KR102135722B1 - Pallet structure for guided missile - Google Patents

Abstract

The present invention includes a base member, a guided grenade support member spaced apart on the base member, and a guided grenade positioned on the top, a guided grenade clamping part positioned on the guided grenade support member to clamp guided grenade, the base member and the guided grenade support member It is spaced apart therebetween and is filled with gas therein, and includes a plurality of gas spring parts elastically supporting the guide missile support member, located at the base member or the guide missile support member, and including a gas supply part for injecting gas into the gas spring part By absorbing shock when transporting guided missiles, it is possible to prevent damage to electronic equipment, enabling accurate hitting of targets during the operation of guided missiles, and ensuring the quality stability and operational stability of guided missiles, enabling stable operation of guided missiles. , Prevents explosion of propulsion engines and greatly improves safety when carrying guided missiles.

Description

Carrier structure for guided missiles {PALLET STRUCTURE FOR GUIDED MISSILE}

The present invention relates to a carrier structure for a guided missile, and to a carrier structure for a guided missile capable of safely transporting a guided missile in which electronic equipment is embedded.

In general, the guided ammunition is equipped with an inertial measuring instrument such as a gyro, which is an electronic device for guiding the shot to a designated target.

In addition, the missile includes a solid propulsion engine that generates energy through a chemical reaction between an oxidant and a fuel.

Solid propulsion engines include propellant grains, propellant grains are susceptible to impact, and each propellant grain confirms impact sensitivity by measuring sensitivity through an impact sensitivity test.

For the maintenance or use of guided munitions, the packaging box used for transportation between troops or companies is made of wood or iron, and only serves to protect damage from exposure from the outside.

The conventional packaging box for transportation was manufactured to be very vulnerable to shock or vibration, and the wooden box was disposed of as a single use and economically inefficient.

That is, the guided munitions had a risk of an accident occurring when the propellant grains contained in the solid propulsion engine were transported by impact.

In addition, the guided munition has built-in electronic equipment for guiding the shot to a designated target, that is, a gyroscope and other built-in inertial meters, and there is a risk of damage to the electronic equipment due to the impact generated during transportation.

0001) Korean Patent Registration No.1592292'Ammunition Transfer Device and Its Operation Method' (2016.02.01.Registration)

An object of the present invention is to provide a carrier structure for a guided missile capable of preventing damage to electronic equipment by absorbing a shock when carrying the guided missile.

Another object of the present invention is to provide a carrier structure for a guided missile that absorbs a shock when the guided missile is transported, prevents an explosion of the propulsion engine by shock and vibration, and can safely transport the guided missile.

In order to achieve the above object of the present invention, an embodiment of a carrier structure for a guided munition according to the present invention includes a base member, a guided grenade support member spaced apart on the base member and a guided grenade located on the top, the guided grenade support member A guided gas clamping portion positioned on the clamping guided missile, and spaced apart between the base member and the guided support member, a plurality of gas springs filled with gas therein to elastically support the guided support member, the base It is characterized in that it comprises a gas supply portion for injecting gas into the gas spring portion, which is located on the member or the guide grenade support member.

In the present invention, between the base member and the guide grenade support member may be a vertical movement guide portion for limiting the horizontal movement of the guide grenade support member.

In the present invention, the moving guide part includes a first rail member protruding to the upper portion of the base member and a second rail member movably coupled to the first rail member, which is positioned to protrude below the guide grenade support member. can do.

In the present invention, the gas supply part connects a gas tank for storing gas, a gas injection hose member for connecting the gas tank and the gas spring part to inject gas into the gas spring part, and a flow path of the gas injection hose member. It may include a gas injection control unit for controlling the gas injection, including a control valve to open and close.

In the present invention, the gas supply unit further includes a plurality of distance displacement sensor units for measuring a distance change between the base member and the guided bullet support member at the position of each gas spring unit, and the gas injection control unit is measured by the distance displacement sensor unit. The gas spring is automatically injected into the gas spring at a position where the distance between the base member and the guide grenade support member is reduced by receiving the displacement of the gap between the base member and the guide grenade support member at the position of each gas spring part. The support member can be kept horizontal.

In the present invention, the guide munition clamping part may include a clamping tube body connected to the gas supply part and receiving gas from the gas supply part and maintained at a predetermined pressure.

In the present invention, the guide grenade clamping portion is mounted on the guide grenade support member and includes a first clamping portion surrounding a portion of the guide grenade and a second clamping portion surrounding at least a portion of the remaining portion of the guide grenade, wherein the first clamping portion supports the guide grenade A lower plate member fixed on the member, a first clamping tube body fixed on the lower plate member, filled with gas therein, and absorbing the shock delivered to the guided grenade, located on top of the first clamping tube body, to the top It includes the first clamping bracket member in which the first guided grenade inserting portion into which a portion of the guided grenade is inserted is located, and the second clamping member is rotatably connected to one side of the first clamping bracket member with a clamping hinge portion and is lowered. A second clamping bracket member in which the second guided grenade inserting portion in which at least a portion of the remaining portion of the guided grenade is opened and inserted is positioned.

In the present invention, the first clamping tube body includes a first pressure sensor capable of measuring internal pressure, the first pressure sensor transmits the measured pressure to the gas supply unit, and the gas supply unit is the first pressure sensor Gas injection into the first clamping tube body is controlled through the pressure value measured by maintaining the internal pressure of the first clamping tube body at a predetermined value.

In the present invention, the second clamping portion is fixed to the upper side of the second clamping bracket member, and a second clamping tube body absorbing the shock transmitted to the missile filled with gas therein and fixed to the upper side of the second clamping tube body The third clamping bracket member, which is located on the upper part and is opened to the upper part to insert a portion of the guided grenade, is rotatably connected to one side of the third clamping bracket member by a clamping hinge part and opened downward. A fourth clamping bracket member in which a fourth guided grenade inserting portion into which at least a portion of the remaining portion of the guide grenade is inserted is located may be further included.

In the present invention, the second clamping tube body includes a second pressure sensor capable of measuring the internal pressure, and the gas supply unit gas to the second clamping tube body through a pressure value measured by the second pressure sensor. By controlling the injection, the internal pressure of the second clamping tube body can be maintained at a predetermined value.

In the present invention, the second clamping portion is fixed to the upper side of the fourth clamping bracket member and is fixed to the upper side of the third clamping tube body and the third clamping tube body that is filled with gas inside and absorbs shock transmitted to the missile. And it may further include an upper plate member located on the top.

In the present invention, the third clamping tube body includes a third pressure sensor capable of measuring the internal pressure, and the gas supply part gas to the third clamping tube body through the pressure value measured by the third pressure sensor. By controlling the injection, the internal pressure of the third clamping tube body can be maintained at a predetermined value.

