CN109489490B - Wind-resistant supporting leg mechanism suitable for intelligent landmine weapon system field layout - Google Patents

Wind-resistant supporting leg mechanism suitable for intelligent landmine weapon system field layout Download PDF

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Publication number
CN109489490B
CN109489490B CN201811577698.8A CN201811577698A CN109489490B CN 109489490 B CN109489490 B CN 109489490B CN 201811577698 A CN201811577698 A CN 201811577698A CN 109489490 B CN109489490 B CN 109489490B
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China
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supporting leg
fluted disc
intelligent
rectangular groove
landmine
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CN109489490A (en
Inventor
刘丽
傅宇雁
曹志义
龙钢
吴威
刘雪静
张悦
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Xian Institute of Modern Control Technology
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Xian Institute of Modern Control Technology
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00Means of attack or defence not otherwise provided for

Abstract

The invention belongs to the technical field of antitank intelligent mines, and particularly relates to an anti-wind type supporting leg mechanism suitable for outdoor layout of an intelligent mine weapon system. The landing leg mechanism provided by the invention can effectively adjust the levelness of the intelligent landmine weapon system, not only meets the stability of the system under different outdoor road conditions, but also structurally reduces the detection errors of the detection radar and the early warning detector; in addition, when the supporting leg mechanism is in a retracted state, the detection radar, the early warning detector sensor and the like can be effectively protected and prevented from being influenced by collision, meanwhile, the size of the recovered system structure is reduced, and the transportation and storage space is saved.

Description

Wind-resistant supporting leg mechanism suitable for intelligent landmine weapon system field layout
Technical Field
The invention belongs to the technical field of antitank intelligent mines, and particularly relates to an anti-wind type supporting leg mechanism suitable for field layout of an intelligent mine weapon system.
Background
Land mines have played an important role in a number of war operations in history. As in the second world war of world war, 4.4% of people in the united states and 33% of vehicles are caused by mine damage; in the war, the number of the components reaches 10% and 56% respectively; in the case of the war, the number of lesions increased to 33% and 77%, respectively. In the 80 s of the twentieth century, with the rapid development of microelectronic technology, novel warhead technology, land mines which can be deployed and the like, land mines are changed from static and passive defense into weapons which can be rapidly deployed and flexibly used and can be counterbalanced with modern mechanical armies. Particularly, the intelligent mines which are developed in succession in the western military kingdom and can autonomously detect, actively attack, accurately strike targets such as armors and the like are developed, so that the mines are changed and expanded in quality from concept, principle, performance to combat mode.
The intelligent antitank mine is a novel autonomous defensive weapon which utilizes high and new technologies such as acoustic and earthquake waves, a microwave detection locator, a millimeter wave/laser sensor to detonate ammunition, a computer, information, microelectronics, dynamics and the like to integrate into a whole and can detect and destroy targets such as armor and the like within a certain distance range. The device can automatically search targets such as a tank and an armored vehicle in a certain range, detect the azimuth and the distance of the targets, carry out firepower decision through a ground command controller, drive a transmitter to rotate to a transmitting position by a servo mechanism, transmit sub-ammunition to the upper air of the targets, scan and identify the targets by a sensor, and detonate a warhead above the targets to attack the top armor of the tank vehicle, thereby realizing accurate striking. An intelligent mine can play a role in blocking hundreds of traditional mines, has wide defense range and high damage rate, and has remarkable military benefit.
The foreign intelligent mines adopt sound sensors and vibration sensors to detect targets, when the sound sensors and the vibration sensors detect noise and vibration generated when a tank armored vehicle runs, a control system starts to identify the targets, the initial positions of the targets are calculated and automatically tracked, and when the targets travel to the attack range, attack ammunition is launched to destroy the targets. The most representative are the M93 wide area mines in the united states, the "MAZAC" anti-armored mines in france, the ADW smart mines in germany, and the "speed-30" attack top-armored smart mines in russia, etc.
The intelligent mines developed abroad at present adopt acoustic and vibration sensor combined mode type detection targets, and the phenomenon of inaccurate target detection or misjudgment often occurs. To overcome these defects, the intelligent mine developed in China consists of a control mine and attack Lei Liangda subsystem, and each combat unit consists of a control mine and an attack Lei Liangda subsystemAnd the attack mines are formed. The control mine is a control command center of the intelligent mine, adopts three sensor combination modes of sound, vibration and radar to pre-warn, identify, position and track an armored target, and a computer control system judges and decides the received information and timely sends out an attack instruction for the most favorable attack mine, and the attack mine emits ammunition attack target after receiving the instruction. Once inaccurate decisions are generated during service, attack mines can be disabled and even misemitted. Among three sensors, acoustic, seismic and radar, radar plays a decisive role in target positioning and tracking.
