阅读说明：本技术 导弹联装模块定位锁紧装置 (Guided missile multi-unit module positioning and locking device ) 是由 吕文波 赵波 刘可平 彭永红 殷翔 杨珺柳 李佳圣 谢润 孙海涛 姜涛 姜晓明 于 2019-10-11 设计创作，主要内容包括：本发明提供了一种导弹联装模块定位锁紧装置,包括全向定位锁紧单元(100)、横向定位锁紧单元(200)、导向定位锁紧单元(400)以及导弹联装模块(300),导弹联装模块(300)包括上层面(310)和下层面(320),安装在上层的导弹联装模块(300)的下层面(320)与安装在下层导弹联装模块(300)的上层面(310)通过全向定位锁紧单元(100)、横向定位锁紧单元(200)和导向定位锁紧单元(400)紧固连接。通过导向、定位、锁紧功能一体化设计,导弹联装模块定位锁紧装置集成度更高,实现了尺寸小、重量轻、成本低的设计,同时操作简便,操作了操作效率。(The invention provides a missile combined module positioning and locking device which comprises an omnidirectional positioning and locking unit (100), a transverse positioning and locking unit (200), a guiding positioning and locking unit (400) and a missile combined module (300), wherein the missile combined module (300) comprises an upper layer (310) and a lower layer (320), the lower layer (320) of the missile combined module (300) arranged on the upper layer is fixedly connected with the upper layer (310) of the missile combined module (300) arranged on the lower layer through the omnidirectional positioning and locking unit (100), the transverse positioning and locking unit (200) and the guiding positioning and locking unit (400), and the missile combined module positioning and locking device is designed in a guide, positioning and locking mode , so that the missile combined module positioning and locking device is higher in integration level, small in size, light in weight and low in cost, simple and convenient to operate and high in operation efficiency.)

The positioning and locking device for the missile multi-unit installation modules is characterized by comprising an omnidirectional positioning and locking unit (100), a transverse positioning and locking unit (200), a guiding positioning and locking unit (400) and a missile multi-unit installation module (300);

the missile multi-unit module (300) comprises an upper layer (310) and a lower layer (320);

the lower layer (320) of the missile multi-unit module (300) arranged on the upper layer is tightly connected with the upper layer (310) of the missile multi-unit module (300) arranged on the lower layer through the omnidirectional positioning locking unit (100), the transverse positioning locking unit (200) and the guiding positioning locking unit (400).

2. The missile multi-unit module positioning and locking device of claim 1, wherein the omnidirectional positioning and locking unit (100) comprises an omnidirectional positioning and locking seat (110), an omnidirectional positioning and locking plate (120), a locking washer combination (500), an omnidirectional upper base (140) and an omnidirectional lower base (150);

the omnidirectional upper base (140), the omnidirectional positioning locking plate (120), the omnidirectional positioning locking seat (110) and the omnidirectional lower base (150) are sequentially connected;

the omnidirectional upper base (140) is provided with a full-upward base groove (141);

the omnidirectional positioning locking plate (120) is arranged on the omnidirectional upper base groove (141) in a matching way and is fixedly connected with the omnidirectional upper base (140);

the omnidirectional lower base (150) is provided with a full-downward base groove (151);

the omnidirectional positioning locking seat (110) is arranged on the omnidirectional lower base groove (151) in a matching way and is fixedly connected with the omnidirectional lower base (150);

an omnidirectional inserting lug (111) and an omnidirectional column section boss (112) are arranged on the omnidirectional positioning locking seat (110);

an omnidirectional guide hole (121) and an omnidirectional fixed clamping groove (122) are arranged on the omnidirectional positioning locking plate (120);

the omnidirectional column boss (112) is arranged in the omnidirectional guide hole (121) in a matching manner, and the omnidirectional positioning locking seat (110) and the omnidirectional positioning locking plate (120) are tightly connected through the omnidirectional inserting support lug (111) and the omnidirectional fixed clamping groove (122) by the locking washer combination (500);

the omnidirectional upper base (140) is fixedly arranged on the lower layer (320);

the omnidirectional lower base (150) is fixedly mounted on the upper deck (310).

