CN217005523U

CN217005523U - Inflatable launch vehicle false target

Info

Publication number: CN217005523U
Application number: CN202220724466.6U
Authority: CN
Inventors: 王向伟; 卫建业; 沙建军; 吕永胜; 罗代吉
Original assignee: Qingdao Jiuwei Huadun Science And Technology Research Institute Co ltd
Current assignee: Qingdao Jiuwei Huadun Science And Technology Research Institute Co ltd
Priority date: 2022-03-30
Filing date: 2022-03-30
Publication date: 2022-07-19
Anticipated expiration: 2032-03-30

Abstract

The utility model provides an inflatable launch vehicle decoy, relate to military use target camouflage technical field, including inflatable launch vehicle body and safety device against wind, launch vehicle body rear portion is equipped with the launcher, be equipped with the guided missile in the launcher, launcher and guided missile are inflatable structure, and make up together, launcher and guided missile intercommunication each other, the launcher passes through the breather pipe and this body coupling of launch vehicle, safety device against wind includes rope and earth anchor, the one end and this body coupling of launch vehicle of one part of them rope, the other end is connected with the earth anchor, and fix the launch vehicle body on the earth's surface through the earth anchor, the one end and the launcher of another part of rope are connected, the other end is connected with the earth anchor, and pull the rope through the earth anchor in order to realize the conversion of guided missile launch state and quiescent condition. This is novel can realize static and two kinds of states of transmission, and two kinds of states can change rapidly as required, and is with low costs, and light in weight is convenient for erect and is removed and receive, has the function of preventing wind, and field operation environment adaptability is strong.

Description

Inflatable launch vehicle false target

Technical Field

The utility model relates to a for military use target camouflage technical field, concretely relates to inflatable launch vehicle decoy.

Background

Military decoys are developed for decades and are various, and are divided into the following types according to structural forms: the method comprises the following steps of inflating type false targets, framework skin type false targets, assembling combined type false targets, compression expanding type false targets, foaming forming type false targets and the like. The inflatable false target is composed of an inflatable component made of plastic, rubber film or fabric, and has the characteristics of high appearance fidelity, light weight, small storage volume, high setting speed, relatively low price and the like. At present, typical military equipment such as missile weapon systems, fighters, helicopters, artilleries, tanks, armored vehicles and the like at home and abroad have corresponding inflatable decoys.

At present, during the simulation process of a false target, most of the false targets only simulate one presenting state of real equipment, and the simulation state is too single.

SUMMERY OF THE UTILITY MODEL

The utility model provides a false target of inflatable launch vehicle, its structural configuration is the launch vehicle, mainly adopts PVC to press from both sides screen cloth and oxford fabric to make and form, can realize static and launch two kinds of states, and two kinds of states can change rapidly as required, and is with low costs, light in weight, be convenient for erect and remove and receive, have the function of preventing wind, and field work environment adaptability is strong.

In order to achieve the purpose, the novel technical scheme is as follows:

the utility model provides an inflatable launch vehicle decoy, includes inflatable launch vehicle body and safety device against wind, launch vehicle body rear portion be equipped with the launcher, the launcher in be equipped with the guided missile, launcher and guided missile be inflatable structure to make up together, launcher and guided missile intercommunication each other, the launcher pass through breather pipe and this body coupling of launch vehicle, safety device against wind include rope and earth anchor, the one end and the launch vehicle body coupling of one of them part rope, the other end is connected with the earth anchor to fix the launch vehicle body at the earth's surface through the earth anchor, the one end and the launcher of another part rope are connected, the other end is connected with the earth anchor, and draw the rope through the earth anchor in order to realize the conversion of guided missile launch state and quiescent condition.

Preferably, the launch vehicle body include the base, the upper end of base from left to right made locomotive, shelter, chassis, breather pipe in proper order, base, locomotive, shelter, chassis, breather pipe communicate each other, the one end and the base of breather pipe be connected, the other end is connected with the one end of launcher bottom towards the rear of a vehicle, the one end of launcher both sides towards the locomotive be connected with the one end of rope respectively, under quiescent condition: the ground anchor pulls the rope and presses the launching rack on the upper surface of the chassis, and at the moment, the vent pipe is compressed, deformed and clamped between the launching rack and the chassis; in the launching state, the ground anchor pulls the rope to erect and keep the launcher stable, and the vent pipe is expanded and formed under the gas pressure.