One embodiment of the carrier structure for a guided munition according to the present invention further comprises a clamp support portion standing on the guided grenade support member and detachably coupled to the second clamping portion to support the location of the second clamping portion, wherein the The clamp support part is a bracket fixing panel member to which the other end of the second clamping bracket member is detachably coupled, a fixed support panel member positioned at a rear side of the bracket fixing panel member, and a lower end fixed to the upper surface of the guided bullet support member, An elastic support positioned between the bracket fixing panel member and the fixing support panel member to absorb a longitudinal impact of guided bullets, and positioned between the bracket fixing panel member and the fixing support panel member to transfer the bracket fixing panel member. , It may include a front and rear movement guide rail portion for guiding the rear movement and limiting the up and down movement of the bracket fixing panel member.

In the present invention, the front and rear movement guide rails are first movable guide members protruding from the rear surface of the bracket fixing panel member and protruding from the front surface of the fixed support panel member so as to be movably coupled to the first movable guide member. 2 may include a moving guide member.

In the present invention, a first bracket fixing part overlapping the bracket fixing panel member is positioned at the other end of the second clamping bracket member, and a first bolt hole through which the first bolt passes is located at the first bracket fixing part, and the A first fastening hole to which a first bolt can be fastened is located on the bracket fixing panel member, and the lower side of the first fastening hole is supported on the front surface of the bracket fixing panel member to support the lower portion of the first bracket fixing part. A first supporting portion that matches one bolt hole to the first fastening hole may be positioned to protrude.

In the present invention, the second clamping portion is fixed to the upper side of the second clamping bracket member, and a second clamping tube body absorbing the shock transmitted to the missile filled with gas therein and fixed to the upper side of the second clamping tube body The third clamping bracket member, which is located on the upper part and is opened to the upper part to insert a portion of the guided grenade, is rotatably connected to one side of the third clamping bracket member by a clamping hinge part and opened downward. A fourth clamping bracket member in which at least a portion of the remaining portion of the guide grenade is inserted, the fourth guide grenade insert is positioned, fixed to the upper side of the fourth clamping bracket member, and filled with gas therein to absorb shock transmitted to the guide grenade Further comprising a clamping tube body and an upper plate member fixed to the upper side of the third clamping tube body and positioned on the upper side, and fixing the second bracket overlapping the bracket fixing panel member to the other end of the fourth clamping bracket member An additional position, a second bolt hole through which a second bolt passes is located in the second bracket fixing portion, and a second fastening hole in which the second bolt can be fastened is located in the bracket fixing panel member, and the bracket fixing panel On the front side of the member, a second supporting portion for matching the second bolt hole to the second fastening hole by supporting the lower portion of the second bracket fixing portion on the lower side of the second fastening hole is protruded, and the upper plate An upper plate fixing part overlapping the bracket fixing panel member is located at the other end of the member, a third bolt hole through which a third bolt is penetrated is located at the upper plate fixing part, and a third bolt is provided at the bracket fixing panel member. A third fastening hole that can be fastened is located, and the third bolt hole is attached to the third fastening hole by supporting a lower portion of the upper plate fixing part on a lower side of the third fastening hole on the front surface of the bracket fixing panel member. The matching third support may be positioned to protrude.

Another embodiment of the carrier structure for a guided munition according to the present invention is a guided grenade support member in which a guided grenade is located on an upper portion, is located on the guided grenade support member, clamps the guided grenade and is filled with gas therein to elastically support the guided grenade support member Guided missile clamping portion having a clamping tube body; It is located on the guide grenade support member, characterized in that it comprises a gas supply for injecting gas into the clamping tube body.

In the present invention, the guide grenade clamping portion is mounted on the guide grenade support member and includes a first clamping portion surrounding a portion of the guide grenade and a second clamping portion surrounding at least a portion of the remaining portion of the guide grenade, wherein the first clamping portion supports the guide grenade A lower plate member fixed on the member, a first clamping tube body fixed on the lower plate member, filled with gas therein, and absorbing the shock delivered to the guided grenade, located on top of the first clamping tube body, to the top It includes the first clamping bracket member in which the first guided grenade inserting portion into which a portion of the guided grenade is inserted is located, and the second clamping member is rotatably connected to one side of the first clamping bracket member with a clamping hinge portion and is lowered. A second clamping bracket member in which the second guided grenade inserting portion in which at least a portion of the remaining portion of the guided grenade is opened and inserted is positioned.

In the present invention, the first clamping tube body includes a first pressure sensor capable of measuring internal pressure, the first pressure sensor transmits the measured pressure to the gas supply unit, and the gas supply unit is the first pressure sensor Gas injection into the first clamping tube body is controlled through the pressure value measured by maintaining the internal pressure of the first clamping tube body at a predetermined value.

In the present invention, the second clamping portion is fixed to the upper side of the second clamping bracket member, and a second clamping tube body absorbing the shock transmitted to the missile filled with gas therein and fixed to the upper side of the second clamping tube body The third clamping bracket member, which is located on the upper part and is opened to the upper part to insert a portion of the guided grenade, is rotatably connected to one side of the third clamping bracket member by a clamping hinge part and opened downward. A fourth clamping bracket member in which a fourth guided grenade inserting portion into which at least a portion of the remaining portion of the guide grenade is inserted is located may be further included.

In the present invention, the second clamping tube body includes a second pressure sensor capable of measuring the internal pressure, and the gas supply unit gas to the second clamping tube body through a pressure value measured by the second pressure sensor. By controlling the injection, the internal pressure of the second clamping tube body can be maintained at a predetermined value.

In the present invention, the second clamping portion is fixed to the upper side of the fourth clamping bracket member and is fixed to the upper side of the third clamping tube body and the third clamping tube body that is filled with gas inside and absorbs shock transmitted to the missile. And it may further include an upper plate member located on the top.

In the present invention, the third clamping tube body includes a third pressure sensor capable of measuring the internal pressure, and the gas supply part gas to the third clamping tube body through the pressure value measured by the third pressure sensor. By controlling the injection, the internal pressure of the third clamping tube body can be maintained at a predetermined value.

Another embodiment of the carrier structure for a guided munition according to the present invention further comprises a clamp support portion standing on the guided grenade support member and detachably coupled to the second clamping portion to support the position of the second clamping portion, The clamp support part is a bracket fixing panel member to which the other end of the second clamping bracket member is detachably coupled, a fixed support panel member positioned at a rear side of the bracket fixing panel member, and a lower end fixed to the upper surface of the guided bullet support member, An elastic support positioned between the bracket fixing panel member and the fixing support panel member to absorb a longitudinal impact of guided bullets, and positioned between the bracket fixing panel member and the fixing support panel member to transfer the bracket fixing panel member. , It may include a front and rear movement guide rail portion for guiding the rear movement and limiting the up and down movement of the bracket fixing panel member.

In the present invention, the front and rear movement guide rails are first movable guide members protruding from the rear surface of the bracket fixing panel member and protruding from the front surface of the fixed support panel member so as to be movably coupled to the first movable guide member. 2 may include a moving guide member.