Disclosure of Invention
First, the technical problem to be solved
The invention aims to solve the technical problems that: how to provide a novel and practical wind-resistant supporting leg mechanism for the ground control subsystem of the antitank intelligent landmine weapon system, and is particularly suitable for the reliable supporting requirement when the ground control subsystem is rapidly arranged. The ground control subsystem is supported and regulated fast by the leg mechanism according to road condition laying requirements, and the detection precision of the acoustic shock early warning detector and the detection radar can be ensured structurally so as to ensure the normal operation of the ground control subsystem.
(II) technical scheme
In order to solve the problems in the prior art, the invention provides an anti-wind type supporting leg mechanism suitable for field layout of an intelligent landmine weapon system, wherein the anti-wind type supporting leg mechanism 1 comprises: the support leg mounting seat 4, the handle component 5, the support leg rod seat 6, the support leg rod welding piece 7, the screw cap 8, the first fluted disc 9, the second fluted disc 10 and the third fluted disc 11;
the main body of the supporting leg rod welding part 7 is of a hollow rectangular rod-shaped structure, the tail part of the supporting leg rod welding part is of a circular arc-shaped tilting structure, and conical screws are uniformly distributed on the tilting part;
the head 7-1 of the supporting leg rod welding piece 7 is connected with the supporting leg rod seat 6;
one end of the supporting leg rod seat 6 is provided with a first supporting leg rod seat connecting part which is connected with the head part 7-1 of the supporting leg rod welding piece 7, and the other end is provided with a second supporting leg rod seat connecting part which is in butt joint with the supporting leg mounting seat 4;
one end of the supporting leg installation seat 4 is provided with a first supporting leg installation seat connecting part for being in butt joint with a second supporting leg rod seat connecting part, and the other end of the supporting leg installation seat 4 is provided with a second supporting leg installation seat connecting part for being in butt joint with the intelligent landmine weapon system cabin 3;
the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part are both arranged into a double-supporting-lug connecting structure; the double-lug connection structure of the second support leg rod seat connection part comprises: left support lugs of the opening of the support leg rod seat and right support lugs of the opening of the support leg rod seat; the double-lug connection structure of the first support leg installation seat connection part comprises: left support lugs of the opening of the supporting leg installation seat and right support lugs of the opening of the supporting leg installation seat;
the outer wall surfaces of the left support lug of the opening of the support leg rod seat and the right support lug of the opening of the support leg rod seat are respectively embedded with a circular boss 6-3, the circular boss 6-3 of the left support lug is provided with a first rectangular groove 6-1 which is vertically arranged, and the circular boss 6-3 of the right support lug is provided with a second rectangular groove 6-2 which is horizontally arranged; the inner wall surface of the left support lug of the opening of the support leg installation seat is provided with a third rectangular groove 4-2 which is horizontally arranged, and the outer wall surface of the right support lug of the opening of the support leg installation seat is provided with a fourth rectangular groove 4-1 which is vertically arranged; the middle parts of the first rectangular groove 6-1 and the second rectangular groove 6-2 are respectively provided with a second through round hole 6-4; the middle parts of the third rectangular groove 4-2 and the fourth rectangular groove 4-1 are respectively provided with a first through round hole 4-6 which is the same as the second through round hole 6-4;
the number of the third fluted discs 11 is two, and the bottom of the first third fluted disc 11 is provided with a third fluted disc bottom boss 11-1 with the position and the shape matched with those of the first rectangular groove 6-1; the bottom of the second third fluted disc 11 is provided with a third fluted disc bottom convex part with the position and the shape matched with those of the second rectangular groove 6-2;
the bottom of the first fluted disc 9 is provided with a first fluted disc bottom boss 9-1 with the position and shape matched with those of the third rectangular groove 4-2, and the middle part of the first fluted disc bottom boss 9-1 is provided with a first fluted disc tail screw member 9-2; the middle part of the first fluted disc tail screw 9-2 is communicated, and the size of the through hole is the same as that of the first through round hole 4-6;
the bottom of the second fluted disc 10 is provided with a second fluted disc bottom boss 10-1 with the position and shape matched with the fourth rectangular groove 4-1;
the middle parts of the third fluted disc 11 and the second fluted disc 10 are respectively provided with through holes which are the same as the second through round holes 6-4 and the first through round holes 4-6;
