CN203083437U

CN203083437U - Wearing type portable missile launching supporting device

Info

Publication number: CN203083437U
Application number: CN 201220676457
Authority: CN
Inventors: 李世龙
Original assignee: TIANWEI ELECTRONIC SYSTEM ENGINEERING Co Ltd XI'AN
Current assignee: TIANWEI ELECTRONIC SYSTEM ENGINEERING Co Ltd XI'AN
Priority date: 2012-12-10
Filing date: 2012-12-10
Publication date: 2013-07-24
Anticipated expiration: 2022-12-10

Abstract

The utility model discloses a wearing type portable missile launching supporting device. A missile clamp is composed of two parallel clamping plates which are connected through an arc end, and the lower ends of the two clamping plates are provided with a knob hole and a rotating shaft hole respectively. A connecting support is a strip-shaped support, a through hole is formed at the upper end of the connecting support, and at least two inserted pins are arranged at the lower end of the connecting support. A vest comprises a waistband and slings which are connected on the waistband, one end of a transverse support is fixed on the front face of the waistband, and pin holes which correspond to the inserted pins at the lower end of the connecting support are formed in the upper surface of the other end of the transverse support. The inserted pins at the lower end of the connecting support are inserted into the pin holes of the transverse support. When used, the wearing type portable missile launching supporting device is worn by an operator, the weight of a missile can be dispersed to a plurality of supporting points, the pitch angle is adjusted through a rotating shaft between the connecting support and the missile clamp, the direction and the angle are adjusted through rotation of the operator, and the wearing type portable missile launching supporting device is flexible in operation, comfortable to wear, suitable for long-term operation and capable of operating in a moving mode, and provides battlefield adaptability.

Description

A kind of portable MISSILE LAUNCHING bracing or strutting arrangement of Wearable

Technical field

The utility model relates to a kind of portable MISSILE LAUNCHING bracing or strutting arrangement of Wearable.

Background technology

Portable MISSILE LAUNCHING bracing or strutting arrangement is a kind of servicing unit for portable MISSILE LAUNCHING, its effect is stably to support portable guided missile launcher, be convenient to orientation angles and luffing angle that operating personnel regulate portable guided missile, realize that aerial target to air defense operational control system assignment and indication aims at and launches.

At present, common portable MISSILE LAUNCHING has two kinds.A kind of is to launch pickaback, operating personnel shoulder the right side with portable guided missile and take on, realize the orientation angles adjusting by the health rotation, holding handle by the right hand moves up and down and portable guided missile is rotated around shoulder realize that luffing angle regulates, the necessary supplemental support of while left hand, guided missile weight is born the shoulder operating personnel.In this radiation pattern, because guided missile weight is bigger, operating personnel rely on shoulder to support, and pressure is concentrated, and makes operating personnel's fatigue easily, reduces operational stability.Another kind is a sitting posture formula launcher, about on " Y " shape support body, respectively set up one piece of portable guided missile, direction rotating shaft is established in " Y " shape frame bottom, about establish the pitching rotating shaft, operating personnel are sitting in Y " in the middle of the shape support body; utilize the friction of foot and bottom rotating disk to make portable guided missile realize that orientation angles regulates, utilize both hands to move up and down to realize luffing angle to regulate, the apparatus structure complexity of this radiation pattern, volume are big, Heavy Weight, move difficulty.

Summary of the invention

Defective or deficiency at above-mentioned prior art existence, the purpose of this utility model is, a kind of portable MISSILE LAUNCHING bracing or strutting arrangement of Wearable is provided, during use it is worn on one's body the operating personnel, guided missile weight can be distributed to a plurality of fulcrums, by the rotation shaft regulated luffing angle between link and the guided missile anchor clamps, rotate the adjusting orientation angles by operating personnel self, flexible operation, comfortable, the suitable long-time operation of wearing, and movable operation provide battlefield adaptability.

In order to realize above-mentioned task, the utility model adopts following technical solution:

A kind of emission bracing or strutting arrangement of portable guided missile Wearable, the guided missile anchor clamps, rotating shaft, tightening knob, link, horizontal support and the vest that comprise the portable guided missile of clamping, described guided missile anchor clamps are made up of two parallel clamping plate that connect by arc tips, and the opposite position of the lower end of two described clamping plate is equipped with knob hole and shaft hole;

Described link is a strip-shaped bracket, and link upper end is provided with the corresponding through hole of shaft hole with the lower end of clamping plate, and the lower end is provided with the latch of at least two vertical directions; Insert between the two clamping plates lower end of guided missile anchor clamps the link upper end, and the through hole of shaft hole and link upper end is passed in rotating shaft, thereby the guided missile anchor clamps are fixed on the link upper end, and the guided missile anchor clamps can rotate with respect to link around the shaft; Described tightening knob passes behind the knob hole on the two clamping plates fixing, can control the clamping degree of two clamping plates by the rotation of tightening knob;

Described vest comprises waistband and is connected braces on the waistband, and an end of horizontal support is fixed on the front of described waistband, and the other end upper surface of described horizontal support is provided with and the corresponding pin-and-hole of the latch of link lower end; The latch of described link lower end inserts in the pin-and-hole of horizontal support, thereby link is fixed on the horizontal support top.

Further, described horizontal support is fixed on the waistband of vest by screw.

The beneficial effects of the utility model are as follows:

But 1, use special-purpose vest disperse weight, avoid operation fatigue, and can move flexibly.

