KR101923995B1 - Apparatus for detention of guided missile - Google Patents

Abstract

The present invention relates to a device for restricting a guided car charged in a launching tube, the guiding carbon restraining device being installed on an inner wall of a launching tube and being contactable with the guided car charged in the launching tube, A navel separating part including a bracket for fixing the navel connecting part and a supporting part for supporting the bracket and inclined at a predetermined angle; At least one pin capable of restraining the movement of the guided car in the launch tube is assembled and installed before the guided car is fired, And a restricting portion formed in a shape capable of supporting the at least one pin, It characterized in that it comprises a housing formed.

Description

[0001] APPARATUS FOR DETENTION OF GUIDED MISSILE [0002]

The present invention relates to a device for restraining missile shot in a launching tube.

 Generally, the guided car charged in the tube maintains an electrical connection with the umbrella connector that supplies power to the guided car. And when the missile is fired, the umbilical separating device separates the umbilicus connector.

The guided vehicle may further include a restraining device for restraining the guided car in order to prevent the guided car from being abnormally detached from the launching tube in the event of accidental ignition or firing of the guided car before the guided car is fired.

A configuration for separating the umbrella connecting unit connected to the guided car from the guided car charged in the launching tube and the restraining device for restricting the guided car to prevent the guided car from escaping are provided as a separate device between the guided car and the launching tube . Generally, since these devices are installed and operated separately, there arises a problem that it is difficult to install and operate the devices when the placement of the components of the guided vehicle is narrow, and there is a problem in designing the guided missile and the launch pipe.

SUMMARY OF THE INVENTION It is an object of the present invention to solve the above-mentioned problems and other problems, and it is an object of the present invention to make it easier and easier to install and operate the restraint device of the umbrella separating device and the guided- And to provide a device for performing the above-described operations.

Further, according to the present invention, it is possible to separate the umbilical connector from the guided missile by using only one device, by making it possible to separate the umbilicus connector from the guided car when the guided car is fired In addition, it is an object of the present invention to provide an apparatus for restricting abnormal departure of the missile.

According to another aspect of the present invention, there is provided a method of controlling a driving force according to the present invention, the method comprising the steps of: providing a bracket that fixes a umbrella connector for supplying power to the guide car, and a support portion having a beveled surface formed to be inclined at a predetermined angle, And an engaging portion engaging with the umbrella separating portion so that the umbrella separating portion can perform sliding movement along an engaging groove formed at an angle equal to an inclination formed on the support portion of the umbilical separating portion; At least one pin capable of restraining the movement of the guided carburetor is assembled and installed in the housing and a restricting portion formed in a shape capable of supporting the at least one pin is formed, Wherein the projecting portion includes a projecting portion projecting outwardly, The umbilical separation portion inserted into the engaging groove, so as to perform a sliding motion is characterized in that the coupling portion coupled to the umbilical separation unit.

In one embodiment, the inclination formed on the engaging portion and the supporting portion is formed such that a distance between the guide bush and the engaging groove is increased as the portion toward the front side of the guided char is distanced, Wherein the distance between the bracket and the guide poles is set to be longer than a distance between the brackets and the guide poles, and when the guide poles are moved forward when the guide poles are fired, And the umbrella connector fixed to the bracket is formed to be separated.

In one embodiment, the bracket of the umbilical separating portion is formed so as to be always in parallel with the guided char when the navel separating portion slides along the engaging groove of the engaging portion.

In one embodiment of the present invention, the engaging portion may be provided at a front portion of the restraining portion on the basis of a direction in which the guide carries forward movement, so that the releasing of the guide car can be released earlier than the separation of the umbilicus connector, Is formed.

In one embodiment, the restraining portion may include a bullet-restraining pin for restraining longitudinal movement of the guided car, releasing the restraint of the guided car before the guided car is fired in accordance with mechanical interlocking with the igniter and the guided car, Wherein upper ends of the projected restraint pin and the restraint pin project upward through the holes formed in the upper surface of the restraint part in contact with the guide cylinder, As shown in FIG.

In one embodiment, the re-restraining pin restrains the lateral movement of the guide car through a screw connection with the guide car, and when the guide car is steadily fired, the upper end restricting the guide car is broken, And is released to be released.

In one embodiment, the housing is characterized in that the engaging portion and the restricting portion are integrally formed.

The effect of the touring cargo restraint apparatus according to the embodiment of the present invention will be described as follows.

According to at least one of the embodiments of the present invention, the present invention allows the arresting device of the missile to separate the umbrella connector connected to the missile when the missile is fired as well as to arrange the missile, There is an effect that there is no need to further install a device for the umbilical separation function.