In the present invention, a first bracket fixing part overlapping the bracket fixing panel member is located at the other end of the second clamping bracket member, and a first bolt hole through which the first bolt passes is located in the first bracket fixing part, A first fastening hole to which a first bolt can be fastened is located on the bracket fixing panel member, and a lower side of the first fastening hole is supported on a front side of the bracket fixing panel member to support the lower portion of the first bracket fixing part. A first supporting portion that matches the first bolt hole to the first fastening hole may be positioned to protrude.

In the present invention, the second clamping portion is fixed to the upper side of the second clamping bracket member, and a second clamping tube body absorbing the shock transmitted to the missile filled with gas therein and fixed to the upper side of the second clamping tube body The third clamping bracket member, which is located on the upper part and is opened to the upper part to insert a portion of the guided grenade, is rotatably connected to one side of the third clamping bracket member by a clamping hinge part and opened downward. A fourth clamping bracket member in which at least a portion of the remaining portion of the guide grenade is inserted, the fourth guide grenade insert is positioned, fixed to the upper side of the fourth clamping bracket member, and filled with gas therein to absorb shock transmitted to the guide grenade Further comprising a clamping tube body and an upper plate member fixed to the upper side of the third clamping tube body and positioned on the upper side, and fixing the second bracket overlapping the bracket fixing panel member to the other end of the fourth clamping bracket member An additional position, a second bolt hole through which a second bolt passes is located in the second bracket fixing portion, and a second fastening hole in which the second bolt can be fastened is located in the bracket fixing panel member, and the bracket fixing panel On the front side of the member, a second supporting portion for matching the second bolt hole to the second fastening hole by supporting the lower portion of the second bracket fixing portion on the lower side of the second fastening hole is protruded, and the upper plate An upper plate fixing part overlapping the bracket fixing panel member is located at the other end of the member, a third bolt hole through which a third bolt is penetrated is located at the upper plate fixing part, and a third bolt is provided at the bracket fixing panel member. A third fastening hole that can be fastened is located, and the third bolt hole is attached to the third fastening hole by supporting a lower portion of the upper plate fixing part on a lower side of the third fastening hole on the front surface of the bracket fixing panel member. The matching third support may be positioned to protrude.

The present invention can prevent damage to electronic equipment by absorbing shock when transporting guided missiles, enabling accurate strike of targets while operating guided missiles and ensuring quality stability and operational stability of guided missiles, thereby enabling stable operation of guided missiles. Effect.

In addition, the present invention absorbs shock when transporting the missile, prevents explosion of the propulsion engine by shock and vibration, and safely transports the missile, thereby preventing safety accidents during the transport of the missile and greatly improving safety when carrying the missile It is effective.

1 is a perspective view showing an embodiment of a carrier structure for guided ammunition according to the present invention.
Figure 2 is a front view showing an embodiment of a carrier structure for guided ammunition according to the present invention.
3 is an enlarged cross-sectional view of a portion A of FIG. 2.
Figure 4 is a view showing an embodiment of the clamp support in the carrier structure for guided ammunition according to the present invention.
Figure 5 is a perspective view showing an example of use of the carrier structure for guided ammunition according to the present invention.
Figure 6 is a perspective view showing another embodiment of the carrier structure for guided ammunition according to the present invention.

The present invention will be described in more detail.

If described in detail by the accompanying drawings, preferred embodiments of the present invention. Prior to the detailed description of the present invention, terms or words used in the present specification and claims described below should not be construed as being limited to conventional or dictionary meanings. Therefore, the configuration shown in the embodiments and the drawings described in this specification are only the most preferred embodiments of the present invention and do not represent all of the technical spirit of the present invention, and thus can replace them at the time of application. It should be understood that there may be equivalents and variations.

Figure 1 is a perspective view showing an embodiment of a carrier structure for a guided munition according to the present invention, Figure 2 is a front view showing an embodiment of a carrier structure for a guided munition according to the present invention, Figure 3 is a view of Figure 2 It is a cross-sectional view of part A enlarged.

1 to 3, the carrier structure for guided ammunition according to the present invention includes a base member 100.

The base member 100 is elastically supported by the gas spring part 400 and a guided bullet support member 200 in which guided bullets are positioned on the top is positioned.

For example, the guided bullet support member 200 is spaced apart from the base member 100 and horizontally positioned parallel to the base member 100 by a gas spring.

The gas spring part 400 is located between the base member 100 and the guided bullet support member 200 so that the lower end portion is located on the base member 100 and the upper end portion supports the lower surface of the guided bullet support member 200 to guide the missile. The support member 200 is elastically supported.

The gas spring 400 is an example in which a gas such as a liquid or gas is filled therein and is formed of an elastic material capable of elongation and contraction, and various known gas spring structures serving as a buffer by filling a gas or gas therein It is noted that a more detailed description may be omitted as it may be modified.

The gas spring part 400 of the present invention is an example in which nitrogen gas is filled in more detail, for example, that the gas is filled therein.

The gas spring part 400 is positioned between the base member 100 and the guide grenade support member 200 so as to stably elastically support the guide grenade support member 200.

The carrier structure for a guided munition according to the present invention has a gas spring portion 400 located at each apex of the square base member 100 and the square guided bullet support member 200, to provide a total of four gas spring portions 400 ) To stably elastically support the guided bullet support plate member.

Between the base member 100 and the guided bullet support member 200, a vertical movement guide 600 for limiting horizontal movement of the guided bullet support member 200 may be located.

The moving guide part 600 is positioned to protrude to the lower portion of the first rail member 610 and the guide grenade support member 200 that protrude to the upper portion of the base member 100, and thus can be moved to the first rail member 610. It may include a second rail member 620 is coupled.

The moving guide part 600 is spaced apart between the base member 100 and the guide grenade support member 200 to stably limit movement of the guide grenade support member 200 in the horizontal direction, and guide the guide grenade The member 200 is moved only in the vertical direction, that is, in the upper and lower directions, thereby maximizing the buffering efficiency by the gas spring unit 400.

On the other hand, the upper surface of the guide munition support member 200 is a guide munition clamping unit 300 for clamping the guide munition to be transported to fix the location of the guide grenade.

In addition, a gas supply unit 500 capable of injecting gas into the gas spring unit 400 is located in the base member 100 or the guided bullet support member 200.

In the present invention, as an example, the gas supply unit 500 is positioned on the guided bullet support member 200.

As an example, the gas supply unit 500 injects gas into the gas spring unit 400, and more specifically, injects nitrogen gas into the gas spring unit 400.

The gas supply unit 500 connects a gas tank 510 for storing gas, a gas tank 510 and a gas spring unit 400, and injects gas into the gas spring unit 400 by injecting gas in the gas tank 510 It includes a gas injection control unit 530 for controlling gas injection, including a hose member 520, a control valve for opening and closing the flow path of the gas injection hose member 520.