3. The missile multi-piece module position locking device of claim 2, wherein the lock washer combination (500) comprises a lock fixing pin (510), a lock lever (520) and a lock nut (530);

the end of the locking rod (520) is tightly installed in the omnidirectional inserting support lug (111) through a locking fixing pin (510), and the other end of the locking rod (520) is tightly installed in the omnidirectional fixing clamping groove (122) through a locking nut (530).

4. The missile coupling module positioning and locking device of claim 2, wherein the omnidirectional column section boss (112) is a boss consisting of a convex spherical surface at the top, a circular truncated cone at the middle and a cylinder at the bottom;

the diameter of the omnidirectional column section boss (112) is D1, and the diameter of the omnidirectional guide hole (121) is D2;

0＜D2-D1≤0.5㎜。

5. the missile multi-piece module alignment and locking device of claim 1, wherein the transverse alignment and locking unit (200) comprises a transverse alignment and locking seat (210), a transverse alignment and locking plate (220), a locking washer combination (500), a transverse base (240) and a transverse lower base (250);

the transverse base (240), the transverse positioning locking plate (220), the transverse positioning locking seat (210) and the transverse lower base (250) are connected in sequence;

the transverse base (240) is provided with a transverse base groove (241);

the transverse positioning locking plate (220) is arranged on the transverse base groove (241) in a matching way and is fixedly connected with the transverse base (240);

the transverse lower base (250) is provided with a transverse lower base groove (251);

the transverse positioning locking seat (210) is arranged on the transverse lower base groove (251) in a matching way and is fixedly connected with the transverse lower base (250);

a transverse inserting lug (211) and a transverse column section boss (212) are arranged on the transverse positioning locking seat (210);

a transverse guide hole (221) and a transverse fixing clamping groove (222) are formed in the transverse positioning locking plate (220);

the transverse column section boss (212) is installed in the transverse guide hole (221) in a matching mode, and the transverse positioning locking seat (210) and the transverse positioning locking plate (220) are fixedly connected through the transverse inserting support lug (211) and the transverse fixing clamping groove (222) by the locking washer combination (500);

the transverse base (240) is tightly installed on the lower layer (320);

a transverse lower base (250) is securely mounted to the upper deck (310).

6. The missile multi-unit module positioning and locking device as claimed in claim 3 and claim 5, wherein the transverse column section boss (212) is a boss consisting of a convex spherical surface at the top and a regular prismatic table at the bottom;

the end of the locking rod (520) is tightly installed in the transverse inserting support lug (211) through a locking fixing pin (510), and the other end of the locking rod (520) is tightly installed in the transverse fixing clamping groove (222) through a locking nut (530).

7. The missile multi-unit module positioning and locking device as claimed in claim 1, wherein the guiding positioning and locking unit (400) comprises a guiding positioning locking seat (410), a guiding positioning locking plate (420), a locking washer combination (500), a guiding upper base (440) and a guiding lower base (450);

the guide upper base (440), the guide positioning locking plate (420), the guide positioning locking seat (410) and the guide lower base (450) are connected in sequence;

the guide upper base (440) is provided with a guide upper base groove (441);

the guide positioning locking plate (420) is installed on the guide upper base groove (441) in a matching way and is fixedly connected with the guide upper base (440);

the guide lower base (450) is provided with a guide lower base groove (451);

the guide positioning locking seat (410) is arranged on the guide lower base groove (451) in a matching way and is fixedly connected with the guide lower base (450);

a guide inserting lug (411) and a guide column section boss (412) are arranged on the guide positioning locking seat (410);

a guide hole (421) and a guide fixing clamping groove (422) are arranged on the guide positioning locking plate (420);

the guide column section boss (412) is arranged in the guide hole (421) in a clearance mode, and the guide positioning locking seat (410) and the guide positioning locking plate (420) are fixedly connected through the guide inserting support lug (411) and the guide fixing clamping groove (422) by the locking washer combination (500);

the guide upper base (440) is fixedly arranged on the lower layer (320);

the lower guide base (450) is mounted securely on the upper deck (310).

8. The missile multi-piece module positioning and locking device of claims 3 and 7, wherein the guide post section boss (412) is a boss consisting of a convex spherical surface at the top, a circular truncated cone at the middle and a cylinder at the bottom;

the diameter of the guide column section boss (412) is D3, and the diameter of the guide hole (421) is D4;

0.5㎜＜D4-D3≤5.5㎜；

the end of the locking lever (520) is tightly installed in the guide inserting support lug (411) through a locking fixing pin (510), and the other end of the locking lever (520) is tightly installed in the guide fixing clamping groove (422) through a locking nut (530).

