device and a missile taking and hanging device; the frame comprises a bottom plate and two side plates, and the bottom plate is concave downwards to form a traversing mechanism channel; the missile storage device comprises a plurality of groups of automatic missile locking mechanisms, and each group of automatic missile locking mechanisms is arranged at the top of the side plate at equal intervals; the missile taking and hanging device comprises a horizontal traversing mechanism, a longitudinal lifting mechanism and a multidirectional travelling mechanism. Through setting up the missile storage device and getting and hanging the missile device on the frame, make the missile hanging car possess the function of storing the missile and getting and hanging the missile simultaneously, utilize horizontal sideslip mechanism and vertical elevating system's cooperation, install the missile after taking down from the frame on the fighter, greatly reduced get the bullet time, promoted and hung bullet efficiency.
Description
Technical Field
The invention relates to a multifunctional bullet hanging vehicle integrating storage, carrying, hanging and anti-trapping and high efficiency, belonging to the technical field of bullet hanging vehicles.
Background
The hanging bullet is an important link in the combat training or actual combat, and the main flow path of the hanging bullet is as follows: the transport tool, the ammunition warehouse, the ammunition hanging apron, the ammunition vehicle and the fighter plane, wherein the distance from the ammunition warehouse to the ammunition hanging apron is relatively long, the ammunition needs to be fetched for the first time, and meanwhile, a plurality of vehicles of the transport tool need to be transported in a reciprocating manner without stopping, so that the time is long; the carrier is stopped near the plane, but the missile hanging vehicle needs to take the bullets for the second time, and most of the missiles are taken only one, and the number of missiles required by the fighter is the number of the reciprocating secondary bullets, so that the reciprocating number takes more time, and the positioning is needed once again after each reciprocating, and the corresponding time is spent.
The prior art has the problems of low efficiency and too many manual intervention operations, the prior art is basically single operation in the industry, a plurality of functions are not concentrated in an automatic bullet hanging vehicle, so that the operations are needed to be repeated in actual combat, the time is prolonged, the combat condition is changed instantly, the existing bullet storage mode is stored through a fixed bullet guiding warehouse, once the bullet storage mode is screened in advance by an adversary, the warehouse is easy to be hit remotely by the adversary, once the bullet storage mode is hit, a nest end is formed, and the effects of a soldier, a mussel fighter and war situation are influenced.
Disclosure of Invention
The technical problems to be solved by the invention are as follows: the multifunctional bullet hanging vehicle is capable of collecting, carrying, hanging, preventing collection and fight and is high in efficiency, and the problem that bullet hanging efficiency is low due to the fact that the bullet hanging vehicle is single in function and too many in operation needing manual intervention in the prior art is solved.
The technical problems to be solved by the invention are realized by adopting the following technical scheme:
A multifunctional missile hanging vehicle integrating storage, carrying, hanging and anti-trapping and high-efficiency comprises a frame, a missile storage device and a missile taking and hanging device;
the frame comprises two side plates which are oppositely arranged, a bottom plate which is arranged at the bottoms of the two side plates, and a traversing mechanism channel which comprises a bottom surface and two opposite side surfaces is formed by downwards concavely forming the bottom plate;
the missile storage device comprises a plurality of groups of automatic missile locking mechanisms, each group of automatic missile locking mechanisms comprises two locking mechanisms, the two locking mechanisms are respectively and oppositely arranged at the top parts of the two side plates, and each group of automatic missile locking mechanisms are arranged at the top parts of the side plates at equal intervals;
The missile taking and hanging device comprises a horizontal traversing mechanism, a longitudinal lifting mechanism and a multidirectional travelling mechanism;
the horizontal traversing mechanism can be horizontally arranged in the traversing mechanism channel in a sliding way, the longitudinal lifting mechanism is arranged on the horizontal traversing mechanism, and the multidirectional travelling mechanism is arranged at the bottom of the bottom plate.