The gas injection hose member 520 includes a plurality of first injection hoses 521 connecting the gas tank 510 and the gas injection control unit 530, and a plurality of gas injection control units 530 and the gas spring control unit 400. A second injection hose 522 is included.

The gas injection control unit 530 stably decomposes gas in the gas tank 510 into a plurality of gas spring units 400, that is, four second injection hoses 522 connected to four gas spring units 400, respectively. It includes a chamber that can be, and allows the gas to be stably injected into the plurality of gas spring portions 400, that is, four gas spring portions 400, through the chamber.

In addition, the gas injection control unit 530 is provided in each of a plurality of second injection hoses 522 connected to a plurality of gas springs 400, includes a plurality of control valves that open and close the flow path, and control the operation of the control valve By opening and closing the flow path of each second injection hose 522 individually to control the injection of gas into each gas spring 400.

When the control valve is opened by filling the gas tank 510 with nitrogen gas in a high pressure state, high pressure nitrogen gas is injected into the gas spring part 400 through the gas injection hose member 520.

In addition, the gas supply unit 500 may further include a plurality of distance displacement sensor units 7000 that measure a distance change between the base member 100 and the guided bullet support member 200 at the position of each gas spring unit 400. have.

The distance displacement sensor unit 7000 is an example of a laser displacement sensor capable of measuring a distance, and further detailed descriptions thereof are omitted, which can be performed using various known displacement sensors.

The distance displacement sensor unit 7000 measures the change in distance between the base member 100 and the guide grenade support member 200 at the position of each gas spring unit 400 and transmits it to the gas injection control unit 530.

The gas injection control unit 530 transmits the displacement of the distance between the base member 100 and the guide grenade support member 200 at the position of each gas spring unit 400 measured by the distance displacement sensor unit 7000, that is, the distance therebetween. The gas spring located at the position where the distance between the base member 100 and the guided bullet support member 200 decreases to automatically inject gas to minimize shock and vibration, and the guided bullet support member 200 maintains the guided bullet in a horizontal state So that it can be stably positioned.

On the other hand, the guided missile clamping part 300 is positioned on the guided missile support member 200 to be spaced apart in the longitudinal direction of the guided missile to stably clamp and support the guided missile.

The guided missile clamping part 300 is mounted on the guided missile support member 200 and includes a first clamping part 310 surrounding a portion of the guided missile and a second clamping part 320 surrounding at least a portion of the rest of the guided missile.

The first clamping part 310 is opened to the upper side and a first guided grenade inserting portion into which a portion of the missile is inserted is located, and the second clamping portion 320 is opened to the lower side and at least a portion of the remaining portion of the guided grenade is inserted into the second The missile insert is located.

The second clamping portion 320 is rotatably connected to a clamping hinge portion on one side of the first clamping portion 310 to rotate to open the first guided bullet inserting portion of the first clamping portion 310 to open the upper portion of the first guided bullet inserting portion It is possible to insert the guided grenade to the side into the first guided grenade insert.

In addition, the other end side of the second clamping part 320 is positioned to be detachably coupled to the other end side of the first clamping part 310 or is detachably coupled to a separate clamping support part to be coupled with the first clamping part 310. An example is to clamp the guided grenade located between the second clamping parts 320.

The guided missile clamping part 300 is filled with a gas therein to absorb shock transmitted to the missile.

In addition, the guided bullet clamping unit 300 is connected to the gas supply unit 500 to receive gas from the gas supply unit 500 and is maintained at a predetermined pressure, and includes a clamping tube body for clamping the guided coal to absorb shock delivered to the guided coal. And it can clamp the missile more stably.

In more detail, the first clamping part 310 is fixed to the lower plate member 311 and the lower plate member 311 which are fixed on the guided bullet support member 200 and is filled with gas therein and delivered to the guided bomb. The first clamping tube member 312, which is located above the first clamping tube body 312 and the first clamping tube body 312, which is opened to the top and inserts a portion of the guided grenade into which a portion of the guided grenade is inserted. Including, the second clamping bracket member 321 is rotatably connected to a clamping hinge portion on one side of the first clamping bracket member 313 and is opened downward and at least a portion of the remaining portion of the guided ammunition is inserted into the second guided bullet It may include a second clamping bracket member 321 in which the insertion portion is located.

The first clamping tube body 312 is filled with gas therein to support the first clamping bracket member 313 to be inserted into the first guided grenade insert of the first clamping bracket to absorb the shock delivered to the seated guided grenade.

In addition, the first clamping tube body 312 may be connected to the gas supply unit 500 to receive gas from the gas supply unit 500 to maintain a predetermined pressure.

The first clamping tube body 312 includes a first pressure sensor capable of measuring internal pressure, and the first pressure sensor delivers the measured pressure to the gas supply unit 500, that is, the gas injection control unit 530.

The gas supply unit 500 further includes a first tube gas injection hose member 540 connecting the first clamping tube body 312 and the gas tank 510, and the first tube gas injection hose member includes a gas injection control unit ( The chamber of 530 and the first clamping tube body 312 are connected to allow gas in the gas tank 510 to be injected into the first clamping tube body 312.

The gas injection control unit 530 includes a control valve for opening and closing the flow path of the first tube gas injection hose member 540 to control the gas injection of the first clamping tube body 312.

The gas injection control unit 530 opens the flow path of the first tube gas injection hose member 540 to inject gas into the first clamping tube body 312 when the pressure value detected by the first pressure sensor is smaller than a preset pressure value. Then, when the pressure value in the first clamping tube body 312 reaches a predetermined pressure value, the flow of the first tube gas injection hose member 540 is closed to stop gas injection.

The first clamping tube body 312 is connected to the gas supply unit 500 during the transport of the missile, so that the internal pressure value is kept constant to stably absorb the shock applied to the missile.

In addition, the second clamping portion 320 is fixed to the upper side of the second clamping bracket member 321, the second clamping tube body 322, which is filled with gas inside to absorb the shock delivered to the guided munition, the second clamping tube One of the third clamping bracket member 323, the third clamping bracket member 323, which is fixed to the upper side of the sieve 322, is located at the top, and is opened to the top to insert a portion of the guided grenade inserting part. It may further include a fourth clamping bracket member 324 that is rotatably connected to the side with a clamping hinge portion and is opened to the bottom to insert a fourth guided grenade insert into which at least a portion of the remaining portion of the missile is inserted.

The guided bullet clamping unit 300 clamps one guided bullet between the first clamping bracket member 313 and the second clamping bracket member 321, and the third clamping bracket member 323 and the fourth clamping bracket member 324 ) Can be transported by stacking a plurality of guided missiles by clamping the other guided missiles to improve the delivery efficiency of guided missiles.

In addition, the second clamping tube body 322 is filled with gas therein to support the third clamping bracket member 323 and is inserted into the third guided grenade insert of the third clamping bracket member 323 and transferred to the seated guided grenade. Absorbs shock.

