CN217767676U

CN217767676U - Ship model missile launcher

Info

Publication number: CN217767676U
Application number: CN202221512944.3U
Authority: CN
Inventors: 董科敏
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-06-16
Filing date: 2022-06-16
Publication date: 2022-11-08
Anticipated expiration: 2032-06-16

Abstract

The utility model relates to a ship model missile launcher, which comprises a launching well, an ignition head mounting assembly and a lead connecting plate assembly; the upper end of the launching well is fixedly connected with an upper fixing plate, the lower end of the launching well is fixedly connected with a lower fixing plate, and the upper end of the upper fixing plate is fixedly connected with a mounting plate; the ignition head mounting assembly comprises a support fixing plate, supports which are arranged transversely and vertically are fixedly mounted on the support fixing plate, an ignition head is mounted at the upper end of each support, and the lower end of each ignition head is connected with a lead which extends out of the lower end of each support; the bracket fixing plate is connected with the lower fixing plate through a positioning pin, and a positioning pin hole matched with the positioning pin is formed in the lower fixing plate; the utility model discloses use the launching shaft subassembly as the platform, carried on the first installation component of ignition, lead wire connecting plate subassembly has simulated the guided missile launching scene of real warship, makes the degree of reduction of naval vessel model have had obvious improvement.

Description

Ship model missile launcher

Technical Field

The utility model relates to a emitter technical field especially relates to a naval vessel model guided missile emitter.

Background

At present, in the aspect of missile launching scenes, because the missile launching scene is limited in multiple aspects, only the appearance structure of a ship model is usually shown on the ship model, and the process of simulating missile launching is difficult to show, so that the reduction degree of the ship model has defects.

SUMMERY OF THE UTILITY MODEL

In order to solve the problems, the utility model provides a ship model missile launcher, which comprises a launching well, an ignition head mounting assembly and a lead connecting plate assembly;

the upper end of the launching well is fixedly connected with an upper fixing plate, the lower end of the launching well is fixedly connected with a lower fixing plate, and the upper end of the upper fixing plate is fixedly connected with a mounting plate;

the ignition head mounting assembly comprises a support fixing plate, supports which are arranged transversely and vertically are fixedly mounted on the support fixing plate, an ignition head is mounted at the upper end of each support, and the lower end of each ignition head is connected with a lead which extends out of the lower end of each support; the bracket fixing plate is connected with the lower fixing plate through a positioning pin, and a positioning pin hole matched with the positioning pin is formed in the lower fixing plate;

the lead connecting plate assembly comprises an insulating substrate, a plurality of wiring copper columns are mounted on the insulating substrate, and the lead penetrates through the wiring copper columns and is then bonded and fixed in a pouring sealant mode; the bracket fixing plate is fixedly connected with the insulating substrate.

Furthermore, a steering engine rotating arm hole is formed in the lower fixing plate.

Furthermore, the middle of the bracket is communicated with the inner cavity of the bracket.

Furthermore, the wiring copper column is used for threading a lead for a structure with a middle part communicated.

Further, the lead is a copper wire.

Further, the ignition head is an electronic ignition head, and the model of the ignition head is WS-FT.

The parameters of the electronic ignition head are as follows:

the model is as follows: WS-FT

Bridge wire resistance: 1.2-1.5 omega

Safe current: 0.18A/5min

Full ignition current: 0.45A/100ms

Rated ignition current: 1.0A/1ms, 0.8A/2ms

Detection or control of the current: less than or equal to 50ms

Vibrating: 2h

Temperature range: minus 20 ℃ to plus 40 ℃.

The utility model discloses owing to adopt above technical scheme, make it compare with prior art, have following beneficial effect:

when the rocket launcher is used, a rocket is inserted into the upper end of the launching well, namely a rocket is installed at the upper end of each support, the bottom of the rocket is circular and is connected with the top end of each support in an inserting mode, then the ignition process of the ignition head is executed through external equipment, the ignition head guides the rocket to ignite and launch the rocket, the processes are independently repeated for 2-5 times respectively, a plurality of rockets can be launched, simulation experiments are conducted, and the launching process of the rocket can be visually seen. A launch process for simulating naval vessel model, the utility model discloses use the launching shaft subassembly as the platform, carried on the first installation component of ignition, lead wire connecting plate subassembly has simulated the guided missile launching scene of real warship, makes the degree of reduction of naval vessel model have had obvious improvement.

Drawings

Fig. 1 is a schematic view of the structure of the launching well installed in the present invention;

fig. 2 is a schematic side view of the launching well mounting structure of the present invention;

fig. 3 is a schematic view of the installation bottom structure of the launching well of the present invention;

fig. 4 is a schematic structural view of the ignition head mounting assembly of the present invention;

fig. 5 is a schematic structural view of the lead connecting plate assembly of the present invention;

fig. 6 is a schematic view of the overall structure of the present invention.

In the figure: the device comprises a launching well 1, an upper fixing plate 2, a lower fixing plate 3, a mounting plate 4, a steering engine rotary arm hole 5, a support fixing plate 6, a support 7, an ignition head 8, a lead 9, a positioning pin 10, an insulating substrate 11, a wiring copper column 12 and glue 13.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention. In the drawings, the size and relative sizes of certain features may be exaggerated for clarity.

In the description of the present invention, unless expressly stated or limited otherwise, the terms "connected" and "connected" are to be construed broadly, e.g., as meaning a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; the term "connected" may refer to a direct connection, an indirect connection through an intermediate medium, a connection between two elements, or an interaction between two elements, and those skilled in the art can understand the specific meaning of the terms in the present invention in specific situations.