Preferably, the locking mechanism comprises a first shell, a first elastic piece, a first telescopic piece, a first clamping plate, a second shell, a second elastic piece, a second telescopic piece and a second clamping plate;
the first elastic piece is arranged in the first shell, the first telescopic piece is connected with the first elastic piece, one end of the first telescopic piece is telescopically arranged in the first shell, and the other end of the first telescopic piece is connected with the first clamping plate;
The second elastic piece is arranged in the second shell, the second telescopic piece is connected with the second elastic piece, one end of the second telescopic piece is telescopically arranged in the second shell, and the other end of the second telescopic piece is connected with the second clamping plate;
the first clamping plate and the second clamping plate are oppositely arranged, and the first shell and the second shell are oppositely arranged at the top of one side plate.
More preferably, the first clamping plate and the second clamping plate form a horn-shaped opening, wherein a first opening formed by one end of the first clamping plate connected with the first telescopic piece and one end of the second clamping plate connected with the second telescopic piece is smaller than a second opening formed by the other ends of the first clamping plate and the second clamping plate, and the caliber of the first opening is smaller than the diameter of the missile.
Preferably, the horizontal traversing mechanism comprises a first guide rail, a traversing base, rollers and a driving assembly;
The first guide rail is arranged on two side surfaces of the transverse moving mechanism channel;
a plurality of groups of rollers are arranged on two sides of the transverse moving base, and the rollers are arranged in the first guide rail;
the driving assembly comprises a first driving motor, a first gear and a first rack;
The first rack is transversely and horizontally arranged at the bottom of the transverse moving base, the first gear is in meshed transmission connection with the first rack, the first gear is arranged on the bottom surface of the transverse moving mechanism channel, and the first gear is connected with the first driving motor.
More preferably, the traversing mechanism channel is a concave structure.
More preferably, the first guide rail is provided at the bottoms of both side surfaces of the traverse mechanism passage.
More preferably, the rollers are symmetrically arranged at two sides of the traversing base.
Preferably, the longitudinal lifting mechanism comprises a bottom frame, a top frame, a second guide rail, a reduced shearing fork arm, a cross rod, a hydraulic cylinder, a mounting platform, a rotating piece, a second driving motor, a translation assembly and a pitching adjusting assembly;
The two sides of the bottom frame and the top frame are respectively provided with a second guide rail, and the bottom frame is arranged on the horizontal transverse moving mechanism;
the reducing type shearing fork arms comprise a plurality of groups of shearing fork arms which are connected in a hinged manner, wherein the first group of shearing fork arms are hinged with the end parts of the second guide rails at the two sides of the underframe, a cross rod is arranged between the second group of shearing fork arms, the two ends of the cross rod are hinged with the second group of shearing fork arms, one end parts of the second group of shearing fork arms are slidably arranged in the second guide rails at the two sides of the top frame, the third group of shearing fork arms are hinged with one end parts of the second guide rails at the two sides of the top frame, and one end parts of the fourth group of shearing fork arms are slidably arranged in the second guide rails at the two sides of the top frame;
the hydraulic cylinder is horizontally arranged on the underframe, and a telescopic rod of the hydraulic cylinder is hinged with the cross rod;
The translation assembly comprises a sliding rail, a sliding block and a carrier plate, wherein the sliding block can be arranged on the sliding rail in a sliding manner, and the carrier plate is arranged on the sliding block;
the pitching adjusting assembly comprises a lifting piece for lifting the missile and an adjusting piece for adjusting the pitching angle of the missile;
The rotating piece is arranged on the top frame, the mounting platform is arranged on the rotating piece, the rotating piece is arranged in the middle of the mounting platform, the rotating piece is connected with the second driving motor, the translation component is arranged on the mounting platform and is positioned on two sides of the rotating piece, and the pitching adjusting component is arranged on the carrier plate.
More preferably, the adjusting piece comprises a limiting clamp and an adjusting hand wheel, a second rack is arranged at the bottom of the limiting clamp, a second gear is arranged at one end of the adjusting hand wheel, and the second rack is in meshed transmission connection with the second gear.
More preferably, the translation assembly further comprises a third rack, a third gear and a third driving motor, the third gear is in meshed transmission connection with the third rack, the third driving motor is connected with the third gear, the third rack and the sliding rail are arranged on the mounting platform in parallel, and the third gear is connected with the carrier plate.