2, can be by changing the dissimilar multiple portable missile tube of guided missile fixture operation.

3, link is connected by pin with horizontal support, and is simple to operation, quick and stable.

Description of drawings

Fig. 1 is the structural representation of launch readiness of the present utility model.

Fig. 2 is the structural representation of guided missile furniture.

Fig. 3 is the structural representation of the utility model emission state.

Below in conjunction with the drawings and specific embodiments the utility model is further explained.

The specific embodiment

As shown in Figure 1 and Figure 2, the emission bracing or strutting arrangement of portable guided missile Wearable of the present utility model, the guided missile anchor clamps 1, rotating shaft 2, tightening knob 3, link 4, horizontal support 5 and the vest 6 that comprise the portable guided missile 7 of clamping, wherein, described guided missile anchor clamps 1 are made up of two parallel clamping plate 1-2 that connect by arc tips 1-1, and the opposite position of the lower end of two described clamping plate 1-2 is equipped with knob hole 1-3 and shaft hole 1-4.

Link 4 is a strip-shaped bracket, and link 4 upper ends are provided with the corresponding through hole of shaft hole 1-4 with the lower end of clamping plate 1-2, and the lower end is provided with the latch 4-1 of at least two vertical directions; Insert between the two clamping plates 1-2 lower end of guided missile anchor clamps 1 link 4 upper ends, and the through hole of shaft hole 1-4 and link 4 upper ends is passed in rotating shaft 2, thereby guided missile anchor clamps 1 are fixed on link 4 upper ends, and guided missile anchor clamps 1 can be around the shaft 2 rotate with respect to link 4; Tightening knob 3 passes behind the knob hole 1-3 on the two clamping plates 1-2 fixing, can control the clamping degree of two clamping plates 1-2 by the rotation of tightening knob 3.

Vest 6 comprises waistband 6-1 and is connected braces 6-2 on the waistband 6-1, and an end of horizontal support 5 is fixed on the front of described waistband 6-1, and the other end upper surface of horizontal support 5 is provided with the corresponding pin-and-hole 5-1 with the latch 4-1 of link 4 lower ends; The latch 4-1 of link 4 lower ends inserts among the pin-and-hole 5-1 of horizontal support 5, thereby link 4 is fixed on the top of horizontal support 5.

When launching preparation, after portable guided missile 7 passed the arc tips 1-1 of guided missile anchor clamps 1, guided missile anchor clamps 1 lower end is installed in link 4 upper ends by rotating shaft 2, tightening knob 3 is screwed the upper end that makes two clamping plates 1-1 clamp link 4, and the guided missile anchor clamps of avoiding being equipped with portable guided missile 72 rotate with respect to link 4 around the shaft; Vest 6 is clothed on one's body the operating personnel, the waistband position that horizontal support 5 is installed is placed the operating personnel front.

As shown in Figure 3, enter emission state, operating personnel pick up the integral body of being made up of guided missile anchor clamps 1, rotating shaft 2, tightening knob 3, link 4 and portable guided missile 7, the latch 4-1 of link 4 lower ends are inserted among the pin-and-hole 5-1 of horizontal support 5 upper ends; The tightening knob 3 of outwarding winding can rotate guided missile anchor clamps 1 with respect to link 4, holds the guided missile handle by the right hand then and moves up and down, and makes 2 rotations around the shaft of portable guided missile realize that luffing angles regulate, and is adjusted to screw behind the correct position to prohibit solid knob 3; Rotate by operating personnel self again and regulate orientation angles.

Claims

1. the emission bracing or strutting arrangement of a portable guided missile Wearable, it is characterized in that, comprise the guided missile anchor clamps (1), rotating shaft (2), tightening knob (3), link (4), horizontal support (5) and the vest (6) that are used for the portable guided missile of clamping (7), described guided missile anchor clamps (1) are made up of the two parallel clamping plate (1-2) that connect by arc tips (1-1), and the opposite position of the lower end of two described clamping plate (1-2) is equipped with knob hole (1-3) and shaft hole (1-4);

Described link (4) is a strip-shaped bracket, and link (4) upper end is provided with the corresponding through hole of shaft hole (1-4) with the lower end of clamping plate (1-2), and the lower end is provided with the latch (4-1) of at least two vertical directions; Insert between two clamping plates (1-2) lower end of guided missile anchor clamps (1) link (4) upper end, the through hole of shaft hole (1-4) and link (4) upper end is passed in rotating shaft (2), thereby guided missile anchor clamps (1) are fixed on link (4) upper end, and guided missile anchor clamps (1) around the shaft (2) rotate with respect to link (4); Knob hole (1-3) back that described tightening knob (3) passes on the two clamping plates (1-2) is fixing, can control the clamping degree of two clamping plates (1-2) by the rotation of tightening knob (3);

Described vest (6) comprises waistband (6-1) and is connected braces (6-2) on the waistband (6-1), one end of horizontal support (5) is fixed on the front of described waistband (6-1), and the other end upper surface of described horizontal support (5) is provided with the corresponding pin-and-hole of latch (4-1) (5-1) with link (4) lower end; The latch (4-1) of described link (4) lower end inserts in the pin-and-hole (5-1) of horizontal support (5), thereby link (4) is fixed on horizontal support (5) top.

2. the emission bracing or strutting arrangement of portable guided missile Wearable as claimed in claim 1 is characterized in that, described horizontal support (5) is fixed on the waistband (6-1) of vest (6) by screw.