9. The missile multi-unit module positioning and locking device of claim 1, wherein the omnidirectional positioning and locking unit (100), the transverse positioning and locking unit (200), and the guiding positioning and locking unit (400) are arranged on the upper layer (310) or the lower layer (320) according to any one of types:

-a parallelogram;

-a trapezoid;

-a triangle.

10. The missile multi-coupling module positioning and locking device as claimed in claim 1, wherein the missile multi-coupling module (300) is of a cuboid structure.

Technical Field

The invention relates to the field of missile weapon system ground launching devices, in particular to a positioning and locking device for missile multi-installation modules.

Background

The missile multi-unit module positioning and locking device is an important component of a missile multi-unit module or a missile launching vehicle. In the working processes of hoisting, fastening, transporting, fighting and the like of the missile multi-unit module to the missile multi-unit module or the missile launching vehicle, the missile multi-unit module positioning and locking device is used for realizing the functions of identifying, surface positioning and locking the missile multi-unit module on the missile multi-unit module or the missile launching vehicle so as to ensure the accurate transmission of the initial azimuth data of the missile launching vehicle to the missile multi-unit module and further provide accurate initial azimuth information for the missile; the positioning and locking device of the missile multi-unit module is released, and the separation of the missile multi-unit module can be realized.

At present, the positioning accuracy, the locking reliability, the use and maintenance convenience, the loading and replacement speed, the appearance size and the characteristic of facilitating image recognition under the background of automatic loading of the missile multi-unit module are all contents which need to be mainly solved and broken through by the positioning and locking device of the missile multi-unit module.A patent document CN208887823U discloses a quick opening and closing locking mechanism for a missile launcher force measuring device, wherein an I-shaped lug and tension spring fixing lugs on two sides are arranged on a mounting surface of a substrate, pairs of plate-shaped locking beams are symmetrically arranged in a narrow through groove, symmetrical positioning slide blocks are fixedly arranged in the middle of the two locking beams towards the mounting surface, a release button hole is arranged in the middle of the narrow through groove, a release button is arranged in the release button hole, a locking block is connected to the upper end of the release button, a cylindrical bulge is arranged in the direction opposite to the release button of the locking block, a pressure spring is arranged on the outer circular surface of the cylindrical bulge, and the other end of the pressure spring is connected with the substrate.

Disclosure of Invention

Aiming at the defects in the prior art, the invention aims to provide missile multi-installation module positioning and locking devices.

The positioning and locking device for missile multi-unit modules comprises an omnidirectional positioning and locking unit 100, a transverse positioning and locking unit 200, a guiding positioning and locking unit 400 and a missile multi-unit module 300;

missile multi-connection module 300 includes an upper level 310 and a lower level 320;

the lower layer 320 of the missile multi-purpose module 300 arranged at the upper layer is tightly connected with the upper layer 310 of the missile multi-purpose module 300 arranged at the lower layer through the omnidirectional positioning locking unit 100, the transverse positioning locking unit 200 and the guiding positioning locking unit 400.

Preferably, the omni-directional positioning locking unit 100 includes an omni-directional positioning locking seat 110, an omni-directional positioning locking plate 120, a locking washer combination 500, an omni-directional upper base 140, and an omni-directional lower base 150;

the omnidirectional upper base 140, the omnidirectional positioning locking plate 120, the omnidirectional positioning locking seat 110 and the omnidirectional lower base 150 are connected in sequence;

the all-upward base 140 is provided with an omni-directional upper base groove 141;

the omnidirectional positioning locking plate 120 is mounted on the omnidirectional upper base groove 141 in a matching manner and is fixedly connected with the omnidirectional upper base 140;

the omnidirectional lower base 150 is provided with a omnidirectional lower base groove 151;

the omnidirectional positioning locking seat 110 is installed on the omnidirectional lower base groove 151 in a matching manner and is fixedly connected with the omnidirectional lower base 150;

the omnidirectional positioning locking seat 110 is provided with an omnidirectional inserting lug 111 and an omnidirectional column section boss 112;

the omnidirectional positioning locking plate 120 is provided with an omnidirectional guide hole 121 and an omnidirectional fixed clamping groove 122;

the omnidirectional column boss 112 is installed in the omnidirectional guide hole 121 in a matching manner, and the omnidirectional positioning locking seat 110 and the omnidirectional positioning locking plate 120 are fastened and connected by the locking washer combination 500 through the omnidirectional inserting support lug 111 and the omnidirectional fixing clamping groove 122;

the full-up base 140 is fixedly mounted on the lower deck 320;

omni-directional lower base 150 is securely mounted to upper deck 310.