More preferably, the four sliding rails are arranged, and each two sliding rails are parallel to each other and are respectively arranged on two sides of the rotating piece.
Preferably, the multidirectional walking mechanism comprises a wheel body, a fourth driving motor, a fifth driving motor, a first transmission gear and a second transmission gear, wherein the side part of the wheel body is connected with the first transmission gear, the fourth driving motor is in transmission connection with the first transmission gear, the top part of the wheel body is connected with the second transmission gear, the fifth driving motor is in transmission connection with the second transmission gear, and the wheel body is connected with the bottom plate.
The beneficial effects of the invention are as follows:
(1) The invention provides a multifunctional missile hanging vehicle which is integrated with storage, carrying, hanging, anti-integrated fight and high-efficiency, and the missile hanging vehicle has the functions of storing missiles and taking the missiles by arranging a missile storing device and a missile taking device on a vehicle frame;
(2) The plurality of missiles are simultaneously locked on the frame by utilizing a plurality of groups of automatic missile locking mechanisms, so that the purpose of storing the missiles on the missile hanging vehicle is realized;
(3) The multi-directional travelling mechanism is utilized, so that the bullet hanging vehicle can steer and travel in multiple directions, and the operation singleness is greatly reduced; the missiles are taken down from the frame one by one and mounted on the fighter plane by utilizing the cooperation of the horizontal traversing mechanism and the longitudinal lifting mechanism, so that the missile taking time is greatly reduced, and the missile hanging efficiency is improved;
(4) Through the missile hanging vehicle loaded with missiles, the missiles are grouped and stored in a plurality of open places or a plurality of fixed buildings, so that the storage function of the goods shelves and the function of preventing striking dispersion are realized, the dispersed escape is realized, and the concentrated destruction can be effectively prevented.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present invention;
FIG. 2 is an enlarged view of A in FIG. 1;
FIG. 3 is an enlarged view of B in FIG. 1;
FIG. 4 is a schematic top view of the present invention;
FIG. 5 is a schematic diagram showing a top view of a missile lifted by the vertical lifting mechanism;
FIG. 6 is a schematic view of the overall structure of the longitudinal lifting mechanism of the present invention;
FIG. 7 is a schematic side view of the longitudinal lifting mechanism of the present invention;
fig. 8 is a schematic diagram of the overall structure of the present invention.
In the figure: 101. a side plate; 102. a bottom plate; 103. a traversing mechanism channel; 201. a first housing; 202. a first elastic member; 203. a first telescopic member; 204. a first clamping plate; 205. a second housing; 206. a second telescopic member; 207. a second clamping plate; 301. a first guide rail; 302. traversing the base; 303. a roller; 304. a chassis; 305. a top frame; 306. a second guide rail; 307. a first set of scissor arms; 308. a second set of scissor arms; 309. a third set of scissor arms; 310. a fourth set of scissor arms; 311. a cross bar; 312. a hydraulic cylinder; 313. a mounting platform; 314. A rotating member; 315. a second driving motor; 316. a slide rail; 317. a slide block; 318. a carrier plate; 319. a third rack; 320. a third gear; 321. a third driving motor; 322. a lifting member; 323. a limiting clamp; 324. An adjusting hand wheel; 325. a wheel body; 326. a fourth driving motor; 327. a fifth driving motor; 328. a first transmission gear; 329. a second transmission gear; 400. and (3) missile.
Detailed Description
The invention will be further described with reference to the following detailed drawings, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the invention easy to understand.
Embodiment one:
referring to fig. 1-8, the present embodiment provides a multifunctional missile hanging vehicle with functions of storage, carrying, hanging, anti-trapping and anti-trapping, and high efficiency, which comprises a frame, a missile storage device and a missile taking and hanging device.
The frame comprises two side plates 101 which are oppositely arranged, a bottom plate 102 which is arranged at the bottoms of the two side plates 101, the bottom plate 102 is downwards concave to form a traversing mechanism channel 103, and the traversing mechanism channel 103 comprises a bottom surface and two opposite side surfaces.