In addition, in the description of the present invention, the terms "first", "second", and "third" are used only for distinguishing between the descriptions.

As shown in the attached drawings 1-6 of the specification, the utility model provides a ship model missile launcher, which comprises a launching well 1, an ignition head mounting assembly and a lead connecting plate assembly;

the upper end of the launching well 1 is fixedly connected with an upper fixing plate 2, the lower end of the launching well 1 is fixedly connected with a lower fixing plate 3, and the upper end of the upper fixing plate 2 is fixedly connected with a mounting plate 4; and the upper fixing plate 2, the lower fixing plate 3 and the mounting plate 4 are provided with through holes matched with the launching well 1, and the through holes are used for mounting the fire head 8 and the rocket.

The ignition head mounting assembly comprises a support fixing plate 6, supports 7 which are transversely and vertically arranged are fixedly mounted on the support fixing plate 6, an ignition head 8 is mounted at the upper end of each support 7, the lower end of each ignition head 8 is connected with a lead 9, and the lead 9 extends out of the lower end of each support 7; the bracket fixing plate 6 is connected with the lower fixing plate 3 through a positioning pin 10, and a positioning pin hole matched with the positioning pin 10 is formed in the lower fixing plate 3;

the lead connecting plate assembly comprises an insulating substrate 11, a plurality of wiring copper columns 12 are mounted on the insulating substrate 11, and the lead 9 penetrates through the wiring copper columns 12 and then is bonded and fixed in a pouring sealant 13 mode; the bracket fixing plate 6 is fixedly connected with the insulating substrate 11, and the glue 13 is epoxy resin and has good insulativity and plasticity.

Furthermore, a steering engine rotating arm hole 5 is formed in the lower fixing plate 3. The steering engine rotary arm hole 5 is used for being connected with external equipment and mainly realizes a preformed hole for installing a motor and a connecting rod structure to add a protective structure to the device.

Furthermore, the middle of the support 7 is a through structure, and the middle through structure is a circular hole which is mainly circular and convenient to process.

Furthermore, the wiring copper columns 12 are of a structure with a through middle and are used for penetrating the lead wires 9, the wiring copper columns 12 are insulated and not connected with each other, and each lead wire 9 penetrates through the wiring copper columns 12 to control the ignition head 8 in each support 7, so that the rocket on each support 7 can be controlled independently.

Further, the lead 9 is a copper wire having good conductivity.

Further, the ignition head 8 is an electronic ignition head with the model of WS-FT.

The embodiment is as follows: the rocket is inserted into the upper end of the launching well 1, namely, one rocket is installed at the upper end of each support 7, the bottom of the rocket is circular and is only required to be inserted into the top end of each support 7, then the ignition head 8 is used for executing the ignition process of the ignition head 8 through external equipment, the ignition head 8 guides the rocket to ignite and launch, the processes are independently repeated for 2-5 times respectively, a plurality of rockets can be launched, a simulation experiment is carried out, and the launching process of the rocket can be visually seen. The utility model is used for simulate the process of launching of naval vessel model, the utility model discloses use the launching shaft subassembly as the platform, carried on the first installation component of ignition, the guided wire connecting plate subassembly has simulated the guided missile launching scene of real warship, makes the reduction degree of naval vessel model have had obvious improvement.

It will be appreciated by those skilled in the art that the invention can be embodied in many other specific forms without departing from the spirit or scope of the invention. Although the embodiments of the present invention have been described, it is to be understood that the present invention should not be limited to such embodiments, and that changes and modifications can be made by one skilled in the art within the spirit and scope of the present invention as defined by the appended claims.

Claims

1. A ship model missile launcher is characterized by comprising a launching well (1), an ignition head mounting assembly and a lead connecting plate assembly;

the upper end of the launching well (1) is fixedly connected with an upper fixing plate (2), the lower end of the launching well (1) is fixedly connected with a lower fixing plate (3), and the upper end of the upper fixing plate (2) is fixedly connected with a mounting plate (4);

the ignition head mounting assembly comprises a support fixing plate (6), supports (7) which are transversely and vertically arranged are fixedly mounted on the support fixing plate (6), an ignition head (8) is mounted at the upper end of each support (7), the lower end of each ignition head (8) is connected with a lead (9), and the lead (9) extends out of the lower end of each support (7); the bracket fixing plate (6) is connected with the lower fixing plate (3) through a positioning pin (10), and a positioning pin hole matched with the positioning pin (10) is formed in the lower fixing plate (3);

the lead connecting plate assembly comprises an insulating substrate (11), a plurality of wiring copper columns (12) are mounted on the insulating substrate (11), and the lead (9) penetrates through the wiring copper columns (12) and then is bonded and fixed in a pouring sealant (13) mode; the bracket fixing plate (6) is fixedly connected with the insulating substrate (11).

2. The ship model missile launcher of claim 1, wherein the lower fixing plate (3) is provided with a steering engine rotating arm hole (5).

3. The ship model missile launcher of claim 1, wherein the support (7) is a through-center structure.

4. The ship model missile launcher of claim 1, wherein the wiring copper cylinder (12) is a through-center structure for threading a wire (9).

5. The ship model missile launching device of claim 1, wherein the lead (9) is a copper wire.

6. The ship model missile launcher of claim 1, wherein the firing head (8) is an electronic firing head of type WS-FT.