Preferably, the launching vehicle body further comprises tires sewn on two sides of the base, and the tires are communicated with the base.

Preferably, a plurality of simulation small parts are sewn on the launching vehicle body, and the simulation small parts are communicated with the base in a direct or indirect mode.

Preferably, the launch vehicle body still include the supporting leg, the supporting leg including locate the base both sides and the top with the anterior supporting leg of shelter intercommunication and locate the base both sides and the top with the rear portion supporting leg of chassis intercommunication.

Preferably, the outer surfaces of the launcher body, the launcher and the missile are all made of PVC sandwich mesh cloth with the thickness of 0.3-0.45mm, and the inner surface of the launcher body, the launcher and the missile is shaped by taking oxford cloth as a lacing wire surface sheet.

Preferably, the front end of the base is provided with an inflation tube, the rear end of the base is provided with an exhaust tube, and the inflation tube and the exhaust tube are respectively provided with a valve.

Preferably, the outer sides of the inflation tube and the exhaust tube are both connected with shielding pieces, when the decoy is not used, the inflation tube and the exhaust tube are pushed into the base, and the shielding pieces shield a connecting port of the inflation tube or the exhaust tube and the base and are connected with the outer surface of the base through thread gluing.

Preferably, the inflation tube, the exhaust tube and the shielding piece are all made of PVC sandwich mesh cloth, and the diameters of the inflation tube and the exhaust tube are both 20 CM.

This novel false target's of inflatable launch vehicle beneficial effect:

(1) this is novel to launching vehicle class structure, according to the true imitation of equipping the model preparation, adopts the part to communicate each other, and the integrated design easily operates, is convenient for store.

(2) The novel PVC net clamping fabric sheet is made of PVC net clamping fabric materials with the thickness of 0.3-0.45mm, and the oxford fabric sheet is used as a lacing wire surface sheet for shaping, so that the novel PVC net clamping fabric sheet is light in overall weight and low in cost.

(3) This novel emitter can realize transmission and two kinds of static states, and two kinds of states can change fast.

(4) This novel air vent all establishes the shielding piece for hide the air vent that temporarily does not use.

(5) This is novel to have safety device, aerifys automobile body both sides and adopts rope and earth anchor fixed, has the anti-wind function.

Drawings

FIG. 1 is a schematic view of the overall structure of the novel static state;

FIG. 2 is a schematic diagram of the overall structure of the novel emitting state;

FIG. 3 is a front view of the present novel fill tube pushed into the base and covered by a shield;

FIG. 4 is a schematic top view of the novel emissive state;

FIG. 5 is a schematic diagram of a rear view structure of the novel emitting state;

1. a headstock; 2. a base; 3. a shelter; 4. a chassis; 5. a breather pipe; 6. a launcher; 7. a missile; 8. a rope; 9. a ground anchor; 10. supporting legs; 11. a tire; 12. widget A; 13. widget B; 14. an inflation tube; 15. a shielding sheet; 16. a spare tire; 17. a widget C; 18. a widget D; 19. a widget E; 20. a widget F; 21. a widget G; 22. a widget H; 23. widget I.

Detailed Description

The present invention is described in detail below with reference to the drawings, which are intended to illustrate preferred embodiments of the present invention and not to limit the scope of the present invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "left", "right", "top", "bottom", "inner", "outer", and the like indicate orientations and positional relationships based on the orientations and positional relationships shown in the drawings, and are only used for describing the present invention and simplifying the description, but do not indicate or imply that the device or the element to be referred to must have a specific orientation and a specific orientation configuration and operation, and thus, should not be construed as limiting the present invention.