The missile storage device comprises a plurality of groups of automatic missile locking mechanisms, each group of automatic missile locking mechanisms comprises two locking mechanisms, the two locking mechanisms are respectively and oppositely arranged at the tops of the two side plates 101, and each group of automatic missile locking mechanisms are equidistantly arranged at the tops of the side plates 101.
The missile taking and hanging device comprises a horizontal traversing mechanism, a longitudinal lifting mechanism and a multidirectional travelling mechanism.
The horizontal traversing mechanism can be horizontally arranged in the traversing mechanism channel 103 in a sliding way, the longitudinal lifting mechanism is arranged on the horizontal traversing mechanism, and the multidirectional travelling mechanism is arranged at the bottom of the bottom plate 102.
The missile hanging vehicle can realize the mounting of all missiles 400 under a single wing only by running to one side wing for one-time positioning, and the missile hanging vehicle does not need to take and position reciprocally, so that a large amount of time can be saved, and the efficiency is higher.
Embodiment two:
referring to fig. 1 to 8, according to the first embodiment, the locking mechanism provided in this embodiment includes a first housing 201, a first elastic member 202, a first telescopic member 203, a first clamping plate 204, a second housing 205, a second elastic member, a second telescopic member 206, and a second clamping plate 207.
The first elastic member 202 is disposed in the first housing 201, the first telescopic member 203 is connected to the first elastic member 202, one end of the first telescopic member 203 is telescopically disposed in the first housing 201, and the other end of the first telescopic member 203 is connected to the first clamping plate 204.
The second elastic member is disposed in the second housing 205, the second telescopic member 206 is connected to the second elastic member, one end of the second telescopic member 206 is telescopically disposed in the second housing 205, and the other end of the second telescopic member 206 is connected to the second clamping plate 207.
The first clamping plate 204 is opposite to the second clamping plate 207, and the first housing 201 and the second housing 205 are opposite to each other and are disposed on top of one side plate 101.
The first clamping plate 204 and the second clamping plate 207 form a horn-shaped opening, wherein a first opening formed by one end of the first clamping plate 204 connected with the first telescopic member 203 and one end of the second clamping plate 207 connected with the second telescopic member 206 is smaller than a second opening formed by the other end of the first clamping plate 204 and the second clamping plate 207, and the caliber of the first opening is smaller than the diameter of the missile 400.
The first elastic piece 202 and the second elastic piece are specifically springs, the locking mechanism stretches and contracts the first stretching piece 203 and the second stretching piece 206 through the springs, the first stretching piece 203 drives the first clamping plate 204 to stretch and contract, the second stretching piece 206 drives the second clamping plate 207 to stretch and contract, when the missile 400 is placed between the first clamping plate 204 and the second clamping plate 207 from the upper portion of the first clamping plate 204 and the upper portion of the second clamping plate 207, the missile 400 extrudes the springs through the first clamping plate 204 and the second clamping plate 207, and the springs act on the first clamping plate 204 and the second clamping plate 207 through elasticity to lock the missile 400.
The missile 400 is transversely erected on two side plates 101 of the frame, namely one end part of the missile 400 is erected on one side plate 101, and the other end part is erected on the other side plate 101; one end of the missile 400 is clamped between the first clamping plate 204 and the second clamping plate 207 of the automatic locking missile device on one side plate 101, the other end of the missile 400 is clamped between the first clamping plate 204 and the second clamping plate 207 of the automatic locking missile device on the other side plate 101, a plurality of groups of automatic locking missile devices are arranged on the two side plates 101, six groups of automatic locking missile devices are arranged in the example, six missiles 400 are clamped by the six groups of automatic locking missile devices, and the missiles 400 are arranged in parallel side by side. By arranging a plurality of groups of automatic missile locking devices, a plurality of missiles 400 can be erected, and when the missiles 400 are transported at one time, the plurality of missiles 400 can be transported, so that the missile hanging time is effectively shortened. By storing the missile-mounted trolleys loaded with the missiles 400 in groups in single or multiple open places or multiple fixed buildings, the storage function of the goods shelves is realized, and when the missile-mounted trolleys loaded with the missiles 400 are detected and locked by enemies in the single or multiple open places or the fixed buildings, each trolley can independently travel to multiple target directions in the shortest time from a storage area, and is far away from a hitting range, so that the functions of scattered escape and centralized destruction prevention are realized.
