CN211552612U

CN211552612U - Guided missile simulation launching device for submarine model

Info

Publication number: CN211552612U
Application number: CN201922496678.4U
Authority: CN
Inventors: 张昭; 黄旭; 王博涵; 赵云婷; 海洋
Original assignee: Csic Ocean Star Beijing Cultural Development Co ltd
Current assignee: Csic Ocean Star Beijing Cultural Development Co ltd
Priority date: 2019-12-31
Filing date: 2019-12-31
Publication date: 2020-09-22
Anticipated expiration: 2029-12-31

Abstract

The utility model belongs to the technical field of the technique of science popularization demonstration military assembly and specifically relates to a guided missile simulation emitter for submarine model is related to, including the launching tube of vertical setting, install guided missile model in the launching tube, connect the direction subassembly between guided missile model and launching tube and set up the drive assembly of guided missile model up-and-down motion in order to simulate the guided missile transmission below the launching tube. The utility model has the advantages that can be for the guided missile vertical launching's of teenagers children's science popularization and show submarine sight.

Description

Guided missile simulation launching device for submarine model

Technical Field

The utility model belongs to the technical field of the technique of science popularization demonstration military assembly and specifically relates to a guided missile simulation emitter for submarine model.

Background

At present, the scientific and technological development of military affairs is fast, and the international social relationship is increasingly complex, the science popularization education of national defense is particularly important. But military science popularization devices and demonstration equipment in China are always lacked, and the vertical launching display equipment of submarine missiles is blank.

Therefore, the utility model provides a set of easy operation, convenient and practical, audio-visual scheme to show the guided missile vertical launching sight of submarine.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a guided missile simulation emitter for submarine model, its advantage can be for the sight of the guided missile vertical launch of teenagers' science popularization and show submarine.

The above technical purpose of the present invention can be achieved by the following technical solutions: a missile simulation launching device for a submarine model comprises a vertically arranged launching barrel, a missile model arranged in the launching barrel, a guide assembly connected between the missile model and the launching barrel, and a driving assembly arranged below the launching barrel and used for driving the missile model to move up and down to simulate missile launching.

By adopting the technical scheme, the missile simulation launching device only comprises the launching barrel, the missile model, the guide assembly and the driving assembly, the whole structure is simple, and when the driving assembly is started, the missile model can be driven to move up and down along the guide assembly, so that missile launching is simulated, and the missile simulation launching device is suitable for the situation that the missile of teenagers and children is popularized and the submarine is vertically launched.

The utility model discloses can further set up to in a preferred example: the launching tube is cylindrical, the interior of the launching tube is hollow, and two ends of the launching tube are open;

the guiding assembly comprises at least three groups of T-shaped guide rails which are fixedly connected to the inner wall of the launching tube and extend along the axial direction of the launching tube and grooved wheels which are arranged on the outer wall of one end, far away from the warhead, of the missile model and correspond to the T-shaped guide rails one to one, the grooved wheels are supported on the T-shaped guide rails in a rolling mode, and the T-shaped guide rails are distributed in a circumferential equidistant mode by taking the missile model as the center.

By adopting the technical scheme, the grooved wheel is supported on the T-shaped guide rail through the groove on the peripheral surface of the grooved wheel in a rolling manner, and the grooved wheel is matched with the T-shaped guide rail for vertically guiding and horizontally limiting the missile model.

The utility model discloses can further set up to in a preferred example: the driving assembly comprises a box base fixedly connected to the bottom of the launching tube and communicated with the launching tube, a fixed pulley mounted on the inner wall of the launching tube close to the top end, and an electric winch mounted on the inner bottom wall of the box body, wherein one end of a rope of the electric winch bypasses the fixed pulley and is fixedly connected with the outer side wall of the missile model far away from one end of the bullet.

By adopting the technical scheme, when the missile is simulated to be launched, the electric winch is started to enable the winding drum to wind the rope, and in the winding process, the missile model moves upwards along the T-shaped guide rail through the grooved pulley under the pulling of the rope until the grooved pulley is contacted with the limiting block; and after the simulation is finished, starting the electric winch again to enable the winding drum to rotate reversely and release the rope until the missile model is reset.

The utility model discloses can further set up to in a preferred example: the winding drum of the electric winch is fixedly connected with three partition plates which divide the winding drum into four areas, each area is internally wound with ropes which are wound to the same direction, four groups of fixed pulleys are correspondingly installed on the inner wall of the launching drum close to the top end, and each rope is wound around the corresponding fixed pulley and fixedly connected with the outer side wall of one end, far away from the warhead, of the missile model.

By adopting the technical scheme, the stability of the missile model in the lifting process is ensured, and the rope and the fixed pulley are uniformly stressed.

The utility model discloses can further set up to in a preferred example: the inner wall of the launching barrel, which is close to one end of the box body base, is fixedly connected with a bearing plate for supporting the missile model, and the bearing plate is provided with a abdication notch for the rope to pass through.