An inflatable launch vehicle false target, as shown in fig. 1-5, comprises an inflatable launch vehicle body and a wind-proof device, wherein a launch frame 6 is arranged at the rear part of the launch vehicle body, a missile 7 is arranged in the launch frame 6, the launch frame 6 and the missile 7 are both in inflatable structures and sewn together, the launch frame 6 and the missile 7 are communicated with each other, the launch frame 6 is connected with the launch vehicle body through a vent pipe 5, the wind-proof device comprises ropes 8 and ground anchors 9 (used for being fixedly connected with the ground), one end of one part of the ropes 8 is connected with the launch vehicle body, the other end of the part of the ropes 8 is connected with the ground anchors 9, and the launch vehicle body is fixed on the ground surface through the ground anchors 9, as shown in fig. 1 and 2, the ropes can be selectively connected on the two sides of a vehicle head and a shelter respectively, one end of the other part of the ropes 8 is connected with the launch frame 6, and the other end of the ropes is connected with the ground anchors 9, and the rope 8 is pulled by the ground anchor 9 to realize the conversion between the launching state and the static state by the missile.

As shown in fig. 1, the launch vehicle body include base 2, the upper end of base 2 from left to right made locomotive 1, shelter 3, chassis 4, breather pipe 5 in proper order, base 2, locomotive 1, shelter 3, chassis 4, breather pipe 5 communicate each other, the one end and the base 2 of breather pipe 5 be connected, the other end is connected with 6 bottoms of launcher towards the one end of rear of a vehicle, 6 both sides of launcher be connected with the one end of rope 8 respectively towards the one end of locomotive, under quiescent condition: the ground anchor 9 pulls the rope 8 and presses the launching frame 6 on the upper surface of the chassis 4, and at the moment, the vent pipe 5 is compressed, deformed and clamped between the launching frame and the chassis 4; as shown in fig. 2, in the shooting state, the ground anchor 9 pulls the rope 8 to erect and keep stable the launcher, and the vent pipe expands and forms under the pressure of gas.

As shown in fig. 1 and 2, the launch vehicle body further comprises tires 11 sewn on two sides of the base 2, and the tires 11 are communicated with the base 2.

As shown in fig. 2 and 4, a plurality of simulation small parts (simulated according to the real launch vehicle small parts) are sewn on the launch vehicle body, and the simulation small parts are communicated with the base in a direct or indirect manner. The small parts directly sewed on the base are directly communicated with the base, and the small parts sewed at the top of the shelter are indirectly communicated with the base through the shelter.

As shown in fig. 1 and 2, the launch vehicle body further comprises support legs 10, wherein the support legs 10 comprise front support legs which are arranged on two sides of the base 2 and the top ends of which are communicated with the square cabin 3 and rear support legs which are arranged on two sides of the base and the top ends of which are communicated with the chassis 4.

As shown in figures 1-5, the outer surfaces of the launcher body, the launcher and the missile are all made of PVC mesh fabrics with the thickness of 0.3-0.45mm, and the inner surfaces of the launcher body, the launcher and the missile are shaped by taking oxford fabric as a lacing wire surface sheet.

As shown in fig. 1, 2 and 3, the front end of the base 2 is provided with an inflation tube 14, the rear end is provided with an exhaust tube (not shown), and the inflation tube 14 and the exhaust tube are respectively provided with a valve.

As shown in fig. 1, 2, and 3, the shielding sheets 15 are connected to the outer sides of the inflation tube 14 and the exhaust tube, when the decoy is not in use, the inflation tube 14 and the exhaust tube are pushed into the base 2, and the shielding sheets 15 shield the connection port between the inflation tube or the exhaust tube and the base and are connected to the outer surface of the base through sticky buckles.

As shown in fig. 1, 2 and 3, the inflation tube 14, the exhaust tube and the shielding sheet 15 are all made of PVC woven fabric, and the diameters of the inflation tube 14 and the exhaust tube are 20 CM.

This neotype theory of use:

this novel use divide into erects and withdraws two links.

Erecting links: firstly, a blower is connected with an inflation tube 14 in the front of a base, an exhaust tube at the rear of the base is closed, a shielding sheet 15 is closed, a blower switch is turned on, the whole launch vehicle decoy is inflated and formed, then one end of a rope 8 is connected with a ground anchor 9, and finally the ground anchor is fixed in the ground as shown in figures 1 and 2.

When inflated, the device is in a launched state, as shown in figure 2. In a static state, the rope 8 of the launching device is pulled towards the vehicle head, the launching device is pulled down on the chassis, the lower end of the rope 8 is connected with the ground anchor 9, and finally the ground anchor is fixed in the ground as shown in fig. 1.