In addition, the second clamping tube body 322 may be connected to the gas supply unit 500 to receive gas from the gas supply unit 500 to maintain a predetermined pressure.

The second clamping tube body 322 includes a second pressure sensor capable of measuring the internal pressure, and the second pressure sensor delivers the measured pressure to the gas supply unit 500, that is, the gas injection control unit 530.

The gas supply unit 500 further includes a second tube gas injection hose member 550 connecting the second clamping tube body 322 and the gas tank 510, and the second tube gas injection hose member 550 is gas The chamber of the injection control unit 530 and the second clamping tube body 322 are connected to allow gas in the gas tank 510 to be injected into the second clamping tube body 322.

The gas injection control unit 530 controls the gas injection of the second clamping tube body 322 including a control valve that opens and closes the flow path of the second tube gas injection hose member 550.

The gas injection control unit 530 opens the flow path of the second tube gas injection hose member 550 and injects gas into the second clamping tube body 322 when the pressure value detected by the second pressure sensor is smaller than a preset pressure value. Then, when the pressure value in the second clamping tube body 322 reaches a predetermined pressure value, the flow of the second tube gas injection hose member 550 is closed to stop gas injection.

The second clamping tube body 322 is connected to the gas supply unit 500 during the transport of the missile, so that the internal pressure value is kept constant so as to stably absorb the shock applied to the missile.

In addition, the second clamping part 320 is fixed to the upper side of the fourth clamping bracket member 324 and is filled with gas therein to absorb the shock transmitted to the missile, the third clamping tube body 325, the third clamping tube It is fixed to the upper side of the sieve 325 may further include an upper plate member 326 located on the top.

The third clamping tube body 325 is filled with gas therein to support the upper portion of the fourth clamping bracket member 324 to absorb the shock generated to the upper side of the missile.

In addition, the third clamping tube body 325 may be connected to the gas supply unit 500 to receive gas from the gas supply unit 500 and be maintained at a predetermined pressure.

The third clamping tube body 325 includes a third pressure sensor capable of measuring the internal pressure, and the third pressure sensor delivers the measured pressure to the gas supply unit 500, that is, the gas injection control unit 530.

The gas supply unit 500 further includes a third tube gas injection hose member 560 connecting the third clamping tube body 325 and the gas tank 510, and the third tube gas injection hose member is a gas injection control unit ( The chamber of 530 and the third clamping tube body 325 are connected to allow gas in the gas tank 510 to be injected into the third clamping tube body 325.

The gas injection control unit 530 controls the gas injection of the third clamping tube body 325 including a control valve that opens and closes the flow path of the third tube gas injection hose member 560.

The gas injection control unit 530 opens the flow path of the third tube gas injection hose member 560 to inject gas into the third clamping tube body 325 when the pressure value detected by the third pressure sensor is smaller than a preset pressure value. Then, when the pressure value in the third clamping tube body 325 reaches a predetermined pressure value, the flow of the third tube gas injection hose member 560 is closed to stop gas injection.

The third clamping tube body 325 is connected to the gas supply unit 500 during the transport of the missile, so that the internal pressure value is kept constant so as to stably absorb the shock applied to the missile.

The carrier structure for the guided munition according to the present invention is placed on the guided grenade support member 200 and the second clamping portion 320 is detachably coupled to clamp support 800 for supporting the position of the second clamping portion 320. ) May be further included.

In the clamp support part 800, the other end side of the second clamping bracket member 321 rotatably connected to one side of the first clamping part 310 is detachably coupled to fix the position of the second clamping part 320. And, the second clamping portion 320 is separated so that it can be rotated.

4 is a view showing an embodiment of the clamp support 800 in the carrier structure for guided ammunition according to the present invention. Referring to FIGS. 1, 2 and 4, the clamp support 800 is a second clamping bracket member. Bracket fixing panel member 810 to which the other end of 321 is detachably coupled, and a fixed supporting panel positioned to be spaced apart from the rear side of the bracket fixing panel member 810, and the lower end fixed to the upper surface of the guided bullet support member 200 Located between the member 820, the bracket fixed panel member 810 and the fixed support panel member 820, the elastic support 830 absorbing the longitudinal impact of the guided missile, the bracket fixed panel member 810 and the fixed support panel It is located between the members 820 to guide the front and rear movement of the bracket fixing panel member 810 and includes a front and rear movement guide rail portion 840 to limit the up and down movement of the bracket fixing panel member 810. .

The front and rear movement guide rails 840 are positioned to protrude on the front surface of the first movable guide member 841 and the fixed support panel member 820 that protrude on the rear surface of the bracket fixed panel member 810, and the first movable guide member ( 841) may include a second movement guide member 842 that is movably coupled to.

The front-rear movement guide rail part 840 is positioned between the bracket fixing panel member 810 and the fixing support panel member 820 to stably guide the movement before and after the bracket fixing panel member 810. .

The bracket fixing panel member is positioned elastically supported by an elastic support 830 on the front of the fixed support panel member 820 fixed to the lower end of the guided bullet support member 200, and is moved by a front and rear movement guide rail part 840 Up and down movements are limited, so they are moved only in the forward and backward directions, that is, in the longitudinal direction of the missile.

The clamp support portion 800 is linearly moved only in the forward and backward directions in a state in which the bracket fixing panel member is elastically supported by the elastic support 830 to absorb the shock generated in the longitudinal direction of the guided bullet during transport of the guided bullet.

The front and rear movement guide rail portion 840 is movably coupled to the second movement guide member 842 to the first movement guide member 841 to guide the bracket fixing panel member 810 to move linearly in the front and rear directions. .

In addition, the other end of the second clamping bracket member 321 overlaps the bracket fixing panel member 810 and the first bracket is detachably coupled to the bracket fixing panel member 810 by bolting the first bolt 811a. The government 321a is located.

In addition, the other end of the fourth clamping bracket member 324 is overlapped with the bracket fixing panel member 810 and the second bracket is detachably coupled to the bracket fixing panel member 810 by fastening the bolt of the second bolt 812a. Government 324a is located.

In addition, at the other end of the upper plate member 326, the upper plate fixing part 326a overlapping with the bracket fixing panel member 810 and detachably coupled to the bracket fixing panel member 810 by fastening the bolt of the third bolt 813a. ) Is located.

A first bolt hole 321b through which the first bolt 811a passes is located in the first bracket fixing portion 321a, and a second bolt through which the second bolt 812a penetrates in the second bracket fixing portion 324a. The hole 324b is positioned, and the third bolt hole 326b through which the third bolt 813a penetrates is located in the upper plate fixing part 326a.

In addition, the bracket fixing panel member 810 has a first fastening hole 811 to which the first bolt 811a can be fastened, a second fastening hole 812 to which the second bolt 812a can be fastened, and a third. The third fastening hole 813 to which the bolt 813a can be fastened is located.