at the butt joint part of the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part:
the third fluted disc bottom boss 11-1 of the first third fluted disc 11 is inserted into the first rectangular groove 6-1; the boss 9-1 at the bottom of the first fluted disc is inserted into the third rectangular groove 4-2;
the third fluted disc bottom convex part of the second and third fluted disc 11 is inserted into the second rectangular groove 6-2; the boss 10-1 at the bottom of the second fluted disc is inserted into the fourth rectangular groove 4-1;
the second supporting leg rod seat connecting part is inserted with the first supporting leg installation seat connecting part, so that two circular bosses 6-3 embedded on two lugs of the supporting leg rod seat 6 are exposed;
a disc spring is added between the first fluted disc 9 and the first third fluted disc 11, so that butt joint is carried out between the left support lug of the opening of the supporting leg rod seat and the left support lug of the opening of the supporting leg installation seat;
a disc spring is added between the second fluted disc 10 and the second third fluted disc 11, so that butt joint is carried out between the right support lug of the opening of the supporting leg rod seat and the right support lug of the opening of the supporting leg installation seat;
the handle assembly 5 includes a handle assembly shaft 5-1 and a shaft end 5-2; the handle assembly shaft 5-1 respectively passes through the third fluted disc 11, the first fluted disc 9, the second fluted disc 10, the second through round hole 6-4 and the first through round hole 4-6, and the shaft tail end 5-2 passes through the first fluted disc tail screw 9-2 and then is fixed by using a nut;
the first toothed disc tail screw 9-2 is sleeved with a spring washer and then screwed down by the nut 8.
The landing leg mechanism 1 is arranged at the lower part of the ground control subsystem 2 of the intelligent landmine weapon system.
The lower surface of the supporting leg mounting seat 4 is provided with a boss 4-3, and the boss 4-3 is mutually guided and matched with a groove 3-1 of the cabin body 3 of the intelligent landmine weapon system; the upper surface of the supporting leg installation seat 4 is provided with a threaded hole 4-4 and two square grooves 4-5 with circular arc openings, the supporting leg installation seat 4 is connected with the intelligent landmine weapon system cabin 3 through the threaded hole 4-4, and the supporting leg mechanism is fixed through the two square grooves 4-5 with circular arc openings on the upper surface of the supporting leg installation seat by adopting a pin shaft.
Wherein, the third fluted disc bottom boss 11-1 of the first third fluted disc 11 is inserted into the first rectangular groove 6-1 and connected by a screw.
Wherein, the boss 9-1 at the bottom of the first fluted disc is inserted into the third rectangular groove 4-2 and is fixed by a screw.
Wherein, the third fluted disc bottom protruding piece of second third fluted disc 11 inserts second rectangular groove 6-2 to adopt the screw connection.
Wherein, the boss 10-1 at the bottom of the second fluted disc is inserted into the fourth rectangular groove 4-1 and fixed by a screw.
Wherein the head 7-1 of the supporting leg rod welding member 7 is connected with the supporting leg rod seat 6 by adopting a screw.
The wind-resistant supporting leg mechanism aims at the ground condition of the layout, and the supporting leg mechanism 1 is adjusted to be in place, so that the stability of the ground control subsystem 2 of the intelligent landmine weapon system is improved, and the field layout of the ground control subsystem 2 of the intelligent landmine weapon system is completed.
Wherein, the landing leg mechanism is equipped with not less than three.
(III) beneficial effects
(1) The locking of the invention is generated by buckling the fluted disc with the end face provided with the teeth, and the hand wheel with the screw is rotated, so that buckling pressure (namely locking or unlocking) can be simultaneously formed or released between two pairs of fluted discs, thereby realizing the reliable locking of the supporting leg structure at any position in the swinging angle.
(2) The locking structure of the fluted disc after being buckled under pressure has a self-locking function, the cuboid convex strips arranged on the back surface of the fluted disc have the functions of positioning and limiting the relative movement between the fluted disc, and gaps between the fluted disc and other mechanisms are eliminated through the paired dished reed, so that the accurate locking of the adjusting position of the supporting leg can be effectively realized, and no looseness can occur due to wind blowing and shaking.
(3) The landing leg seat and the control cabin thin-wall body are positioned and matched and installed through a plane and cuboid matching key groove, and are limited and fixed through screws arranged below the cabin cover plate. The structure has large stress surface and strong random impact resistance, can greatly improve random supporting load borne by the thin-wall cabin body, and can prevent the connection limiting screw from loosening and falling off due to the fact that the landing leg shakes along with wind.