By adopting the technical scheme, the bearing plate is arranged for supporting the missile model and sharing the stress of the rope.

The utility model discloses can further set up to in a preferred example: and an oil pressure buffer for buffering the missile model is arranged on the bearing plate.

By adopting the technical scheme, the oil pressure buffer is arranged for buffering the missile model, and hard collision between the missile model and the bearing plate during resetting is avoided.

The utility model discloses can further set up to in a preferred example: the one end that the launching tube kept away from the box base is articulated to have a apron.

Through adopting above-mentioned technical scheme, shelter from the top opening of launching tube to it is dustproof.

The utility model discloses can further set up to in a preferred example: and the top end of the T-shaped guide rail is connected with a limiting block through a bolt.

Through adopting above-mentioned technical scheme, the setting of stopper for spacing the sheave, prevent that it from deviating from on the T shape guide rail.

The utility model discloses can further set up to in a preferred example: and an observation window made of transparent materials is arranged on the side wall of the launch canister.

By adopting the technical scheme, teenagers and children can more visually see the launching condition in the launching tube.

To sum up, the utility model discloses a beneficial technological effect does:

1. the missile simulation launching device is only composed of four parts, namely a launching barrel, a missile model, a guide component and a driving component, the overall structure is simple, and when the driving component is started, the missile model can be driven to move up and down along the guide component, so that missile launching is simulated, and the missile simulation launching device is a scene for promoting science of teenagers and children and showing the vertical launching of a submarine missile;

2. the arrangement of a plurality of groups of ropes and fixed pulleys can ensure the stability of the missile model in the lifting process and ensure that the ropes and the fixed pulleys are uniformly stressed;

3. and the hydraulic buffer is arranged and used for buffering the missile model and avoiding rigid collision between the missile model and the supporting plate when the missile model is reset.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a sectional view showing the internal structure of the launch canister and the connection between the drive assembly and the missile model;

FIG. 3 is an enlarged partial schematic view of portion A of FIG. 2;

fig. 4 is a sectional view showing the connection of the rope to the missile model around the fixed sheave.

Reference numeral, 1, a launch canister; 11. a cover plate; 12. a support plate; 13. an observation window; 2. a missile model; 3. a guide assembly; 31. a T-shaped guide rail; 32. a grooved wheel; 33. a limiting block; 4. a drive assembly; 41. a base of the box body; 42. a fixed pulley; 43. an electric hoist; 44. a rope; 45. a reel; 46. a partition plate; 5. and a hydraulic shock absorber.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings.

Referring to fig. 1 and 2, for the utility model discloses a guided missile simulation emitter for submarine model, it is located submarine model's middle part, guided missile simulation emitter includes the launching tube 1 of vertical setting, install guided missile model 2 in launching tube 1, connect the direction subassembly 3 between guided missile model 2 and launching tube 1 and set up the drive assembly 4 that just is connected with guided missile model 2 in launching tube 1 below, drive assembly 4 can drive guided missile model 2 along direction subassembly 3 up-and-down motion, thereby the simulated missile transmission, for teenagers ' science popularization and show submarine's the perpendicular transmission of guided missile sight.

The launching tube 1 is cylindrical, the interior of the launching tube is hollow, and two ends of the launching tube are open. The top of the launching tube 1 is hinged with a cover plate 11 for dust prevention. The inner wall of the launching tube 1 close to the bottom is fixedly connected with a bearing plate 12 for supporting the missile model 2. The upper surface of the supporting plate 12 is provided with an oil pressure buffer 5, when the missile model 2 descends, the oil pressure buffer 5 can buffer the missile model 2, and hard collision between the missile model 2 and the supporting plate 12 is avoided.

In order to enable teenagers and children to more visually see the emission condition inside the emission tube 1, an observation window 13 made of a transparent material is arranged on the side wall of the emission tube 1, and the transparent material can be acrylic or toughened glass.

Referring to fig. 2 and 3, the guiding assembly 3 comprises at least three sets of T-shaped guide rails 31 fixed on the inner wall of the launching tube 1 through bolts and grooved wheels 32 installed on the outer wall of one end, far away from the warhead, of the missile model 2 and corresponding to the T-shaped guide rails 31 one by one, the T-shaped guide rails 31 extend along the axis direction of the launching tube 1, the grooved wheels 32 are supported on the T-shaped guide rails 31 in a rolling manner through grooves on the peripheral surface of the grooved wheels, the T-shaped guide rails 31 are distributed equidistantly around the missile model 2 as the center, and the arrangement mode is used for conducting vertical guiding and horizontal limiting on the missile model 2.

The top end of the T-shaped guide rail 31 is connected with a limiting block 33 through a bolt, and the limiting block is used for limiting the grooved wheel 32 and preventing the grooved wheel from being separated from the T-shaped guide rail 31.