The first bolt 811a penetrates the first bolt hole 321b and is fastened to the first fastening hole 811 to fix the first bracket fixing portion 321a to the bracket fixing panel member 810. In addition, the second bolt 812a penetrates through the second bolt hole 324b and is fastened to the second fastening hole 812 to fix the second bracket fixing portion 324a to the bracket fixing panel member 810. In addition, the third bolt 813a penetrates through the third bolt hole 326b and is fastened to the third fastening hole 813 to fix the upper plate member 326 to the bracket fixing panel member 810.

The front side of the bracket fixing panel member 810 supports the lower portion of the first bracket fixing portion 321a on the lower side of the first fastening hole 811 to attach the first bolt hole 321b to the first fastening hole 811. Support the lower portion of the second bracket fixing portion 324a on the lower side of the first supporting portion 814 and the second fastening hole 812 to match the second bolt hole 324b to the second fastening hole 812. Supporting the lower portion of the upper plate fixing portion 326a on the lower side of the second supporting portion 815 and the third fastening hole 813 to match, the third bolt hole 326b matches the third fastening hole 813. The third supporting portions 816 may be positioned to protrude respectively.

The first supporting portion 814 supports the first bracket fixing portion 321a so that the first bolt hole 321b coincides with the first fastening hole 811 so that the first bolt 811a is a first bolt hole ( It can be easily fastened to the first fastening hole (811) through 321b).

The second supporting portion 815 supports the second bracket fixing portion 324a so that the second bolt hole 324b coincides with the second fastening hole 812 so that the second bolt 812a is a second bolt hole ( 324b) to facilitate fastening to the second fastening hole 812.

The third supporting portion 816 supports the upper plate fixing portion 326a so that the third bolt hole 326b coincides with the third fastening hole 813 so that the third bolt 813a is a third bolt hole 326b. ) To be easily fastened to the third fastening hole 813.

The first bracket fixing part 321a, the second bracket fixing part 324a, and the upper plate fixing part 326a are coupled and fixed to the bracket fixing panel member, respectively, so that the second clamping bracket member 321 and the fourth clamping bracket member are fixed. (324), by limiting the up and down movement of the upper plate member 326, the guided clamp and the third clamping bracket member 323 clamped between the first clamping bracket member 313 and the second clamping bracket member 321 And the fourth clamping bracket member 324 so that the guided missile clamped between the clamping member 324 can be stably clamped.

That is, the clamp support portion 800 can absorb the shock generated in the longitudinal direction of the guided bullet during transportation through the bracket fixing panel portion elastically supported to be moved before and after by the elastic support 830.

5 is a perspective view showing an example of the use of a carrier structure for a guided munition according to the present invention, and referring to FIG. 5, a guided missile 10 is located on a guided member 200 of a guided structure for a guided structure according to the present invention It is clamped and positioned by a plurality of guided missile clamping parts 300.

The carrier structure for guided ammunition according to the present invention can absorb the shock generated during transportation of guided ammunition 10 into the gas spring 400 and reduce the shock delivered to the guided ammunition 10.

In addition, the carrier structure for the guided munition according to the present invention is the first clamping tube body 312, the second clamping tube body 322, the third clamping tube body 325 to the impact generated during the transport of the guided bullet 10 It is possible to minimize the impact transmitted to the guided bullet 10 by absorbing more through.

6 is a perspective view showing another embodiment of a carrier structure for a guided munition according to the present invention, and referring to FIG. 6, a carrier structure for a guided munition according to the present invention according to the present invention is located at the top of the guided bullet support member 200 It may further include a cover box member 900 which is positioned to be opened and closed and mounted on the guided bullet clamping part 300.

The cover box member 900 is coupled to the box hinge part 910, that is, the guide missile support member 200 so as to be rotatable by a hinge and rotated around the hinge to open and close.

The cover box member 900 is formed with a space for storing the guided bullet 10 therein, and the lower portion is formed of an open box body, and the guided bullet 10 is positioned inside through the opened lower portion.

The cover box member 900 is locked in a closed state by a cover lock (not shown), and is unlocked to be opened.

It is revealed that the cover lock part can be variously modified by using a locking structure of a known opening and closing part such as a buckle, and thus detailed description is omitted.

Then, the cover box member 900 is rotated and opened to expose the guided missile 10 stored therein so as to be separated from the guided missile clamping part 300.

The cover box member 900 prevents direct impact to the guided bullet 10 due to external factors during transportation to secure safety during guided bullet transportation, and can prevent damage to electronic equipment due to external impact during transportation.

The present invention can prevent the damage of electronic equipment by absorbing shock when transporting the guided missile 10, so that it is possible to accurately strike the target during operation of the guided missile 10, and ensure the quality stability and operational stability of the guided missile 10 There is an effect that enables stable operation of the guided missile 10.

In addition, the present invention absorbs shock when transporting the missile 10 to prevent an explosion of the propulsion engine due to shock and vibration and can safely transport the missile 10 to prevent a safety accident during the transport of the missile 10 , It has the effect of significantly improving the safety when the guided bullet 10 is transported.

The present invention is not limited to the above-described embodiments, but can be implemented by variously changing within a range not departing from the gist of the present invention.

10: guided bullet 100: base member
200: guide grenade support member 300: guide grenade clamping part
310: first clamping portion 311: lower plate member
312: 1st clamping tube body 313: 1st clamping bracket member
320: 2nd clamping part 321: 2nd clamping bracket member
321a: First bracket fixing part 321b: First bolt hole
322: 2nd clamping tube body 323: 3rd clamping bracket member
324: 4th clamping bracket member 324a: 2nd bracket fixing part
324b: second bolt hole 325: third clamping tube body
326: upper plate member 326a: upper plate fixing part
326b: third bolt hole 400: gas spring
500: gas supply unit 510: gas tank
520: gas injection hose member 521: first injection hose
522: second injection hose 530: gas injection control
540: first tube gas injection hose member 550: second tube gas injection hose member
560: third tube gas injection hose member 600: moving up and down guide
610: first rail member 620: second rail member
700: distance displacement sensor unit 800: clamp support unit
810: Bracket fixing panel member 811: First fastening
812: Second fastening 813: Third fastening
814: first support portion 815: second support portion
816: third support 820: fixed support panel member
830: elastic support 840: front and rear movement guide rail portion
841: first movement guide member 842: second movement guide member
900: cover box member 910: box hinge portion

Claims (27)