(4) The structural principle of the invention can be slightly improved according to the requirement, and can be applied to the supporting mechanism of similar products, thereby having wide application prospect.
Drawings
Fig. 1, 2 and 14 are schematic illustrations of the assembly of the leg mechanism and ground control subsystem of the present invention.
Fig. 3 is a schematic diagram of a leg mechanism.
Fig. 4 is a schematic view of the partial structure of fig. 3.
FIG. 5 is a schematic view of the leg mechanism in the ground control subsystem in a collapsed position.
Fig. 6 is a schematic view of the leg bar weld of fig. 3.
FIG. 7 is a schematic view of the third toothed disc of FIG. 4.
Fig. 8 is a schematic view of the leg bar base of fig. 3.
FIG. 9 is a schematic view of the first toothed disc of FIG. 3.
FIG. 10 is a schematic view of the second toothed disc of FIG. 3.
Fig. 11 is a schematic view of the leg mount of fig. 3.
FIG. 12 is a schematic view of the mounting surface of the leg lever mount and handle assembly of FIG. 3.
Fig. 13 is a schematic view of the handle assembly of fig. 3.
Wherein, 1 supporting leg mechanism; 2, a ground control subsystem; 3, a ground control subsystem cabin; 4, a supporting leg mounting seat; 5 a handle assembly; 6, supporting leg rod seats; 7, welding the supporting leg rod; 8, a nut; 9 a first fluted disc; 10 a second toothed disc; 11 a third fluted disc; 12 limit nails; three grooves are formed at the corresponding connection positions of the 3-1 supporting leg mechanism and the ground control subsystem; 4-3 lower surface bosses of the supporting leg installation seat; 4-4 screw holes on the upper surface of the supporting leg installation seat; 4-5 opening square grooves with circular arcs on the upper surface of the supporting leg installation seat; 5-1 a handle assembly shaft; 5-2 a handle assembly shaft end; 7-1 leg bar weld head; 9-1 a boss at the bottom of the first fluted disc; 9-2 a first fluted disc tail screw; 10-1 a boss at the bottom of the second fluted disc; 11-1 third fluted disc bottom boss.
Detailed Description
For the purposes of clarity, content, and advantages of the present invention, a detailed description of the embodiments of the present invention will be described in detail below with reference to the drawings and examples.
In order to solve the problems in the prior art, the invention provides an anti-wind type supporting leg mechanism suitable for field layout of an intelligent landmine weapon system, as shown in fig. 1-14, the anti-wind type supporting leg mechanism 1 comprises: the support leg mounting seat 4, the handle component 5, the support leg rod seat 6, the support leg rod welding piece 7, the screw cap 8, the first fluted disc 9, the second fluted disc 10 and the third fluted disc 11;
the main body of the supporting leg rod welding part 7 is of a hollow rectangular rod-shaped structure, the tail part of the supporting leg rod welding part is of a circular arc-shaped tilting structure, and conical screws are uniformly distributed on the tilting part;
the head 7-1 of the supporting leg rod welding piece 7 is connected with the supporting leg rod seat 6;
one end of the supporting leg rod seat 6 is provided with a first supporting leg rod seat connecting part which is connected with the head part 7-1 of the supporting leg rod welding piece 7, and the other end is provided with a second supporting leg rod seat connecting part which is in butt joint with the supporting leg mounting seat 4;
one end of the supporting leg installation seat 4 is provided with a first supporting leg installation seat connecting part for being in butt joint with a second supporting leg rod seat connecting part, and the other end of the supporting leg installation seat 4 is provided with a second supporting leg installation seat connecting part for being in butt joint with the intelligent landmine weapon system cabin 3;
the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part are both arranged into a double-supporting-lug connecting structure; the double-lug connection structure of the second support leg rod seat connection part comprises: left support lugs of the opening of the support leg rod seat and right support lugs of the opening of the support leg rod seat; the double-lug connection structure of the first support leg installation seat connection part comprises: left support lugs of the opening of the supporting leg installation seat and right support lugs of the opening of the supporting leg installation seat;