Further, the present invention can perform both the restraint function and the umbilical separation function of the missile with only one device, thereby reducing the number of devices installed between the missile and the launch tube, and reducing the complexity of design and operation .

FIG. 1 is an exemplary view showing an example in which a guide car capturing apparatus according to an embodiment of the present invention is installed between a guide gun loaded in a launch tube and the launch tube.
FIG. 2 is an exemplary view showing an example of each constituent element constituting the touring cargo restraint apparatus according to the embodiment of the present invention.
FIG. 3 is an exemplary view showing an example of a guide charger for restraining a guide bug, which can perform both a restraining function and a belly button separating function of the components shown in FIG. 2.

It is noted that the technical terms used herein are used only to describe specific embodiments and are not intended to limit the invention. Also, the singular forms "as used herein include plural referents unless the context clearly dictates otherwise. In this specification, "comprises" Or "include." Should not be construed to encompass the various components or steps described in the specification, and some of the components or portions may not be included, or may include additional components or steps And the like.

Further, in the description of the technology disclosed in this specification, a detailed description of related arts will be omitted if it is determined that the gist of the technology disclosed in this specification may be obscured.

Hereinafter, embodiments disclosed in this specification will be described in detail with reference to the accompanying drawings.

First, FIG. 1 is an exemplary view showing an example in which the guide car capturing apparatus 100 according to the embodiment of the present invention is installed between the guide cylinder charged in the launch tube and the launch tube.

1, the guide restraining apparatus 100 according to the embodiment of the present invention is installed on the inner wall of the launching pipe 300 and connected to the guide poles 200 loaded in the launching pipe 300. As shown in FIG. 1, .

The guide restraining apparatus 100 according to the embodiment of the present invention may be integrally formed to simultaneously perform the function of separating the guide bush 200 from the umbrella and restricting the guide ball. When the guide car 200 is mounted in the launch pipe 300, the guide car restraint device 100 maintains the umbrella connecting device connected to the guide car 200 to supply power to the guide car 200, When the missile 200 is moved forward due to firing when the missile 200 is fired, the navel connector can be automatically separated from the missile 200 according to the movement of the missile 200.

The guide restraining device 100 restrains the longitudinal movement and the abnormal shots of the guide car 200 in the launch pipe 300 and mechanically interlocks with the guide car 200, So that the restraint of the missile 200 can be released before launching. In addition, the guided-car restraint apparatus 100 may also perform a guided-cargo-restraining function for the purpose of repairing the guided car due to the misfire of the propelling engine when the guided car 200 is launched normally. Techniques required for the present invention include designing / manufacturing technology of navel connecting bases with electrical connection to high-reliability charcoal, mechanism releasing performance, and designing / manufacturing technology of bullet-proof restraining device from bullet loading and vibration and impact.

FIG. 2 is an exemplary view showing an example of each constituent element constituting the guide charger 100 according to the embodiment of the present invention.

Referring to FIG. 2, the guide car capturing apparatus 100 according to an embodiment of the present invention includes a guide pin 200 for supplying power to the guide car 200 when the guide car 200 is loaded into the guide pipe 300, A umbrella separating part 130 connected to the guide cylinder 200 and serving to separate the guide cylinder 200 from the umbrella connector during the launch of the guide cylinder 200, A housing 150 that includes a restraining portion 110 that can be assembled with at least one pin used to restrain the structure 200 and maintains structural strength and provides an interface that can be assembled with the launching tube 300, As shown in FIG.

The navel separating part 130 may include a bracket 132 having a groove on which the umbilical connector can be mounted and a support part 131 protruding from the lower end of the bracket 132. The supporting portion 131 may be formed as a flat structure protruding downward from both side edges of the bracket 132. Herein, the 'downward' direction refers to the direction of the launch tube 300 when the touring car capturing apparatus 100 according to the embodiment of the present invention is installed between the guide cylinder 200 and the launch tube 300, May refer to the direction of the guide poles 200. In the following description, the 'forward' direction refers to a direction in which the guide car 200 is moved forward when the guide car 200 loaded in the launch pipe 300 is fired, the 'rear direction' Quot; direction "

2, the supporting portions 131 may be protrusions protruding downward from both side edges of the bracket 132, respectively. Also, the support portions 131 may be formed to have different lengths from the ends protruding from one end and protruding from the other end, and may be formed to be inclined at a predetermined angle. In addition, the predetermined angle may be formed such that the distance from the guide cylinder 200 to the front part of the guide cylinder 200 is increased.

2, each of the support portions 131 has a length protruding from each end of each of the brackets 132 at the front portion, a length of the protruding portion from each end of the brackets 132 at the rear portion, As shown in Fig. 2, a right triangle having a right-angled portion facing forward can be formed. This is to ensure that the bracket 132 is always parallel to the guide cylinder 200 when the bracket 132 slides along an inclined surface formed on each support portion 131.