Base member;
A guided grenade support member positioned spaced apart on the base member and having a guided grenade on top;
A guided missile clamping portion located on the guided missile support member to clamp the guided missile;
A plurality of gas spring portions which are spaced apart between the base member and the guide grenade support member and are filled with gas to elastically support the guide grenade support member; And
It is located on the base member or the guide grenade support member and includes a gas supply unit for injecting gas into the gas spring unit,
The guided bullet clamping unit,
A first clamping part mounted on the guide grenade support member and surrounding a portion of the guide grenade; And
It includes a second clamping portion surrounding at least a portion of the remaining portion of the missile,
The first clamping portion,
A first clamping bracket member positioned on the guided grenade support member and in which a first guided grenade insert into which a portion of the guided grenade is inserted,
The second clamping portion,
It includes a second clamping bracket member which is rotatably connected to one side of the first clamping bracket member with a clamping hinge and is opened to the bottom to insert a second guided grenade insert into which at least a portion of the remaining portion of the guided grenade is inserted,
It is located on the guide grenade support member and further comprises a clamp support portion detachably coupled to the second clamping portion to support the position of the second clamping portion,
The clamp support
A bracket fixing panel member detachably coupled to the other end of the second clamping bracket member;
A fixed support panel member which is spaced apart from the rear side of the bracket fixing panel member and whose lower end is fixed to the upper surface of the guided bullet support member;
An elastic support positioned between the bracket fixing panel member and the fixing support panel member to absorb a longitudinal impact of the guided bullet;
It is located between the bracket fixed panel member and the fixed support panel member to guide the front and rear movement of the bracket fixed panel member and includes a front and rear movement guide rail portion for limiting the up and down movement of the bracket fixed panel member,
A first bracket fixing part overlapping the bracket fixing panel member is located at the other end of the second clamping bracket member,
A first bolt hole through which a first bolt passes is located in the first bracket fixing part, and a first fastening hole through which a first bolt can be fastened is located in the bracket fixing panel member,
The front of the bracket fixing panel member is positioned so as to protrude the first supporting portion for supporting the lower portion of the first bracket fixing portion on the lower side of the first fastening hole to match the first bolt hole to the first fastening hole. Carrier structure for guided munitions, characterized in that.
The method according to claim 1,
A carrier structure for a guided munition, characterized in that an elevating movement guide portion for limiting horizontal movement of the guided grenade support member is positioned between the base member and the guided grenade support member.
The method according to claim 2,
The moving guide unit,
A first rail member protruding above the base member; And
Carrier structure for a guided munition, characterized in that it comprises a second rail member that is movably coupled to the first rail member is protruded to the lower portion of the guide munition support member.
The method according to claim 1,
The gas supply unit,
A gas tank for storing gas;
A gas injection hose member connecting the gas tank and the gas spring portion to inject the gas in the gas tank into the gas spring portion; And
And a gas injection control unit for controlling gas injection, including a control valve for opening and closing the flow path of the gas injection hose member.
The method according to claim 4,
The gas supply unit further includes a plurality of distance displacement sensor units for measuring a change in distance between the base member and the guide grenade support member at the position of each gas spring unit,
The gas injection control unit is in a position where the distance between the base member and the guide grenade support member is reduced by receiving a displacement of the gap between the base member and the guide grenade support member at a position of each gas spring unit measured by the distance displacement sensor unit. A carrier structure for a missile, characterized in that the gas spring is automatically injected into the gas spring so that the guide missile support member is horizontal.
The method according to claim 1,
The guided missile clamping part
And a clamping tube body connected to the gas supply unit to receive gas from the gas supply unit and maintained at a predetermined pressure.
The method according to claim 6,
The first clamping portion,
A lower plate member fixed on the guide grenade support member;
It is fixed on the lower plate member and is filled with gas therein, absorbs shock transmitted to the guided munition, and further includes a first clamping tube body on which the first clamping bracket member is located. Vs structure.
The method according to claim 7,
The first clamping tube body includes a first pressure sensor capable of measuring internal pressure, and the first pressure sensor delivers the measured pressure to the gas supply,
The gas supply unit controls the gas injection into the first clamping tube body through the pressure value measured by the first pressure sensor, and maintains the internal pressure of the first clamping tube body at a predetermined value. Dragon carrier structure.
The method according to claim 7,
The second clamping portion,
A second clamping tube body fixed to the upper side of the second clamping bracket member and filled with gas therein to absorb shock transmitted to the missile;
A third clamping bracket member which is fixed to the upper side of the second clamping tube body, is located at the top and is opened to the top, and a third guided bullet inserting part into which a portion of the missile is inserted is located;
It characterized in that it further comprises a fourth clamping bracket member which is rotatably connected to one side of the third clamping bracket member with a clamping hinge part and is opened to the bottom to insert a fourth guided grenade insert into which at least a portion of the remaining portion of the missile is inserted. A carrier structure for guided ammunition.
The method according to claim 9,
The second clamping tube body includes a second pressure sensor capable of measuring the internal pressure,
The gas supply unit controls the gas injection into the second clamping tube body through the pressure value measured by the second pressure sensor, and maintains the internal pressure of the second clamping tube body at a predetermined value. Dragon carrier structure.
The method according to claim 9,
The second clamping portion,
A third clamping tube body fixed to the upper side of the fourth clamping bracket member and filled with gas therein to absorb shock transmitted to the missile; And
A carrier structure for a guided munition, further comprising an upper plate member fixed to an upper side of the third clamping tube body and positioned on the upper side.
The method according to claim 11,
The third clamping tube body includes a third pressure sensor capable of measuring the internal pressure,
The gas supply unit controls the gas injection into the third clamping tube body through the pressure value measured by the third pressure sensor to maintain the internal pressure of the third clamping tube body at a predetermined value. Dragon carrier structure.
delete The method according to claim 1,
The front and rear movement guide rail portion
A first movement guide member protruding from a rear side of the bracket fixing panel member; And
A carrier structure for a guided munition, comprising a second movement guide member positioned protrudingly in front of the fixed support panel member and movably coupled to the first movement guide member.
delete The method according to claim 1,
The second clamping portion,
A second clamping tube body fixed to the upper side of the second clamping bracket member and filled with gas therein to absorb shock transmitted to the missile;
A third clamping bracket member which is fixed to the upper side of the second clamping tube body, is located at the top and is opened to the top, and a third guided bullet inserting part into which a portion of the missile is inserted is located;
A fourth clamping bracket member rotatably connected to a side of the third clamping bracket member with a clamping hinge part and opened to the bottom to insert a fourth guided grenade insert into which at least a portion of the remaining portion of the guided grenade is inserted;
A third clamping tube body fixed to the upper side of the fourth clamping bracket member and filled with gas therein to absorb shock transmitted to the missile; And
It is further fixed to the upper side of the third clamping tube body and further includes an upper plate member located on the upper side,
A second bracket fixing part overlapping the bracket fixing panel member is positioned at the other end of the fourth clamping bracket member,
A second bolt hole through which a second bolt passes is located in the second bracket fixing portion, and a second fastening hole in which the second bolt can be fastened is located in the bracket fixing panel member,