Preferably, the lock washer assembly 500 includes a lock fixing pin 510, a lock lever 520, and a lock nut 530;

the end of the locking lever 520 is tightly fixed in the omnidirectional plug-in lug 111 by the locking fixing pin 510, and the other end of the locking lever 520 is tightly fixed in the omnidirectional fixing slot 122 by the locking nut 530.

Preferably, the omnidirectional column section boss 112 is a boss composed of a convex spherical surface at the top, a circular truncated cone at the middle and a cylinder at the bottom;

the diameter of the omnidirectional column section boss 112 is D1, and the diameter of the omnidirectional guide hole 121 is D2;

0＜D2-D1≤0.5㎜。

preferably, the lateral positioning locking unit 200 comprises a lateral positioning locking seat 210, a lateral positioning locking plate 220, a locking washer combination 500, a lateral base 240 and a lateral lower base 250;

the transverse base 240, the transverse positioning locking plate 220, the transverse positioning locking seat 210 and the transverse lower base 250 are connected in sequence;

the lateral base 240 is provided with a lateral base groove 241;

the transverse positioning locking plate 220 is matched and arranged on the transverse base groove 241 and is fixedly connected with the transverse base 240;

the lateral lower base 250 is provided with a lateral lower base groove 251;

the transverse positioning locking seat 210 is matched and arranged on the transverse lower base groove 251 and is fixedly connected with the transverse lower base 250;

the transverse positioning locking seat 210 is provided with a transverse inserting lug 211 and a transverse column section boss 212;

the transverse positioning locking plate 220 is provided with a transverse guide hole 221 and a transverse fixing clamping groove 222;

the transverse column section boss 212 is installed in the transverse guide hole 221 in a matching manner, and the transverse positioning locking seat 210 and the transverse positioning locking plate 220 are fixedly connected through the transverse inserting support lug 211 and the transverse fixing clamping groove 222 by the locking washer combination 500;

the transverse base 240 is tightly mounted on the lower deck 320;

the transverse lower base 250 is securely mounted to the upper deck 310.

Preferably, the transverse pillar segment boss 212 is a boss consisting of a convex spherical surface at the top and a regular frustum of a prism at the bottom;

the end of the locking lever 520 is tightly fixed in the transverse plug-in lug 211 by the locking fixing pin 510, and the other end of the locking lever 520 is tightly fixed in the transverse fixing slot 222 by the locking nut 530.

Preferably, the guiding position locking unit 400 comprises a guiding position locking seat 410, a guiding position locking plate 420, a locking washer combination 500, a guiding upper base 440 and a guiding lower base 450;

the guide upper base 440, the guide positioning locking plate 420, the guide positioning locking seat 410 and the guide lower base 450 are connected in sequence;

the guide upper base 440 is provided with a guide upper base groove 441;

the guide positioning locking plate 420 is arranged on the groove 441 of the guide upper base in a matching way and is fixedly connected with the guide upper base 440;

the guide lower base 450 is provided with a guide lower base groove 451;

the guiding and positioning locking seat 410 is arranged on the guiding lower base groove 451 in a matching way and is fixedly connected with the guiding lower base 450;

the guiding and positioning locking seat 410 is provided with a guiding insertion support lug 411 and a guiding column section boss 412;

the guide positioning locking plate 420 is provided with a guide hole 421 and a guide fixing clamping groove 422;

the guide column section boss 412 is arranged in the guide hole 421 in a clearance mode, and the guide positioning locking seat 410 and the guide positioning locking plate 420 are tightly connected through the guide inserting support lug 411 and the guide fixing clamping groove 422 by the locking washer combination 500;

the guide upper base 440 is fixedly mounted on the lower deck 320;

the guide lower base 450 is securely mounted to the upper deck 310.