Embodiment III:
referring to fig. 1 to 8, according to a first embodiment, the horizontal traversing mechanism provided in this embodiment includes a first guide rail 301, a traversing base 302, a roller 303, and a driving assembly.
The first guide rail 301 is arranged on two side surfaces of the traversing mechanism channel 103; the two sides of the traversing base 302 are provided with a plurality of groups of rollers 303, the rollers 303 are arranged in the first guide rail 301, specifically, two rollers 303 are symmetrically arranged on two sides of the traversing base 302 to balance the stress of the traversing base 302, the rollers 303 are connected with the traversing base 302 through bearings, the rollers 303 are provided with two groups, and the rollers 303 are respectively arranged near two ends of the traversing base 302.
The driving assembly comprises a first driving motor, a first gear and a first rack, wherein the first rack is transversely and horizontally arranged at the bottom of the transverse moving base 302, the first gear is in meshed transmission connection with the first rack, the first gear is arranged on the bottom surface of the transverse moving mechanism channel 103, and the first gear is connected with the first driving motor.
The traversing mechanism channel 103 is a concave structure, which is used for providing a walking space for a horizontal traversing mechanism and can accommodate a longitudinal lifting mechanism.
The first guide rail 301 is disposed at the bottom of two sides of the traversing mechanism channel 103, so as to provide more space above the horizontal traversing mechanism for the longitudinal lifting mechanism, so that the longitudinal lifting mechanism does not collide with the missile 400 when traversing along with the horizontal traversing mechanism.
Specifically, the horizontal traversing mechanism traverses in such a manner that the first driving motor drives the first gear to rotate, so that the traversing base 302 moves laterally due to the meshing transmission of the first rack and the first gear, and the roller 303 moves laterally in the first rail 301 during the lateral movement.
Embodiment four:
Referring to fig. 1 to 8, according to the first embodiment, the longitudinal lifting mechanism provided in this embodiment includes a bottom frame 304, a top frame 305, a second guide rail 306, a reduced scissor arm, a cross bar 311, a hydraulic cylinder 312, a mounting platform 313, a rotating member 314, a second driving motor 315, a translation assembly, and a pitch adjustment assembly.
The two sides of the bottom frame 304 and the top frame 305 are respectively provided with a second guide rail 306, and the bottom frame 304 is arranged on the horizontal traversing mechanism.
The reduced-type scissor arms comprise a plurality of groups of scissor arms which are connected in a hinged manner, wherein a first group of scissor arms 307 are hinged with the end parts of second guide rails 306 on two sides of a bottom frame 304, a cross rod 311 is arranged between the second group of scissor arms 308, two ends of the cross rod 311 are hinged with the second group of scissor arms 308, one end part of the second group of scissor arms 308 is slidably arranged in the second guide rails 306 on two sides of a top frame 305, a third group of scissor arms 309 are hinged with one end part of the second guide rails 306 on two sides of the top frame 305, one end part of the fourth group of scissor arms 310 is slidably arranged in the second guide rails 306 on two sides of the top frame 305, and the sliding mode of the second scissor arms in the guide rails on the bottom frame 304 and the sliding mode of the fourth scissor arms in the guide rails on the top frame 305 are pulleys arranged at the end parts and slide in the guide rails through the pulleys.
The hydraulic cylinder 312 is horizontally arranged on the chassis 304, the telescopic rod of the hydraulic cylinder 312 is hinged with the cross rod 311, when the telescopic rod stretches, the cross rod 311 is pushed to enable the second shearing fork arm to move towards the direction close to the first shearing fork arm, so that the inclined shearing fork arm is straightened, the lifting state of the longitudinal lifting mechanism is realized, when the telescopic rod contracts, the cross rod 311 is pulled to enable the second shearing fork arm to move towards the direction far away from the first shearing fork arm, and therefore the straightened shearing fork arm is enabled to restore to incline, and the descending state of the longitudinal lifting mechanism is realized.