On the front surface of the bracket fixing panel member, a second supporting portion for supporting the lower portion of the second bracket fixing portion to match the second bolt hole to the second fastening hole is protruded on the lower side of the second fastening hole. ,
An upper plate fixing part overlapping the bracket fixing panel member is located at the other end of the upper plate member,
A third bolt hole through which a third bolt penetrates is positioned in the upper plate fixing part, and a third fastening hole through which a third bolt can be fastened is located in the bracket fixing panel member,
On the front surface of the bracket fixing panel member, a third supporting portion supporting the lower portion of the upper plate fixing portion and matching the third bolt hole to the third fastening hole is protruded on the lower side of the third fastening hole. Characterized by a carrier structure for guided missiles.
A guided grenade support member with a guided grenade positioned over it;
A guided missile clamping part located on the guided missile support member to clamp the guided missile and having a gas filled therein to provide a clamping tube body elastically supporting the guided missile support member;
Located in the guide grenade support member and includes a gas supply for injecting gas into the clamping tube body,
The guided bullet clamping unit,
A first clamping part mounted on the guide grenade support member and surrounding a portion of the guide grenade; And
It includes a second clamping portion surrounding at least a portion of the remaining portion of the missile,
The first clamping portion,
A first clamping bracket member positioned on the guided grenade support member and in which a first guided grenade insert into which a portion of the guided grenade is inserted,
The second clamping portion,
It includes a second clamping bracket member which is rotatably connected to one side of the first clamping bracket member with a clamping hinge and is opened to the bottom to insert a second guided grenade insert into which at least a portion of the remaining portion of the guided grenade is inserted,
It is located on the guide grenade support member and further comprises a clamp support portion detachably coupled to the second clamping portion to support the position of the second clamping portion,
The clamp support
A bracket fixing panel member detachably coupled to the other end of the second clamping bracket member;
A fixed support panel member which is spaced apart from the rear side of the bracket fixing panel member and whose lower end is fixed to the upper surface of the guided bullet support member;
An elastic support positioned between the bracket fixing panel member and the fixing support panel member to absorb a longitudinal impact of the guided bullet;
It is located between the bracket fixed panel member and the fixed support panel member to guide the front and rear movement of the bracket fixed panel member and includes a front and rear movement guide rail portion for limiting the up and down movement of the bracket fixed panel member,
A first bracket fixing part overlapping the bracket fixing panel member is positioned at the other end of the second clamping bracket member,
A first bolt hole through which a first bolt penetrates is located in the first bracket fixing part, and a first fastening hole in which the first bolt can be fastened is located in the bracket fixing panel member,
The front of the bracket fixing panel member is positioned so as to protrude the first supporting portion for supporting the lower portion of the first bracket fixing portion on the lower side of the first fastening hole to match the first bolt hole to the first fastening hole. Carrier structure for guided munitions, characterized in that.
The method according to claim 17,
The first clamping portion,
A lower plate member fixed on the guide grenade support member;
It is fixed on the lower plate member, the gas is filled therein, absorbs the shock transmitted to the guided munition, and further comprises a first clamping tube body in which the first clamping bracket member is located on top. Structure.
The method according to claim 18,
The first clamping tube body includes a first pressure sensor capable of measuring internal pressure, and the first pressure sensor delivers the measured pressure to the gas supply,
The gas supply unit controls the gas injection into the first clamping tube body through the pressure value measured by the first pressure sensor, and maintains the internal pressure of the first clamping tube body at a predetermined value. Dragon carrier structure.
The method according to claim 18,
The second clamping portion,
A second clamping tube body fixed to the upper side of the second clamping bracket member and filled with gas therein to absorb shock transmitted to the missile;
A third clamping bracket member which is fixed to the upper side of the second clamping tube body, is located at the top and is opened to the top, and a third guided bullet inserting part into which a portion of the missile is inserted is located;
It characterized in that it further comprises a fourth clamping bracket member which is rotatably connected to one side of the third clamping bracket member with a clamping hinge part and is opened to the bottom to insert a fourth guided grenade insert into which at least a portion of the remaining portion of the missile is inserted. A carrier structure for guided ammunition.
The method according to claim 20,
The second clamping tube body includes a second pressure sensor capable of measuring the internal pressure,
The gas supply unit controls the gas injection into the second clamping tube body through the pressure value measured by the second pressure sensor to maintain the internal pressure of the second clamping tube body at a preset value. Dragon carrier structure.
The method according to claim 20,
The second clamping portion,
A third clamping tube body fixed to the upper side of the fourth clamping bracket member and filled with gas therein to absorb shock transmitted to the guided missile; And
A carrier structure for a guided munition, further comprising an upper plate member fixed to an upper side of the third clamping tube body and positioned on the upper side.
The method according to claim 22,
The third clamping tube body includes a third pressure sensor capable of measuring the internal pressure,
The gas supply unit controls the gas injection into the third clamping tube body through the pressure value measured by the third pressure sensor to maintain the internal pressure of the third clamping tube body at a predetermined value. Dragon carrier structure.
delete The method according to claim 17,
The front and rear movement guide rail portion
A first movement guide member protruding from a rear side of the bracket fixing panel member; And
A carrier structure for a guided munition, comprising a second movement guide member positioned protrudingly in front of the fixed support panel member and movably coupled to the first movement guide member.
delete The method according to claim 17,
The second clamping portion,
A second clamping tube body fixed to the upper side of the second clamping bracket member and filled with gas therein to absorb shock transmitted to the missile;
A third clamping bracket member which is fixed to the upper side of the second clamping tube body, is located at the top and is opened to the top, and a third guided bullet inserting part into which a portion of the missile is inserted is located;
A fourth clamping bracket member rotatably connected to a side of the third clamping bracket member with a clamping hinge part and opened to the bottom to insert a fourth guided grenade insert into which at least a portion of the remaining portion of the guided grenade is inserted;
A third clamping tube body fixed to the upper side of the fourth clamping bracket member and filled with gas therein to absorb shock transmitted to the missile; And
It is further fixed to the upper side of the third clamping tube body and further includes an upper plate member located on the upper side,
A second bracket fixing part overlapping the bracket fixing panel member is positioned at the other end of the fourth clamping bracket member,
A second bolt hole through which a second bolt passes is located in the second bracket fixing portion, and a second fastening hole in which the second bolt can be fastened is located in the bracket fixing panel member,
On the front surface of the bracket fixing panel member, a second supporting portion for supporting the lower portion of the second bracket fixing portion to match the second bolt hole to the second fastening hole is protruded on the lower side of the second fastening hole. ,
An upper plate fixing part overlapping the bracket fixing panel member is located at the other end of the upper plate member,
A third bolt hole through which a third bolt penetrates is positioned in the upper plate fixing part, and a third fastening hole through which a third bolt can be fastened is located in the bracket fixing panel member,
On the front surface of the bracket fixing panel member, a third supporting portion supporting the lower portion of the upper plate fixing portion and matching the third bolt hole to the third fastening hole is protruded on the lower side of the third fastening hole. Characterized by a carrier structure for guided missiles.

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