Preferably, the guide column section boss 412 is a boss consisting of a convex spherical surface at the top, a circular truncated cone at the middle and a cylinder at the bottom;

the diameter of the guide column section boss 412 is D3, and the diameter of the guide hole 421 is D4;

0.5㎜＜D4-D3≤5.5㎜；

the end of the locking lever 520 is tightly fixed in the guiding plug-in lug 411 by the locking fixing pin 510, and the other end of the locking lever 520 is tightly fixed in the guiding fixing slot 422 by the locking nut 530.

Preferably, the omni-directional positioning locking unit 100, the transverse positioning locking unit 200 and the guiding positioning locking unit 400 are arranged on the upper layer 310 or the lower layer 320 according to any of the following forms:

-a parallelogram;

-a trapezoid;

-a triangle.

Preferably, the missile multi-unit module 300 is a rectangular parallelepiped structure.

Compared with the prior art, the invention has the following beneficial effects:

1. through the integrated design of the guide, positioning and locking functions , the guided missile multi-unit module positioning and locking device has the functions of guide, positioning and locking at the same time, and is high in integration level, small in size, light in weight and low in cost.

2. According to the characteristics of the modules which need to be connected, the omnidirectional positioning locking unit, the transverse positioning locking unit and the guiding positioning locking unit are arranged in a coplanar or step-shaped distributed manner according to a parallelogram or a trapezoid or a triangle, and a plurality of positioning locking units work together to realize surface positioning within a certain precision range between the modules and sequential locking between two or more layers of modules.

3. The upper base and the lower base of the positioning and locking units with three different functions adopt a split design, the side is respectively welded with the upper and lower layers of missile combined modules, the side is respectively in threaded connection with the positioning and locking seat and the positioning and locking plate, the guided missile combined modules are integrally connected with threaded holes of the positioning and locking seat and the positioning and locking plate after welding, the central marking line of the positioning and locking units is integrally installed according to the set layout shape, and the higher-precision surface positioning of the guided missile combined module positioning and locking device is ensured.

4. The missile multi-unit module positioning and locking device integrates a positioning function and a locking function into an body, so that a separate tensioning device in the traditional design is not needed, the operation steps are fewer, the operation time is shorter, and the operation efficiency is higher.

5. The omnidirectional positioning locking unit, the transverse positioning locking unit and the guiding positioning locking unit which form the positioning locking device of the missile multi-unit module are designed according to the characteristics and the appearance contour which are convenient for machine identification in an intelligent automatic loading image identification scene, and can be used for the automatic loading working condition of the missile multi-unit module.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

FIG. 1 is a schematic structural diagram of a positioning and locking device of a missile multi-unit module;

FIG. 2 is an exploded view of the omni-directional positioning locking unit;

FIG. 3 is an exploded view of the lateral positioning locking unit;

FIG. 4 is an exploded view of the pilot positioning locking unit;

FIG. 5 is an exploded view of the lock washer assembly;

FIG. 6 is an exploded view of a missile multi-unit module positioning and locking device;

fig. 7 is a schematic structural diagram of a positioning and locking device of a missile multi-unit module.

The figures show that:

Detailed Description

The present invention is described in detail below with reference to specific examples which will assist those skilled in the art to further the present invention, but not to limit the invention in any way.

According to the positioning and locking device of missile multi-level modules provided by the invention, as shown in fig. 1, the positioning and locking device comprises an omnidirectional positioning and locking unit 100, a transverse positioning and locking unit 200, a guiding positioning and locking unit 400 and a missile multi-level module 300, wherein the missile multi-level module 300 comprises an upper layer 310 and a lower layer 320, in preferred examples, the missile multi-level module 300 is in a cuboid structure, the lower layer 320 of the missile multi-level module 300 arranged on the upper layer is fixedly connected with the upper layer 310 of the missile multi-level module 300 arranged on the lower layer through the omnidirectional positioning and locking unit 100, the transverse positioning and locking unit 200 and the guiding positioning and locking unit 400, and the missile multi-level module positioning and locking device simultaneously has the functions of guiding, positioning and locking through the integrated design of the guiding, positioning and locking functions , and has the advantages of high integration level, small size, light weight and low cost.