the outer wall surfaces of the left support lug of the opening of the support leg rod seat and the right support lug of the opening of the support leg rod seat are respectively embedded with a circular boss 6-3, the circular boss 6-3 of the left support lug is provided with a first rectangular groove 6-1 which is vertically arranged, and the circular boss 6-3 of the right support lug is provided with a second rectangular groove 6-2 which is horizontally arranged; the inner wall surface of the left support lug of the opening of the support leg installation seat is provided with a third rectangular groove 4-2 which is horizontally arranged, and the outer wall surface of the right support lug of the opening of the support leg installation seat is provided with a fourth rectangular groove 4-1 which is vertically arranged; the middle parts of the first rectangular groove 6-1 and the second rectangular groove 6-2 are respectively provided with a second through round hole 6-4; the middle parts of the third rectangular groove 4-2 and the fourth rectangular groove 4-1 are respectively provided with a first through round hole 4-6 which is the same as the second through round hole 6-4;
the number of the third fluted discs 11 is two, and the bottom of the first third fluted disc 11 is provided with a third fluted disc bottom boss 11-1 with the position and the shape matched with those of the first rectangular groove 6-1; the bottom of the second third fluted disc 11 is provided with a third fluted disc bottom convex part with the position and the shape matched with those of the second rectangular groove 6-2;
the bottom of the first fluted disc 9 is provided with a first fluted disc bottom boss 9-1 with the position and shape matched with those of the third rectangular groove 4-2, and the middle part of the first fluted disc bottom boss 9-1 is provided with a first fluted disc tail screw member 9-2; the middle part of the first fluted disc tail screw 9-2 is communicated, and the size of the through hole is the same as that of the first through round hole 4-6;
the bottom of the second fluted disc 10 is provided with a second fluted disc bottom boss 10-1 with the position and shape matched with the fourth rectangular groove 4-1;
the middle parts of the third fluted disc 11 and the second fluted disc 10 are respectively provided with through holes which are the same as the second through round holes 6-4 and the first through round holes 4-6;
at the butt joint part of the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part:
the third fluted disc bottom boss 11-1 of the first third fluted disc 11 is inserted into the first rectangular groove 6-1; the boss 9-1 at the bottom of the first fluted disc is inserted into the third rectangular groove 4-2;
the third fluted disc bottom convex part of the second and third fluted disc 11 is inserted into the second rectangular groove 6-2; the boss 10-1 at the bottom of the second fluted disc is inserted into the fourth rectangular groove 4-1;
the second supporting leg rod seat connecting part is inserted with the first supporting leg installation seat connecting part, so that two circular bosses 6-3 embedded on two lugs of the supporting leg rod seat 6 are exposed;
a disc spring is added between the first fluted disc 9 and the first third fluted disc 11, so that butt joint is carried out between the left support lug of the opening of the supporting leg rod seat and the left support lug of the opening of the supporting leg installation seat;
a disc spring is added between the second fluted disc 10 and the second third fluted disc 11, so that butt joint is carried out between the right support lug of the opening of the supporting leg rod seat and the right support lug of the opening of the supporting leg installation seat;
the handle assembly 5 includes a handle assembly shaft 5-1 and a shaft end 5-2; the handle assembly shaft 5-1 respectively passes through the third fluted disc 11, the first fluted disc 9, the second fluted disc 10, the second through round hole 6-4 and the first through round hole 4-6, and the shaft tail end 5-2 passes through the first fluted disc tail screw 9-2 and then is fixed by using a nut;
the first toothed disc tail screw 9-2 is sleeved with a spring washer and then screwed down by the nut 8.
The landing leg mechanism 1 is arranged at the lower part of the ground control subsystem 2 of the intelligent landmine weapon system.
The lower surface of the supporting leg mounting seat 4 is provided with a boss 4-3, and the boss 4-3 is mutually guided and matched with a groove 3-1 of the cabin body 3 of the intelligent landmine weapon system; the upper surface of the supporting leg installation seat 4 is provided with a threaded hole 4-4 and two square grooves 4-5 with circular arc openings, the supporting leg installation seat 4 is connected with the intelligent landmine weapon system cabin 3 through the threaded hole 4-4, and the supporting leg mechanism is fixed through the two square grooves 4-5 with circular arc openings on the upper surface of the supporting leg installation seat by adopting a pin shaft.
Wherein, the third fluted disc bottom boss 11-1 of the first third fluted disc 11 is inserted into the first rectangular groove 6-1 and connected by a screw.
Wherein, the boss 9-1 at the bottom of the first fluted disc is inserted into the third rectangular groove 4-2 and is fixed by a screw.
Wherein, the third fluted disc bottom protruding piece of second third fluted disc 11 inserts second rectangular groove 6-2 to adopt the screw connection.