Meanwhile, the front and rear portions of the housing 150 may be formed differently. The navel separating part 130 may be coupled to the front portion of the housing 150. 2, the front portion of the housing 150 has an angle of an inclined surface formed by each of the supporting portions 131 so that each supporting portion 131 formed to be inclined at the predetermined angle can be engaged, As shown in FIG. In addition, the inclined housing 150 may be formed with a coupling groove 121 formed to allow the supporting portions 131 to be coupled therewith. Hereinafter, a portion of the front portion of the housing 150 where the coupling groove 121 is formed and which is inclined at the predetermined angle will be referred to as a coupling portion 120.
On the other hand, protrusions 131a may be formed on the ends of the respective support parts 131 as shown in the following figure. The protrusions 131a may be formed to protrude outwardly from the obliquely formed oblique portions of the support portions 131 in the shape of a right triangle. The protrusions 131a may be inserted into the coupling grooves 121 of the housing 150 to engage the supporting portions 131 of the umbilical separator 130 with the coupling grooves 121. Therefore, the umbilical separating part 130 can be coupled to the engaging part 120. The protrusions 131a can be guided and slid by the coupling grooves 121 so that the umbilical separating part 130 can perform a sliding motion along an inclined surface formed in front of the housing 150 .
[Drawing]

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A restraining part 110 is formed behind the housing 150 of the touring car restraint apparatus 100 according to an embodiment of the present invention so as to restrain the movement of the guided car 200 prior to launching the guided car 200 . Here, the engaging portion 120 may be formed at a front portion of the restricting portion 110 with respect to a direction in which the guide cylinder 200 advances when the guide cylinder 200 is fired.

The coupling part 120 is formed at the front part of the restraining part 110 so that the guided car 200 whose restraint is released from the restraining part 110 starts to move forward as the guided car 200 is fired The navel separating part 130 slides along the inclination so that the umbrella connecting part fixed to the bracket 132 can be separated from the guide car 200. [ That is, to release the restraint of the guide gun 200 rather than the separation of the umbilicus connector.

Meanwhile, the touring car restraint apparatus 100 according to the embodiment of the present invention may use a bullet pin 111 and / or a restraint pin 112 to restrain the guided car 200. The restraint pin 110 and / or the restraint pin 112 are assembled and installed in the restraining part 110, and the restraining part 110 is fixed to the restraint pin 111 and / (Not shown).

The bullet restraint pin 111 and / or the restraint pin 112 (not shown) provided on the restraining part 110 are formed on one surface of the restraining part 110 adjacent to the top surface of the restraining part 110, At least one hole through which the upper end of the protrusion can protrude can be formed. A part of the upper ends of the bullet restraint pin 111 and / or the restraint pin 112 protruding through the holes formed in the upper surface of the restraining part 110 performs the function of restraining and releasing the guided air 200 .

That is, the upper ends of the bullet-restraining pins 111 and / or the restraining pins 112 protruding from the restraining part 110 are brought into contact with the guiding curtains 200 so that the longitudinal or lateral movement of the guided- You can arrest them. That is, when the bullet restraint pin 111 and / or the restraint pin 112 are assembled to the restraining portion 110, the assembly prevents the deviation of the guided air 200 and releases the restraint upon launching the guided- It is possible to perform a restraining function.

Meanwhile, the guide cylinder 200 in the launch tube 300 is restrained by the protruding upper end of the bullet restraining pin 111, so that the deviation can be prevented due to the longitudinal movement and the abnormal emission. The bullet restraining pin 111 can release the restraint of the guided vehicle 200 by mechanically interlocking with the igniter and the guiding charger 200 so that the constraint can be released before the guiding charger 200 is fired. The restraint pin 112 can restrain the guided car 200 in the lateral direction through screwing with the guided car 200 in the launch tube 300. When the guided car 200 is fired at a normal time, The restraint of the guided car 200 can be released.

Meanwhile, the bullet restraint pin 111 and the restraint pin 112 bear an external force for restraining the guided car 200 when the guided car 200 is ignited abnormally and the restraint pin 112 May be formed of a high strength material so as to support the load by the front end.

FIG. 3 is an exemplary view showing an example of a guide charger for restraining the guide rails, which can perform both the restraining function and the belly button separating function of the components shown in FIG.

When the guide missile 200 is loaded into the launch tube 300, the guide catcher 100 according to the embodiment of the present invention in which the elliptical separator 130 is coupled can be mounted. The umbilical connecting unit connected to the guide cylinder 200 may be coupled to the bracket of the umbilical separating unit 130 and may be fixed to the inside of the cylinder tube 300 . The re-restraining pin 112 is fastened to fix the guide cylinder 200 inside the launch tube 300.