Further , as shown in fig. 1, in preferred examples, the omnidirectional positioning and locking unit 100, the transverse positioning and locking unit 200, and the guiding positioning and locking unit 400 are arranged in a coplanar distributed manner in a rectangular arrangement, wherein the number of the transverse positioning and locking units 200 is two and arranged at two opposite corners of the rectangle, the omnidirectional positioning and locking unit 100 and the guiding positioning and locking unit 400 are respectively installed at the other two opposite corners of the rectangle to jointly work with the missile coupling module 300 through four positions of the four locking units, so as to jointly realize surface positioning within the fixed precision range of between the modules, and sequential locking between two or more layers of modules, among variants, the omnidirectional positioning and locking unit 100, the transverse positioning and locking unit 200, and the guiding positioning and locking unit 400 are arranged in a trapezoidal manner between two missile coupling modules 300, both ends of the upper bottom of the trapezoid are respectively installed with the omnidirectional positioning and locking unit 100 and the transverse positioning and locking unit 400, among variants, both ends of the trapezoid are respectively installed with the omnidirectional positioning and locking unit 100, the transverse positioning and locking unit 200, the guiding positioning and locking unit 400, and the guiding positioning and locking unit 400 are arranged in a trapezoidal manner that the two layers of the modules are firmly connected in a ladder-shaped manner, so that the modules are arranged in parallel connection with the same height of the triangle, and the trapezoidal module, and the modules, so that the modules are firmly connected in a stable manner.

Specifically, as shown in fig. 2, the omnidirectional positioning locking unit 100 includes an omnidirectional positioning locking seat 110, an omnidirectional positioning locking plate 120, a locking washer assembly 500, an omnidirectional upper base 140, and an omnidirectional lower base 150, the omnidirectional upper base 140, the omnidirectional positioning locking plate 120, the omnidirectional positioning locking seat 110, and the omnidirectional lower base 150 are sequentially connected, the omnidirectional upper base 140 is provided with an omnidirectional upper base groove 141, the omnidirectional positioning locking plate 120 is fittingly installed on the omnidirectional upper base groove 141 and is tightly connected with the omnidirectional upper base 140, in preferred examples, the front surface of the base groove 141 is provided with a plurality of blind holes with internal threads, the omnidirectional positioning locking plate 120 is provided with a plurality of through holes, and bolts are tightly fastened in the blind holes with internal threads through holes, so that the omnidirectional positioning locking plate 120 and the omnidirectional upper base 140 are tightly connected to the .

, as shown in fig. 2, the omnidirectional lower base 150 is provided with a full downward base groove 151, the omnidirectional positioning locking seat 110 is fittingly installed on the omnidirectional lower base groove 151 and is tightly connected with the omnidirectional lower base 150, in preferred examples, the front surface of the omnidirectional lower base groove 151 is provided with a plurality of blind holes with internal threads, the omnidirectional positioning locking seat 110 is provided with a plurality of through holes, and bolts are fastened in the blind holes with internal threads through the through holes, so that the omnidirectional lower base 150 and the omnidirectional positioning locking seat 110 are tightly connected with .

Further , an omnidirectional inserting support lug 111 and an omnidirectional column section boss 112 are arranged on the omnidirectional positioning locking seat 110, an omnidirectional guide hole 121 and an omnidirectional fixed clamping groove 122 are arranged on the omnidirectional positioning locking plate 120, the omnidirectional column section boss 112 is installed in the omnidirectional guide hole 121 in a matched manner, the locking washer combination 500 fastens the omnidirectional positioning locking seat 110 and the omnidirectional positioning locking plate 120 through the omnidirectional inserting support lug 111 and the omnidirectional fixed clamping groove 122, as shown in fig. 2, the omnidirectional column section boss 112 is a boss consisting of a convex spherical surface at the top, a round table in the middle and a cylinder at the bottom, the omnidirectional column section boss 112 has a diameter of D1, the omnidirectional guide hole 121 has a diameter of D2, 0 < D2-D1, which is not more than 0.5 mm, a spherical surface or a conical section formed by the convex spherical surface at the top of the omnidirectional column section boss 112 and the round table in the middle guides the corresponding omnidirectional guide hole to slide towards the cylinder section in a butting process, the cylinder section is matched with the corresponding omnidirectional guide hole 121, the cylinder section is matched with the cylinder section 121, the longitudinal and transverse distance and the locking unit arranged in the locking device are arranged according to realize the positioning accuracy of the connection device, the locking device, the optimal positioning seat 110 and the positioning seat 110, the optimal positioning seat 120 is 3875 mm, the optimal positioning seat 120, the optimal positioning seat diameter of which is 3875, and the cylinder section forming example.