Wherein, the boss 10-1 at the bottom of the second fluted disc is inserted into the fourth rectangular groove 4-1 and fixed by a screw.
Wherein the head 7-1 of the supporting leg rod welding member 7 is connected with the supporting leg rod seat 6 by adopting a screw.
The wind-resistant supporting leg mechanism aims at the ground condition of the layout, and the supporting leg mechanism 1 is adjusted to be in place, so that the stability of the ground control subsystem 2 of the intelligent landmine weapon system is improved, and the field layout of the ground control subsystem 2 of the intelligent landmine weapon system is completed.
Wherein, the landing leg mechanism is equipped with not less than three.
In summary, when the ground control subsystem is laid in the wild, the swing angle of the landing leg can be respectively adjusted and fixed according to the ground laying condition, the levelness of the subsystem can be quickly adjusted, the requirements of the subsystem on the stability of arrangement under the conditions of large windward side and high gravity center elevation when the control subsystem detects radar pull-up can be effectively ensured, and the landing leg mechanism is simple to operate, so that great convenience is brought to quick laying of intelligent mines, and the intelligent mine can adapt to and avoid the influence of various ground environments on the working performance of a weapon system.
The invention provides a supporting leg mechanism, which is used for fixing the upper part of a cabin body at the lower part of a ground control subsystem. The lower end of the supporting leg installation seat is provided with a rectangular boss, the boss is scratched into a hook-shaped groove of the ground control subsystem cabin body, and the upper surface of the supporting leg installation seat is tightly attached to the outer edge of the upper end of the subsystem cabin body. The outer edge of the cabin body is provided with a through hole and two threaded holes corresponding to the positions of the supporting legs, and the supporting leg mechanism is fixed by adopting screws through the through hole of the cabin body and the threaded holes on the upper surface of the supporting leg installation seat; the supporting leg installation seat is clamped by using screws through two threaded holes of the symmetrical through holes of the cabin body and rectangular grooves on the left side and the right side of the upper surface of the supporting leg installation seat.
The supporting leg mechanism provided by the invention consists of a supporting leg mounting seat, a first fluted disc, a nut, supporting legs, a second fluted disc, a handle component and the like. The landing leg mount pad and landing leg pole mount pad are the open slot form structure that has the circular arc appearance, have made things convenient for the free rotation of landing leg round handle subassembly axle, and handle subassembly axle passes landing leg pole mount pad, landing leg mount pad, first fluted disc, second fluted disc and third fluted disc, and the end is fixed with the nut. The handle is rotated anticlockwise, so that the support leg rod can be rotated, and a pin shaft is arranged on the side face of the support leg rod mounting seat so as to prevent excessive rotation of the support leg rod; the handle is rotated clockwise, the fluted discs with the tooth buckles on the end surfaces can be mutually meshed, the elastic disc springs arranged in pairs between the fluted discs can further eliminate the structure locking clearance, and the locking surfaces of the fluted discs, the supporting leg rod installation seats and the supporting leg installation seats are prevented from loosening due to shaking along with wind during the arrangement of the subsystem.
Example 1
According to the preferred embodiment of the invention, as shown in fig. 3, the leg mechanism comprises a leg mounting seat 4, a handle assembly 5, a leg rod seat 6, a leg rod welding part 7, a nut 8, a first fluted disc 9, a second fluted disc 10, a third fluted disc 11 and a limit nail 12.
According to the structure shown in fig. 1, after the locking force is released by rotating the hand wheel, the supporting effect can be adjusted by moving the supporting leg rod outwards or inwards, and when the floor with the ground nail below the supporting leg is reliably contacted with the ground, the hand wheel is screwed down to lock the position of the supporting leg.
According to the figures 1, 2 and 14, the supporting leg mechanism mounting seat is connected with the control cabin body through the matching strip in the form of an end face and a key groove, and is limited and connected with the body through a screw arranged above the supporting leg seat.
According to the structure shown in fig. 4, the 2 pairs of fluted discs, the 2 pairs of butterfly-shaped reeds, the 2 connecting seats and the like forming the supporting leg locking mechanism are connected in series through the hand wheel shaft, and when the hand wheel with threads is rotated clockwise or anticlockwise, the supporting leg rod seat fixedly connected with the supporting leg can be pushed to move leftwards or rightwards, so that the first fluted disc and the second fluted disc fixedly connected with the supporting leg rod seat are driven to move leftwards or rightwards, and the first fluted disc and the second fluted disc are respectively buckled or released with the third fluted disc, so that the locking or unlocking function of the supporting leg mechanism is realized.
