CN203083428U

CN203083428U - Portable guided missile single-shot sitting-type launching supporting device

Info

Publication number: CN203083428U
Application number: CN 201220673872
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 portable guided missile single-shot sitting-type launching supporting device. A missile fixture is composed of two parallel clamping plates which are connected through arc-shaped ends and the lower ends of the clamping plates are provided with knob holes and rotary shaft holes. The upper end of a connecting frame is provided with through holes which correspond to the rotary shaft holes at the lower ends of the clamping plates. The upper end of the connecting frame is inserted between the lower ends of the two clamping plates of the missile fixture, and a rotary shaft penetrates through the rotary shaft holes and the through holes at the upper end of the connecting frame. A fastening knob penetrates through the knob holes in the two clamping plates and then is fixed. A saddle is installed at the top end of a tripod through a supporting rod. A supporting frame comprises a horizontal cross rod and a vertical support, wherein the upper end of the vertical support is provided with a pin hole which corresponds to a plug pin at the lower end of the connecting frame. The plug pin at the lower end of the connecting frame is inserted into the pin hole of the supporting frame, and therefore the connecting frame is fixed above the supporting frame. The portable guided missile single-shot sitting-type launching supporting device reduces fatigue and is applicable to long-time operation, a portable missile can be borne on the launching supporting device all the time during a launching process, and the device is simple in structure, low in weight, convenient to carry along, and capable of providing battlefield adaptability.

Description

A kind of portable guided missile single-shot sitting posture emission bracing or strutting arrangement

Technical field

The utility model relates to a kind of portable MISSILE LAUNCHING bracing or strutting arrangement, and operating personnel can launch on the bracing or strutting arrangement by seat.

Background technology

Portable MISSILE LAUNCHING bracing or strutting arrangement is the servicing unit of portable MISSILE LAUNCHING, effect is the portable guided missile launcher of stable support, 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 that by health rotation orientation angles regulates, hold handle by the right hand and move up and down and portable guided missile rotate around shoulder realize that luffing angle regulates, simultaneously the necessary supplemental support of left hand, guided missile weight is born the shoulder operating personnel, having subject matter is the guided missile Heavy Weight, and operating personnel rely on shoulder to support, and pressure is concentrated, make operating personnel's fatigue easily, reduce operational stability.Before emission, need jackknife portable guided missile picked up from ground and shoulder negatively, need jackknife after the emission portable guided missile is put to ground.Another kind is a seat posture 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's seat is at 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, complex structure, 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 guided missile single-shot sitting posture emission bracing or strutting arrangement is provided, this device supports on the ground by three-legged support, the portable guided missile of guided missile clamp, with after link is connected, guided missile weight is born on the three-legged support by bracing frame, operating personnel are sitting in seat and go up by foot and ground friction adjusting orientation angles, by the rotation shaft regulated luffing angle between link and the guided missile anchor clamps.Seat type operation is launched, is lessened fatigue, suitable long-time operation, and portable guided missile can be born all the time on the emission bracing or strutting arrangement in the emission process, and simple in structure, in light weight, be convenient to portable, battlefield adaptability is provided.

A kind of portable guided missile single-shot sitting posture is launched bracing or strutting arrangement, comprises guided missile anchor clamps, rotating shaft, tightening knob, link, bracing frame, seat and the A-frame of the portable guided missile of clamping; Wherein, 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;

Link is a strip-shaped bracket, and the link upper end is provided with and the corresponding through hole of the shaft hole of clamping plate lower end, 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; 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;

Seat is installed in the tripod top by support bar; Bracing frame comprises horizontal cross bar and perpendicular frame, and described perpendicular frame lower end is fixed on horizontal cross bar one end, and the horizontal cross bar other end is installed on the support bar by bearing, and horizontal cross bar can rotate around support bar by bearing; The upper end of perpendicular frame is provided with and the corresponding pin-and-hole of the latch of link lower end; The latch of link lower end inserts in the pin-and-hole of bracing frame, thereby link is fixed on the top of bracing frame.

The beneficial effects of the utility model are as follows:

1, by replacing guided missile anchor clamps, but the multiple portable guided missile of clamping.

2, operating personnel are sitting on the seat, use three-legged support to bear equipment and personnel's weight, avoid operation fatigue, and are easy and simple to handle.When not carrying out firing operation, can be used as portable guided missile support, support guided missile.

3, link uses pin to be connected with bracing frame, and is quick and stable.Can pack up during emission bracing or strutting arrangement three-legged support portable, also can use other supporting way.

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.

The specific embodiment

As shown in Figure 1 and Figure 2, portable guided missile single-shot sitting posture of the present utility model is launched bracing or strutting arrangement, comprises guided missile anchor clamps 2, rotating shaft 3, tightening knob 4, link 5, bracing frame 6, seat 7 and the A-frame 8 of the portable guided missile 1 of clamping; Wherein, described guided missile anchor clamps 2 are made up of two parallel clamping plate 2-2 that connect by arc tips 2-1, and the opposite position of the lower end of two described clamping plate 2-2 is equipped with knob hole 2-3 and shaft hole 2-4.