When the guide fire signal is received in this state, the bullet restraining pin 111 can release the restraint of the guide gun 200. The upper end of the re-restraining pin 112 may be broken, and the restraint of the guided car 200 may be released.

When the missile 200 is launched, the missile 200 can start moving forward along the shooter 300. 3, the umbrella separating part 130, which fixes the umbrella connector, moves along the inclined surface of the engaging groove 121 in accordance with forward movement of the guide cylinder 200. As shown in FIG.

3, the navel separating part 130 slides along the inclined surface of the engaging groove 121, and the distance from the guide cylinder 200 can be increased. As the distance between the guide cylinder 200 and the navel separating part 130 is increased, the navel connector fixed to the bracket 132 of the navel separating part 130 can be separated from the guide cylinder 200.

Accordingly, the touring car capturing apparatus 100 according to the embodiment of the present invention not only performs the function of restricting the touring car 200, but also carries out the launching of the touring car 200 according to the shape of the touring carcass capturing device 100 The guide cylinder 200 of the guide cylinder 200 is automatically separated when the guide cylinder 200 moves forward, so that a separate device for separating the guide cylinder 200 can be dispensed with.

While the invention has been shown and described with reference to certain preferred embodiments thereof, it will be understood by those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. That is, those skilled in the art will appreciate that various modifications and changes may be made without departing from the spirit and scope of the present invention. Therefore, the embodiments disclosed in the present invention are not intended to limit the scope of the present invention but to limit the scope of the technical idea of the present invention. The scope of protection of the present invention should be construed according to the following claims, and all technical ideas within the scope of equivalents should be construed as falling within the scope of the present invention.

100: a guide railing restraining device 110: a restraining part
111: bullet constrained pin 112: redefined pin
120: engaging portion 121: engaging groove
130: navel separating part 131: supporting part
132: bracket 150: housing
200: missile 300: launcher

Claims (7)

A guide cap restraint device installed on an inner wall of a launching tube, the guide cap restricting device being capable of contacting a guide cylinder loaded in the launch tube,
A umbrella separating part including a bracket to which a umbrella connector for supplying power to the guide car is fixed and a supporting part supporting the bracket and having a beveled surface inclined at a predetermined angle; And
An engaging portion that engages with the umbilical separating portion to enable the umbilicus separating portion to perform sliding movement along an engaging groove formed at an angle equal to an inclination formed on the support portion of the umbilical separating portion,
At least one pin capable of restraining the movement of the guide car in the launch tube is assembled and installed before the guide car is fired and a restraining part formed in a shape capable of supporting the at least one pin is formed In addition,
The support portion
And a protrusion protruding outwardly on the oblique surface,
The projection
And the umbrella separating portion is inserted into the engaging groove to engage the engaging portion with the umbilical separating portion so that the umbilicus separating portion performs sliding movement along the inclination of the engaging groove. 2. The apparatus according to claim 1, wherein the engaging portion and the inclination formed on the supporting portion
Wherein the distance between the guide bush and the guide groove is set to be longer than the distance between the guide bush and the guide groove,
Wherein the umbrella coupling unit fixed to the bracket is separated according to a distance between the bracket and the guide ball which is extended by the sliding motion of the umbrella separating unit when the guide car moves forward when the guide car is fired. Guided coal restraint system. The apparatus according to claim 1,
Wherein the bracket of the umbrella separating portion is formed so as to maintain a state in which the bracket of the umbrella separating portion is always in parallel with the guided car when the navel separating portion slides along the engaging groove of the engaging portion. The connector according to claim 1,
Wherein the guide charger is formed at a front portion of the restricting portion with respect to a direction in which the guide car is moved forward so that the restraint of the guide car can be released earlier than the separation of the umbrella connector at the time of launching the guide car. The apparatus according to claim 1,
A gun-restraining pin for restraining longitudinal movement of the guided car and releasing restraint of the guided car before the guided car is fired in accordance with the mechanical interlocking with the igniter and the guided car, and a material for restraining the lateral movement of the guided car in the launch tube Wherein the upper ends of the restraining pins are protruded through holes formed in the upper surface of the restraining part in contact with the guide car, and the upper ends of the projected restraining pin and the restraining pin are formed so as to restrain the guide car. . 6. The apparatus of claim 5, wherein the re-
Wherein the guide shaft is configured to restrain lateral movement of the guide car through a screw connection with the guide car, and to break the upper end of the guide car to restrict the guide car when the guide car is steadily fired. The connector according to claim 1,
Wherein the engaging portion and the restricting portion are integrally formed.

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