According to the figures 6, 8, 9, 10 and 11, the two pairs of fluted discs are respectively limited with the connecting seat through the circular grooves and the rectangular convex strips and are fixedly connected with the connecting seat through screws, so that the problem of loosening caused by the change or movement of the locking positions of the fluted discs due to the relative rotation of the fluted discs after locking can be solved.
The foregoing is merely a preferred embodiment of the present invention, and it should be noted that modifications and variations could be made by those skilled in the art without departing from the technical principles of the present invention, and such modifications and variations should also be regarded as being within the scope of the invention.

Claims (10)

1. Wind-resistant landing leg mechanism suitable for intelligent mine weapon system field layout, its characterized in that, wind-resistant landing leg mechanism (1) includes: the landing leg mounting seat (4), the handle assembly (5), the landing leg rod seat (6), the landing leg rod welding piece (7), the screw cap (8), the first fluted disc (9), the second fluted disc (10) and the third fluted disc (11);
the main body of the supporting leg rod welding part (7) is of a hollow rectangular rod-shaped structure, the tail part of the supporting leg rod welding part is of a circular arc-shaped tilting structure, and conical screws are uniformly distributed on the tilting part;
the head (7-1) of the supporting leg rod welding piece (7) is connected with the supporting leg rod seat (6);
one end of the supporting leg rod seat (6) is provided with a first supporting leg rod seat connecting part which is connected with the head part (7-1) of the supporting leg rod welding piece (7), and the other end of the supporting leg rod seat is provided with a second supporting leg rod seat connecting part which is in butt joint with the supporting leg mounting seat (4);
one end of the supporting leg installation seat (4) is provided with a first supporting leg installation seat connecting part for being in butt joint with a second supporting leg rod seat connecting part, and the other end of the supporting leg installation seat is provided with a second supporting leg installation seat connecting part for being in butt joint with the intelligent landmine weapon system cabin body (3);
the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part are both arranged into a double-supporting-lug connecting structure; the double-lug connection structure of the second support leg rod seat connection part comprises: left support lugs of the opening of the support leg rod seat and right support lugs of the opening of the support leg rod seat; the double-lug connection structure of the first support leg installation seat connection part comprises: left support lugs of the opening of the supporting leg installation seat and right support lugs of the opening of the supporting leg installation seat;
the outer wall surfaces of the left support lug of the opening of the support leg rod seat and the right support lug of the opening of the support leg rod seat are respectively embedded with a circular boss (6-3), the circular boss (6-3) of the left support lug is provided with a first rectangular groove (6-1) which is vertically arranged, and the circular boss (6-3) of the right support lug is provided with a second rectangular groove (6-2) which is horizontally arranged; the inner wall surface of the left support lug of the opening of the support leg installation seat is provided with a third rectangular groove (4-2) which is horizontally arranged, and the outer wall surface of the right support lug of the opening of the support leg installation seat is provided with a fourth rectangular groove (4-1) which is vertically arranged; the middle parts of the first rectangular groove (6-1) and the second rectangular groove (6-2) are respectively provided with a second through round hole (6-4); the middle parts of the third rectangular groove (4-2) and the fourth rectangular groove (4-1) are respectively provided with a first through round hole (4-6) which is the same as the second through round hole (6-4);
the number of the third fluted discs (11) is two, and the bottom of the first third fluted disc (11) is provided with a third fluted disc bottom boss (11-1) with the position and the shape matched with those of the first rectangular groove (6-1); the bottom of the second third fluted disc (11) is provided with a third fluted disc bottom convex part with the position and the shape matched with those of the second rectangular groove (6-2);
the bottom of the first fluted disc (9) is provided with a first fluted disc bottom boss (9-1) with the position and shape matched with those of the third rectangular groove (4-2), and the middle part of the first fluted disc bottom boss (9-1) is provided with a first fluted disc tail screw member (9-2); the middle part of the first fluted disc tail screw member (9-2) is communicated, and the size of the through hole is the same as that of the first through round hole (4-6);
the bottom of the second fluted disc (10) is provided with a second fluted disc bottom boss (10-1) with the position and shape matched with the fourth rectangular groove (4-1);
the middle parts of the third fluted disc (11) and the second fluted disc (10) are respectively provided with through holes which are the same as the second through round holes (6-4) and the first through round holes (4-6);