Specifically, as shown in fig. 2, the diameter of the spherical section of the omnidirectional column section boss 112, the taper of the circular truncated cone section, the diameter of the cylindrical section, and the height are determined by comprehensive calculation according to the initial docking deviation of the missile coupling module 300, the tangential load borne by the module in the transportation and missile launching processes, and the image recognition accuracy in the docking process, and the top view profile of the omnidirectional positioning locking seat 110 from the omnidirectional column section boss 112 to the omnidirectional lower base 150 direction is composed of a central circle, a rectangular main body boundary, and a rectangular outward extending boundary, so as to provide an image recognition mark for hoisting.

Specifically, as shown in fig. 5, the lock washer assembly 500 includes a lock fixing pin 510, a lock rod 520 and a lock nut 530. in preferred embodiments of , the omnidirectional plug-in lug 111 is two extended holed lugs with a gap therebetween, the holed end of the lock rod 520 is mounted in the gap between the lugs, the lock fixing pin 510 passes through the lug hole and the holed end of the lock rod 520 to tightly connect the lock rod 520 in the gap between the omnidirectional plug-in lugs 111, the other end of the lock rod 520 is tightly mounted in the omnidirectional fixing slot 122 by the lock nut 530, so that the omnidirectional upper base 140 and the omnidirectional lower base 150 are tightly connected together at , the omnidirectional upper base 140 is tightly mounted at the lower level 320, e.g., by welding, the omnidirectional lower base 150 is tightly mounted at the upper level 310, e.g., by welding, so that the omnidirectional upper base 140 and the omnidirectional lower base 150 are tightly connected by the lock washer assembly 500, the horizontal base 240 and the horizontal lower base 250 are also connected by the lock washer assembly 500, the upper base 440 and the lower base 450 are also connected by the lock washer assembly 500, and the lock positioning module 300 is loosened by the vertical positioning module, the vertical positioning module is a vertical positioning module, and a vertical positioning module is achieved by the vertical positioning module, the vertical.

Specifically, as shown in fig. 3, the transverse positioning and locking unit 200 comprises a transverse positioning and locking seat 210, a transverse positioning and locking plate 220, a locking washer assembly 500, a transverse base 240 and a transverse lower base 250, wherein the transverse base 240, the transverse positioning and locking plate 220, the transverse positioning and locking seat 210 and the transverse lower base 250 are connected in sequence, the transverse base 240 is provided with a transverse base groove 241, the transverse positioning and locking plate 220 is mounted on the transverse base groove 241 and is fixedly connected with the transverse base 240, the transverse lower base 250 is provided with a transverse lower base groove 251, the transverse positioning and locking seat 210 is mounted on the transverse lower base groove 251 and is fixedly connected with the transverse lower base 250, the transverse positioning and locking seat 210 is provided with a transverse plug lug 211 and a transverse column boss 212, the transverse positioning and locking plate 220 is provided with a transverse guide hole 221 and a transverse fixing slot 222, the transverse column boss 212 is mounted in the transverse guide hole 221, the locking washer assembly 500 fastens the transverse positioning and locking seat 210 and the transverse positioning and locking plate 220 through the transverse plug lug 211 and the transverse fixing slot 222, the transverse plug lug boss 240 is mounted on the upper base seat 220 and the transverse fixing slot 212, the transverse plug lug boss 240, the transverse plug lug boss 212 is mounted on the transverse guide slot mount interface of the transverse guide platform 250, the transverse column mounting face of the transverse positioning and the transverse column mounting face, the transverse column module is provided with a transverse positioning and a transverse column module, the transverse connection module is provided with a transverse connection module, the transverse connection module is provided with the transverse connection module.