The translation assembly comprises a sliding rail 316, a sliding block 317, and a carrier plate 318, wherein the sliding block 317 is slidably disposed on the sliding rail 316, and the carrier plate 318 is disposed on the sliding block 317. Four slide rails 316 are provided, and each two slide rails 316 are parallel to each other and are respectively arranged at two sides of the rotating member 314, so that stability of the translation assembly is improved. The translation assembly is moved on the slide rail 316 by the slide 317, thereby driving the carrier plate 318 to move. The translation assembly further comprises a third rack 319, a third gear 320 and a third driving motor 321, the third gear 320 is in meshed transmission connection with the third rack 319, the third driving motor 321 is connected with the third gear 320, the third rack 319 and the sliding rail 316 are arranged on the mounting platform 313 in parallel, and the third gear 320 is connected with the carrier plate 318. Specifically, the translation mode of the translation assembly is that the third driving motor 321 drives the third gear 320 to rotate, and then the third gear 319 is meshed and driven to drive the carrier plate 318 so as to drive the sliding block 317 to move along the sliding rail 316, so that the carrier plate 318 can move stably at a constant speed, and the missile 400 can move stably.
The pitch adjusting assembly comprises a lifting member 322 for lifting the missile 400 and an adjusting member for adjusting the pitch angle of the missile 400, wherein the upper part of the lifting member 322 is in a circular arc structure, so that the missile 400 is supported on the lifting member 322 and is not easy to shake out.
The rotating member 314 is arranged on the top frame 305, the mounting platform 313 is arranged on the rotating member 314, the rotating member 314 is arranged in the middle of the mounting platform 313, the rotating member 314 is connected with the second driving motor 315, the translation assembly is arranged on the mounting platform 313 and positioned on two sides of the rotating member 314, and the pitching adjusting assembly is arranged on the carrier plate 318. The rotation of the mounting platform 313 is that the second driving motor 315 drives the rotating member 314 to rotate, so as to drive the mounting platform 313 to rotate with the rotating member 314 as a rotation center.
The regulating part comprises a limiting clamp 323 and an adjusting hand wheel 324, a second rack is arranged at the bottom of the limiting clamp 323, a second gear is arranged at one end of the adjusting hand wheel 324, the second rack is in meshed transmission connection with the second gear, the limiting clamp 323 is of a V-shaped structure, the missile 400 can be smoothly adjusted during adjustment, and the adjusting range is larger.
Specifically, the adjusting piece is used in a manner that the hand wheel is rotated clockwise, the second rack is meshed with the second gear to drive, the second rack moves leftwards, the limiting clamp 323 moves leftwards or rightwards together with the second rack, the limiting clamp 323 is matched with the upper part of the lifting piece 322, one side of the missile 400 is contacted with one side of the limiting clamp 323, the other side of the missile 400 is contacted with the arc-shaped structure of the lifting piece 322, the missile 400 is pushed upwards along with the movement of the limiting clamp 323 to achieve lifting, the second rack is meshed with the second gear to drive through anticlockwise rotation of the hand wheel, the second rack moves rightwards, the limiting clamp 323 moves rightwards together with the second rack, the missile 400 pushed along with the movement of the limiting clamp 323 abuts against the limiting clamp 323 and the upper part of the lifting piece 322 to slide downwards, and therefore pitching adjustment of the missile 400 is achieved.
Embodiment four:
Referring to fig. 1-8, according to a first embodiment, the multidirectional walking mechanism provided by the present embodiment includes a wheel body 325, a fourth driving motor 326, a fifth driving motor 327, a first transmission gear 328, and a second transmission gear 329, wherein a side portion of the wheel body 325 is connected with the first transmission gear 328, the fourth driving motor 326 is in transmission connection with the first transmission gear 328, a top portion of the wheel body 325 is connected with the second transmission gear 329, the fifth driving motor 327 is in transmission connection with the second transmission gear 329, and the wheel body 325 is connected with the bottom plate 102.