at the butt joint part of the second supporting leg rod seat connecting part and the first supporting leg installation seat connecting part:
a third fluted disc bottom boss (11-1) of the first third fluted disc (11) is inserted into the first rectangular groove (6-1); the boss (9-1) at the bottom of the first fluted disc is inserted into the third rectangular groove (4-2);
a third fluted disc bottom convex part of the second and third fluted disc (11) is inserted into the second rectangular groove (6-2); the boss (10-1) at the bottom of the second fluted disc is inserted into the fourth rectangular groove (4-1);
the second support leg rod seat connecting part is inserted with the first support leg installation seat connecting part, so that two circular bosses (6-3) embedded on two lugs of the support leg rod seat (6) are exposed;
a disc spring is added between the first fluted disc (9) and the first third fluted disc (11), so that butt joint is carried out between the left lug of the opening of the supporting leg rod seat and the left lug of the opening of the supporting leg installation seat;
a disc spring is added between the second fluted disc (10) and the second third fluted disc (11), so that butt joint is carried out between the right support lug of the opening of the supporting leg rod seat and the right support lug of the opening of the supporting leg installation seat;
the handle assembly (5) comprises a handle assembly shaft (5-1) and a shaft end (5-2); the handle assembly shaft (5-1) respectively penetrates through the third fluted disc (11), the first fluted disc (9), the second fluted disc (10) and the second through round hole (6-4) and the first through round hole (4-6), and the shaft tail end (5-2) penetrates through the first fluted disc tail threaded piece (9-2) and is fixed by using a nut;
the first fluted disc tail screw (9-2) is sleeved with a spring washer and then is screwed by the nut (8).
2. The wind-resistant supporting leg mechanism suitable for field deployment of intelligent landmine weapon systems as claimed in claim 1, wherein the supporting leg mechanism (1) is arranged at the lower part of a ground control subsystem (2) of the intelligent landmine weapon system.
3. The wind-resistant supporting leg mechanism suitable for outdoor layout of intelligent landmine weapon systems, as claimed in claim 1, is characterized in that a boss (4-3) is arranged on the lower surface of the supporting leg mounting seat (4), and the boss (4-3) is mutually guided and matched with a groove-shaped groove (3-1) of the cabin body (3) of the intelligent landmine weapon system; the upper surface of the supporting leg installation seat (4) is provided with a threaded hole (4-4) and two open square grooves (4-5) with circular arcs, the supporting leg installation seat (4) is connected with the intelligent landmine weapon system cabin body (3) through the threaded hole (4-4), and the supporting leg mechanism is fixed through the two open square grooves (4-5) on the upper surface of the supporting leg installation seat by adopting a pin shaft.
4. Wind-resistant leg mechanism suitable for field deployment of intelligent landmine weapon systems according to claim 1, characterized in that the third toothed disc bottom boss (11-1) of the first third toothed disc (11) is inserted into the first rectangular slot (6-1) and connected with a screw.
5. Wind-resistant leg mechanism suitable for field deployment of smart landmine weapon systems according to claim 1, characterized in that the first toothed disc bottom boss (9-1) is inserted into the third rectangular slot (4-2) and screwed.
6. Wind-resistant leg mechanism suitable for field deployment of intelligent landmine weapon systems according to claim 1, characterized in that the third toothed disc bottom male member of the second third toothed disc (11) is inserted into the second rectangular groove (6-2) and connected with screws.
7. Wind-resistant leg mechanism suitable for field deployment of smart landmine weapon systems according to claim 1, characterized in that the second toothed disc bottom boss (10-1) is inserted into the fourth rectangular slot (4-1) and screwed.
8. Wind-resistant leg mechanism suitable for field deployment of intelligent landmine weapon systems according to claim 1, characterized in that the head (7-1) of the leg bar welding member (7) is screwed with the leg bar seat (6).
9. The wind-resistant supporting leg mechanism suitable for field layout of intelligent landmine weapon systems, as claimed in claim 1, is characterized in that the wind-resistant supporting leg mechanism is used for the field layout of the intelligent landmine weapon system ground control subsystem (2) by adjusting the supporting leg mechanism (1) in place according to the ground condition of the layout place, so that the stability of the intelligent landmine weapon system ground control subsystem (2) is improved.
10. The wind-resistant leg mechanism for outdoor deployment of intelligent land mine weapon systems of claim 1, wherein said leg mechanism is provided with at least three.
CN201811577698.8A 2018-12-20 2018-12-20 Wind-resistant supporting leg mechanism suitable for intelligent landmine weapon system field layout Active CN109489490B (en)

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