Specifically, as shown in fig. 4, the guiding, positioning and locking unit 400 includes a guiding and positioning locking seat 410, a guiding and positioning locking plate 420, a locking washer assembly 500, a guiding upper base 440 and a guiding lower base 450, the guiding upper base 440, the guiding and positioning locking plate 420, the guiding and positioning locking seat 410 and the guiding lower base 450 are sequentially connected, the guiding upper base 440 is provided with a guiding upper base groove 441, the guiding and positioning locking plate 420 is fittingly installed on the guiding upper base groove 441 and is tightly connected with the guiding upper base 440, the guiding lower base 450 is provided with a guiding lower base groove 451, the guiding and positioning locking seat 410 is fittingly installed on the guiding lower base groove 451 and is tightly connected with the guiding lower base 450, the guiding and positioning locking seat 410 is provided with a guiding insertion lug 411 and a guiding column section boss 412, the guiding and a guiding fixing slot 422 are provided on the guiding and positioning locking plate 420, the guiding and positioning locking plate 420 is provided with a guiding guide hole 421 and a guiding fixing slot 422, the guiding column section boss 412 is installed in the guiding guide hole 421 through a gap, the locking washer assembly 500 fasteningly connected with the guiding upper base 440 and the guiding column boss, the guiding locking seat 410 is installed on the lower base, the guiding column section boss 410, the guiding column boss is preferably, the guiding column boss is composed of which has a diameter of 3975 mm, the top of a cylindrical guide column section, the top of a cylindrical boss of which is equal to 3-35 mm, the top of the cylindrical boss, the cylindrical boss of which is equal to 35 mm, the cylindrical boss of which.

The three types of positioning and locking units work together to realize surface positioning of the connected two layers of modules within the fixed precision range of and sequential locking of two or more layers of modules.

As shown in fig. 6 and 7, in preferred examples, the omnidirectional positioning locking unit 100, the transverse positioning locking unit 200, and the guiding positioning locking unit 400 are arranged in a coplanar and distributed manner according to a rectangular shape, the diameter of the cylindrical section of the omnidirectional positioning locking seat 110 is 45mm, the diameter of the cylindrical section of the transverse positioning locking seat 210 is 45mm, the diameter of the cylindrical section of the guiding positioning locking seat 410 is 40mm, and the diameters of the omnidirectional guiding hole 121, the transverse guiding hole 221, and the guiding hole 421 are all 45.5mm, so that 3' precision surface positioning between the upper missile coupling module 300 and the lower missile coupling module 300 and reliable locking of a 5.5t load of the missile coupling module can be realized.

By taking the positioning and locking units as an example according to a rectangular arrangement, the working principle of the invention is as follows:

as shown in fig. 6 and 7, marking a mark line at a locking installation position of the missile coupling module 300, respectively welding the omnidirectional upper base 140, the two horizontal bases 240 and the guide upper base 440 on the lower layer 320 of the missile coupling module 300 according to the mark line, respectively welding the omnidirectional upper base 140, the horizontal base 240 and the guide upper base 440 with the omnidirectional positioning locking plate 120, the horizontal positioning locking plate 220 and the guide positioning locking plate 420 through bolts, respectively welding the omnidirectional lower base 150, the two horizontal lower bases 250 and the guide lower base 450 on the upper layer 310 of the missile coupling module 300 according to the mark line, respectively welding the omnidirectional lower base 150, the horizontal positioning locking seat 210 and the guide positioning locking seat 410 through bolts, respectively, when installing a missile, missile coupling modules 300 move to be directly above another missile coupling modules 300, operating the upper rectangular coupling module 300 to descend to be close to the lower coupling module 300 when installing a missile, respectively enabling the missile coupling modules to descend to be close to the lower coupling module 300 according to the top points of the omnidirectional positioning locking seat 110, the horizontal positioning locking seat 210 and the horizontal positioning locking seat 410, respectively, and the missile coupling modules 300 to be capable of being automatically installed in a vertical positioning and guiding connection mode, and enabling the guide post coupling modules to be sequentially arranged in a loading scene, and enabling the upper and horizontal coupling module 300 to be sequentially arranged in a loading and a loading model, and enabling the top point of a loading and a loading model to be sequentially to be conveniently realized by two layers of a loading model.

In the description of the present application, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present application and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application.

The foregoing description of specific embodiments of the present invention has been presented. It is to be understood that the present invention is not limited to the specific embodiments described above, and that various changes or modifications may be made by one skilled in the art within the scope of the appended claims without departing from the spirit of the invention. The embodiments and features of the embodiments of the present application may be combined with each other arbitrarily without conflict.