Link 5 is a strip-shaped bracket, and link 5 upper ends are provided with the corresponding through hole of shaft hole 2-4 with clamping plate 2-2 lower end, and the lower end is provided with the latch 5-1 of at least two vertical directions; Insert between the two clamping plates 2-2 lower end of guided missile anchor clamps 2 link 5 upper ends, and the through hole of shaft hole 2-4 and link 5 upper ends is passed in rotating shaft 3, thereby guided missile anchor clamps 2 are fixed on link 5 upper ends, and guided missile anchor clamps 2 can be around the shaft 3 rotate with respect to link 5; Tightening knob 4 passes behind the knob hole 2-3 on the two clamping plates 2-2 fixing, can control the clamping degree of two clamping plates 2-2 by the rotation of tightening knob 4.

Seat 7 is installed in tripod 8 tops by support bar 9.Three-legged support 8 launches the back and places on the ground.Bracing frame 6 comprises horizontal cross bar 6-2 and perpendicular frame 6-3, and described perpendicular frame 6-3 lower end is fixed on horizontal cross bar 6-2 one end, and the horizontal cross bar 6-2 other end is installed on the support bar 9 by bearing 10, and horizontal cross bar 6-2 can be by bearing 10 around support bar 9 rotations; The upper end of perpendicular frame 6-3 is provided with the corresponding pin-and-hole 6-1 with the latch 5-1 of link 5 lower ends; The latch 5-1 of link 5 lower ends inserts among the pin-and-hole 6-1 of bracing frame 6, thereby link 5 is fixed on the top of bracing frame 6.

When launching preparation, after portable guided missile 1 passed the arc tips 2-1 of guided missile anchor clamps 2, guided missile anchor clamps 2 lower ends are installed in link 5 upper ends by rotating shaft 3, tightening knob 4 screwed make two clamping plates 2-1 clamp link 5, the guided missile anchor clamps 2 of avoiding being equipped with portable guided missile 13 rotate with respect to link 5 around the shaft; Three-legged support 8 is launched, bracing frame 6 is connected on the support bar 9 of A-frame 8 tops by bearing 10, three-legged support 8 supports to ground.

As shown in Figure 3, enter emission state, operating personnel pick up the integral body of being made up of guided missile anchor clamps 2, rotating shaft 3, tightening knob 4, link 5 and portable guided missile 1, the latch 5-1 of link 5 lower ends are inserted among the pin-and-hole 6-1 of bracing frame 6 upper ends; Operating personnel's both legs separately are sitting on the seat 7 towards transmit direction.The tightening knob 4 of outwarding winding, the tightening knob 4 of outwarding winding can rotate guided missile anchor clamps 2 with respect to link 5 in certain angle, hold the guided missile handle by the right hand then and move up and down, make 3 rotations around the shaft of portable guided missile realize that luffing angles regulate, be adjusted to screw behind the correct position and prohibit solid knob 4; By operating personnel foot and ground friction, make bracing frame 6 realize regulating orientation angles around support bar 9 rotations at last by bearing.

Claims

1. a portable guided missile single-shot sitting posture is launched bracing or strutting arrangement, it is characterized in that, comprise guided missile anchor clamps (2), rotating shaft (3), tightening knob (4), link (5), bracing frame (6), seat (7) and the A-frame (8) of the portable guided missile of clamping (1); Wherein, described guided missile anchor clamps (2) are made up of the two parallel clamping plate (2-2) that connect by arc tips (2-1), and the opposite position of the lower end of two described clamping plate (2-2) is equipped with knob hole (2-3) and shaft hole (2-4);

Link (5) is a strip-shaped bracket, and link (5) upper end is provided with the corresponding through hole of shaft hole (2-4) with clamping plate (2-2) lower end, and the lower end is provided with the latch (5-1) of at least two vertical directions; Insert between two clamping plates (2-2) lower end of guided missile anchor clamps (2) link (5) upper end, the through hole of shaft hole (2-4) and link (5) upper end is passed in rotating shaft (3), thereby guided missile anchor clamps (2) are fixed on link (5) upper end, and guided missile anchor clamps (2) around the shaft (3) rotate with respect to link (5); Knob hole (2-3) back that tightening knob (4) passes on the two clamping plates (2-2) is fixing, can control the clamping degree of two clamping plates (2-2) by the rotation of tightening knob (4);

Seat (7) is installed in tripod (8) top by support bar (9); Bracing frame (6) comprises horizontal cross bar (6-2) and perpendicular frame (6-3), described perpendicular frame (6-3) lower end is fixed on horizontal cross bar (6-2) end, horizontal cross bar (6-2) other end is installed on the support bar (9) by bearing (10), and horizontal cross bar (6-2) can pass through bearing (10) and rotate around support bar (9); The upper end of perpendicular frame (6-3) is provided with the corresponding pin-and-hole of latch (5-1) (6-1) with link (5) lower end; The latch (5-1) of link (5) lower end inserts in the pin-and-hole (6-1) of bracing frame (6), thereby link (5) is fixed on the top of bracing frame (6).