The wheels are provided with four wheels which are respectively arranged at four corners of the bottom plate 102. The fourth driving motor 326 drives the first transmission gear 328 to rotate, so that the vehicle body can walk forwards or backwards; the fifth driving motor 327 drives the second transmission gear 329 to rotate, so that the vehicle body can deflect leftwards or rightwards, the traveling direction of the vehicle body can be exchanged by the reverse driving of the fourth driving motor 326, the fifth driving motor 327 drives the wheel body 325 to rotate leftwards or rightwards, the vehicle body can keep stable when traveling, the vehicle body is not required to turn around when the traveling direction is required to be exchanged, the vehicle body can travel in multiple directions, and the vehicle body can keep stable.
The foregoing has shown and described the basic principles, principal features and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, but is capable of various changes and modifications without departing from the spirit and scope of the invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The multifunctional missile hanging vehicle is characterized by comprising a vehicle frame, a missile storage device and a missile taking and hanging device;
the frame comprises two side plates which are oppositely arranged, a bottom plate which is arranged at the bottoms of the two side plates, and a traversing mechanism channel which comprises a bottom surface and two opposite side surfaces is formed by downwards concavely forming the bottom plate;
the missile storage device comprises a plurality of groups of automatic missile locking mechanisms, each group of automatic missile locking mechanisms comprises two locking mechanisms, the two locking mechanisms are respectively and oppositely arranged at the top parts of the two side plates, and each group of automatic missile locking mechanisms are arranged at the top parts of the side plates at equal intervals;
The missile taking and hanging device comprises a horizontal traversing mechanism, a longitudinal lifting mechanism and a multidirectional travelling mechanism;
The horizontal traversing mechanism can be horizontally arranged in the traversing mechanism channel in a sliding way, the longitudinal lifting mechanism is arranged on the horizontal traversing mechanism, and the multidirectional travelling mechanism is arranged at the bottom of the bottom plate;
The horizontal traversing mechanism comprises a first guide rail, a traversing base, rollers and a driving assembly;
The first guide rail is arranged on two side surfaces of the transverse moving mechanism channel;
a plurality of groups of rollers are arranged on two sides of the transverse moving base, and the rollers are arranged in the first guide rail;
the driving assembly comprises a first driving motor, a first gear and a first rack;
The first rack is transversely and horizontally arranged at the bottom of the transverse moving base, the first gear is in meshed transmission connection with the first rack, the first gear is arranged on the bottom surface of the transverse moving mechanism channel, and the first gear is connected with the first driving motor;
The longitudinal lifting mechanism comprises a bottom frame, a top frame, a second guide rail, a reduced shearing fork arm, a cross rod, a hydraulic cylinder, a mounting platform, a rotating piece, a second driving motor, a translation assembly and a pitching adjusting assembly;
The two sides of the bottom frame and the top frame are respectively provided with a second guide rail, and the bottom frame is arranged on the horizontal transverse moving mechanism;
the reducing type shearing fork arms comprise a plurality of groups of shearing fork arms which are connected in a hinged manner, wherein the first group of shearing fork arms are hinged with the end parts of the second guide rails at the two sides of the underframe, a cross rod is arranged between the second group of shearing fork arms, the two ends of the cross rod are hinged with the second group of shearing fork arms, one end parts of the second group of shearing fork arms are slidably arranged in the second guide rails at the two sides of the top frame, the third group of shearing fork arms are hinged with one end parts of the second guide rails at the two sides of the top frame, and one end parts of the fourth group of shearing fork arms are slidably arranged in the second guide rails at the two sides of the top frame;
the hydraulic cylinder is horizontally arranged on the underframe, and a telescopic rod of the hydraulic cylinder is hinged with the cross rod;
The translation assembly comprises a sliding rail, a sliding block and a carrier plate, wherein the sliding block can be arranged on the sliding rail in a sliding manner, and the carrier plate is arranged on the sliding block;
the pitching adjusting assembly comprises a lifting piece for lifting the missile and an adjusting piece for adjusting the pitching angle of the missile;
The rotating piece is arranged on the top frame, the mounting platform is arranged on the rotating piece, the rotating piece is arranged in the middle of the mounting platform, the rotating piece is connected with the second driving motor, the translation component is arranged on the mounting platform and is positioned on two sides of the rotating piece, and the pitching adjusting component is arranged on the carrier plate.