In the withdrawing link, the ground anchor 9 is firstly pulled out of the ground, the connection between the ground anchor 9 and the rope 8 is simultaneously unfastened, the residual gas in the launching vehicle body is pumped out through the exhaust pipe by using the exhaust function of the blower, under the general condition, the blower can not completely pump out the gas in the vehicle body, the blower is stopped when the residual 1/6 gas is left, the inflation pipe and the exhaust pipe are opened simultaneously, the launching vehicle body is pressed to discharge the gas, then the inflation pipe and the exhaust pipe are pushed into the base, the shielding piece is covered, the inflatable launching vehicle body is folded, and the winding drum is placed into the packaging bag.

Claims

1. An inflatable launch vehicle decoy, characterized by: including inflatable launch vehicle body and safety device against wind, launch vehicle body rear portion be equipped with the launcher, the launcher in be equipped with the guided missile, launcher and guided missile be inflatable structure to make together, launcher and guided missile intercommunication each other, the launcher pass through breather pipe and launch vehicle body coupling, safety device against wind include rope and earth anchor, the one end and the launch vehicle body coupling of a part of rope wherein, the other end is connected with the earth anchor to fix the launch vehicle body at the earth's surface through the earth anchor, the one end and the launcher of another part of rope are connected, the other end is connected with the earth anchor to draw the rope through the earth anchor in order to realize the conversion of guided missile launch state and quiescent condition.

2. An inflatable launch vehicle decoy as recited in claim 1, wherein: the launch vehicle body include the base, the upper end of base from left to right made locomotive, shelter, chassis, breather pipe in proper order, base, locomotive, shelter, chassis, breather pipe communicate each other, the one end and the base of breather pipe be connected, the other end is connected with the one end of launch frame bottom towards the rear of a vehicle, the one end of launch frame both sides orientation locomotive be connected with the one end of rope respectively, under quiescent condition: the ground anchor pulls the rope and presses the launching rack on the upper surface of the chassis, and at the moment, the vent pipe is compressed, deformed and clamped between the launching rack and the chassis; in the launching state, the ground anchor pulls the rope to enable the launching frame to be erected and kept stable, and the vent pipe is formed in an expansion mode under the gas pressure.

3. An inflatable launch vehicle decoy as recited in claim 2, wherein: the launching vehicle body further comprises tires sewn on two sides of the base, and the tires are communicated with the base.

4. An inflatable launch vehicle decoy as recited in claim 3, wherein: the launching vehicle body is also sewed with a plurality of simulation small parts which are communicated with the base in a direct or indirect way.

5. An inflatable launch vehicle decoy as recited in claim 4, wherein: the launching vehicle body further comprises supporting legs, wherein the supporting legs comprise front supporting legs and rear supporting legs, the front supporting legs are arranged on two sides of the base, the top ends of the front supporting legs are communicated with the square cabin, and the rear supporting legs are arranged on two sides of the base, and the top ends of the rear supporting legs are communicated with the chassis.

6. An inflatable launch vehicle decoy as claimed in any one of claims 2 to 5, wherein: the outer surfaces of the launcher body, the launcher and the missile are all made of PVC sandwich mesh cloth with the thickness of 0.3-0.45mm, and the inner surface is shaped by taking oxford as a lacing wire surface piece.

7. An inflatable launch vehicle decoy as recited in claim 6, wherein: the front end of the base is provided with an inflation tube, the rear end of the base is provided with an exhaust tube, and the inflation tube and the exhaust tube are respectively provided with a valve.

8. An inflatable launch vehicle decoy as recited in claim 7, wherein: the utility model discloses a false target of air inflation pipe and blast pipe, including the base, the gas tube be connected with the shielding piece outside and all be connected with shielding piece, when the false target does not use, gas tube and blast pipe push in the base, shielding piece cover the connector of gas tube or blast pipe and base to be connected through the thread gluing with the base surface.

9. An inflatable launch vehicle decoy as recited in claim 8, wherein: the inflation tube, the exhaust tube and the shielding piece are all made of PVC sandwich mesh cloth, and the diameters of the inflation tube and the exhaust tube are both 20 CM.