Referring to fig. 2 and 4, the driving assembly 4 includes a box base 41 fixedly connected to the bottom of the launch canister 1 and communicated with the launch canister 1, a fixed pulley 42 mounted on the inner wall of the launch canister 1 near the top end, and an electric hoist 43 mounted on the inner bottom wall of the box, the fixed pulley 42 is located above the T-shaped guide rail 31, one end of a rope 44 of the electric hoist 43 bypasses the fixed pulley 42 and is fixedly connected to the outer side wall of the missile model 2 far from the warhead end, an abdicating notch for the rope 44 to pass through is formed in the support plate 12, and an electric control device of the electric hoist 43 is arranged outside the box base 41 so as to be operated by a worker.

When the simulated missile is launched, the electric winch 43 is started, the winding drum 45 winds the rope 44, and in the winding process, the missile model 2 moves upwards along the T-shaped guide rail 31 through the grooved pulley 32 under the pulling of the rope 44 until the grooved pulley 32 is contacted with the limiting block 33, and the missile model is stopped; after the simulation is finished, the electric winch 43 is started again, the winding drum 45 rotates reversely to release the rope until the missile model 2 contacts the oil buffer 5, and the machine is stopped.

In order to ensure the stability of the missile model 2 in the lifting process and enable the ropes 44 and the fixed pulleys 42 to be stressed uniformly, three partition plates 46 for dividing the winding drum 45 into four areas are fixedly connected to the winding drum 45 of the electric winch 43, the ropes 44 with the same winding direction are wound in each area, four groups of fixed pulleys 42 are correspondingly installed on the inner wall, close to the top end, of the launching drum 1, each rope 44 bypasses the corresponding fixed pulley 42 and is fixedly connected with the outer side wall, far away from the warhead, of the missile model 2, and when the electric winch 43 is started, the winding drum 45 can drive the four ropes 44 to be retracted simultaneously.

The embodiment of this specific implementation mode is the preferred embodiment of the present invention, not limit according to this the utility model discloses a protection scope, so: all equivalent changes made according to the structure, shape and principle of the utility model are covered within the protection scope of the utility model.

Claims

1. A missile simulation launching device for a submarine model is characterized in that: the missile launching device comprises a vertically arranged launching tube (1), a missile model (2) installed in the launching tube (1), a guide assembly (3) connected between the missile model (2) and the launching tube (1), and a driving assembly (4) arranged below the launching tube (1) and used for driving the missile model (2) to move up and down to simulate missile launching.

2. The missile simulation launcher for the submarine model according to claim 1, wherein: the launching tube (1) is cylindrical, the interior of the launching tube is hollow, and two ends of the launching tube are open;

the guiding component (3) comprises at least three groups of T-shaped guide rails (31) which are fixedly connected to the inner wall of the launching tube (1) and extend along the axial direction of the launching tube (1) and grooved wheels (32) which are arranged on the outer wall of one end, far away from the warhead, of the missile model (2) and correspond to the T-shaped guide rails (31) one by one, wherein the grooved wheels (32) are supported on the T-shaped guide rails (31) in a rolling manner, and the missile model (2) is used as the center between the T-shaped guide rails (31) to be distributed at equal intervals in the circumference.

3. The missile simulation launcher for the submarine model according to claim 1, wherein: the driving assembly (4) comprises a box base (41) fixedly connected to the bottom of the launching tube (1) and communicated with the launching tube (1), a fixed pulley (42) mounted on the inner wall, close to the top end, of the launching tube (1) and an electric winch (43) mounted on the inner wall of the box inner wall, one end of a rope (44) of the electric winch (43) bypasses the fixed pulley (42) and is fixedly connected with the outer side wall, far away from one end of the bullet head, of the missile model (2).

4. The missile simulation launcher for the submarine model according to claim 3, wherein: the solid connection has three partitions (46) of separating into four regions with reel (45) on reel (45) of electric hoist (43), and it winds to the same rope (44) all to twine in every region, and corresponding on the inner wall that launch canister (1) is close to the top installs four sets of fixed pulleys (42), and every rope (44) all walks around corresponding fixed pulley (42) and keep away from the lateral wall rigid coupling of warhead one end with missile model (2).

5. The missile simulation launcher for the submarine model according to claim 3, wherein: the inner wall of the launching tube (1) close to one end of the box body base (41) is fixedly connected with a bearing plate (12) for supporting the missile model (2), and the bearing plate (12) is provided with a yielding notch for the rope (44) to pass through.

6. The missile simulation launcher for the submarine model according to claim 5, wherein: and an oil pressure buffer (5) for buffering the missile model (2) is arranged on the bearing plate (12).

7. The missile simulation launcher for the submarine model according to claim 1, wherein: one end of the launching tube (1) far away from the box body base (41) is hinged with a cover plate (11).

8. The missile simulation launcher for the submarine model according to claim 2, wherein: the top end of the T-shaped guide rail (31) is connected with a limiting block (33) through a bolt.

9. The missile simulation launcher for the submarine model according to claim 1, wherein: and an observation window (13) made of transparent materials is arranged on the side wall of the launching tube (1).