2. The multi-function vehicle of claim 1, wherein the locking mechanism comprises a first housing, a first elastic member, a first telescoping member, a first catch plate, a second housing, a second elastic member, a second telescoping member, a second catch plate;
the first elastic piece is arranged in the first shell, the first telescopic piece is connected with the first elastic piece, one end of the first telescopic piece is telescopically arranged in the first shell, and the other end of the first telescopic piece is connected with the first clamping plate;
The second elastic piece is arranged in the second shell, the second telescopic piece is connected with the second elastic piece, one end of the second telescopic piece is telescopically arranged in the second shell, and the other end of the second telescopic piece is connected with the second clamping plate;
the first clamping plate and the second clamping plate are oppositely arranged, and the first shell and the second shell are oppositely arranged at the top of one side plate.
3. The multifunctional bullet hanging vehicle of claim 1 wherein the adjusting member comprises a limiting clamp and an adjusting hand wheel, a second rack is arranged at the bottom of the limiting clamp, a second gear is arranged at one end of the adjusting hand wheel, and the second rack is in meshed transmission connection with the second gear.
4. The multi-functional bullet hanging vehicle of claim 1, wherein the translation assembly further comprises a third rack, a third gear and a third driving motor, the third gear is in meshed transmission connection with the third rack, the third driving motor is connected with the third gear, the third rack and the sliding rail are arranged on the mounting platform in parallel, and the third gear is connected with the carrier plate.
5. The multifunctional bullet hanging vehicle according to claim 1, wherein the number of the sliding rails is four, and each two sliding rails are parallel to each other and are respectively arranged on two sides of the rotating member.
6. The multi-functional hanging bullet vehicle of claim 1 wherein the multi-directional running mechanism comprises a wheel body, a fourth drive motor, a fifth drive motor, a first drive gear, a second drive gear, the side of the wheel body is connected with the first drive gear, the fourth drive motor is in drive connection with the first drive gear, the top of the wheel body is connected with the second drive gear, the fifth drive motor is in drive connection with the second drive gear, and the wheel body is connected with the bottom plate.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111182684.8A CN113928586B (en) | 2021-10-11 | 2021-10-11 | Multifunctional bullet hanging vehicle capable of collecting, storing, carrying, hanging and preventing collection and fight and high efficiency |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111182684.8A CN113928586B (en) | 2021-10-11 | 2021-10-11 | Multifunctional bullet hanging vehicle capable of collecting, storing, carrying, hanging and preventing collection and fight and high efficiency |
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| CN113928586A CN113928586A (en) | 2022-01-14 |
| CN113928586B true CN113928586B (en) | 2024-04-26 |
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| CN202180934U (en) * | 2011-07-20 | 2012-04-04 | 西安理工大学 | Missile hanging device of four-degree-of-freedom mechanical arm |
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| CN206886597U (en) * | 2017-06-28 | 2018-01-16 | 成都立航科技有限公司 | A kind of lifting mechanism for the lifting of missile |
| CN108216676A (en) * | 2018-01-22 | 2018-06-29 | 大连四达高技术发展有限公司 | Multiple degrees of freedom AGV fortune, bomb hoist device people's system |
| CN210592481U (en) * | 2019-08-22 | 2020-05-22 | 西安新宇航空维修工程有限公司 | Multi-degree-of-freedom aircraft missile hanging trailer |
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| CN202180934U (en) * | 2011-07-20 | 2012-04-04 | 西安理工大学 | Missile hanging device of four-degree-of-freedom mechanical arm |
| CN104192320A (en) * | 2014-09-19 | 2014-12-10 | 扬州万方电子技术有限责任公司 | Novel ammunition suspending vehicle |
| CN204508617U (en) * | 2014-12-31 | 2015-07-29 | 四川航泰航空装备有限公司 | A kind of aircraft bomb truck |
| CN206886597U (en) * | 2017-06-28 | 2018-01-16 | 成都立航科技有限公司 | A kind of lifting mechanism for the lifting of missile |
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| CN113928586A (en) | 2022-01-14 |
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