CN214470421U - Supporting and fixing device for guided missile and bomb - Google Patents

Supporting and fixing device for guided missile and bomb Download PDF

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Publication number
CN214470421U
CN214470421U CN202120025330.1U CN202120025330U CN214470421U CN 214470421 U CN214470421 U CN 214470421U CN 202120025330 U CN202120025330 U CN 202120025330U CN 214470421 U CN214470421 U CN 214470421U
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CN
China
Prior art keywords
hasp
missile
support
fixing device
plate
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Active
Application number
CN202120025330.1U
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Chinese (zh)
Inventor
严超亮
张义帅
王行中
王群
陈洪卫
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Shandong Jukai New Material Co.,Ltd.
Original Assignee
Shandong Jukai Civil Air Defense Engineering Co ltd
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Priority to CN202120025330.1U priority Critical patent/CN214470421U/en
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Publication of CN214470421U publication Critical patent/CN214470421U/en
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Abstract

The utility model relates to a supporting and fixing device for guided missiles and bombs, which comprises a missile support and a frame-type beam, wherein the frame-type beam is provided with a positioning hole, the missile support is integrally fixed in the positioning hole, the bottom of the missile support is provided with a missile seat adapter plate and a plurality of positioning pins, the positioning pins are inserted into the frame-type beam, and the bottom of the missile seat adapter plate is connected with the frame-type beam through a connecting piece; the two sides of the bullet support are provided with a bullet seat hook plate and a hasp lock which are mutually matched and connected, and the bullet seat hook plate and the hasp lock are used for fixing a bullet body placed at the top of the bullet support roller assembly. The elastic seat hook plate and the hasp lock are respectively fixed on two sides of the elastic support through the canvas press plate and the canvas; an anti-static rubber is arranged in the middle of the canvas bag pressing plate; the front and the back surfaces of the elastic support are provided with hasp locks. The utility model has the advantages that, the anti-static rubber on the sack contacts with the surface of the projectile body, increases the frictional force, prevents the rotation of the projectile body.

Description

Supporting and fixing device for guided missile and bomb
Technical Field
The utility model belongs to the technical field of projectile body fixing device, concretely relates to support fixing device of guided missile and bomb.
Background
Missile weaponry needs to pass through the transportation process from production to equipment units and task training, the transportation environment influences the performance of the missile weaponry, and the good and bad of the equipment transportation performance are necessarily related to the equipment reliability; the transportation mode comprises personnel carrying, vehicle transportation, ship transportation, air transportation and air delivery, and the research on the transportation performance of the missile weaponry has practical significance.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the above problem, providing an increase frictional force prevents the support fixing device of projectile body pivoted guided missile and bomb.
In order to achieve the above object, the utility model provides a following technical scheme:
a supporting and fixing device for guided missiles and bombs comprises a missile support and a frame-type beam, and is characterized in that the frame-type beam is provided with a positioning hole, the missile support is integrally fixed in the positioning hole, the bottom of the missile support is provided with a missile seat adapter plate and a plurality of positioning pins, the positioning pins are inserted into the frame-type beam, and the bottom of the missile seat adapter plate is connected with the frame-type beam through a connecting piece;
the two sides of the bullet support are provided with a bullet seat hook plate and a hasp lock which are mutually matched and connected, and the bullet seat hook plate and the hasp lock are used for fixing a bullet body placed at the top of the bullet support roller assembly.
Further, the elastic seat hook plate and the hasp lock are fixed on two sides of the elastic support through the canvas press plate and the canvas respectively.
Furthermore, an anti-static rubber is arranged in the middle of the canvas press plate.
Furthermore, a hasp handle and a spring pin are arranged on the hasp lock.
Furthermore, the connecting piece is a bolt and a self-locking nut or a double nut which are connected in a matched mode.
Furthermore, the front and the rear surfaces of the elastic support are provided with snap locks.
Furthermore, the hasp lock comprises a hasp base and a hasp handle fixed on the hasp base, and the hasp base, the hasp handle and the hook T-shaped stud are coaxially connected through a fastening bolt below the hasp base; and a hook ring nut and a second hook plate are sequentially connected below the hook T-shaped stud.
Furthermore, the hook T-shaped stud is connected with the pin shaft gasket and the hasp handle through a pin shaft, and the hook T-shaped stud rotates within an effective range.
Furthermore, the hasp base is connected with the hasp adapter plate or the door plate fixing plate through a countersunk screw, and the middle of the hasp base is additionally provided with the canvas adapter plate when the hasp base is fixed with the hasp adapter plate.
Compared with the prior art, the beneficial effects of the utility model reside in that:
the utility model discloses place the projectile body on an, two bullet support subassemblies of b, and the fulcrum position needs unanimous with projectile body fulcrum position, because the projectile body directly places and to have the rotation on bullet support subassembly, twine the sack on the projectile body surface, pull out quick-release spring catch, adjust hasp ring nut, make it closely detain mutually with the couple board, promote the hasp handle downwards, make the couple board closely detain mutually with hasp ring nut, let prevent static rubber and projectile body surface contact on the sack, increase frictional force, insert quick-release spring catch, prevent the rotation of projectile body.
Drawings
In order to more clearly illustrate the technical solution of the embodiment of the present invention, the drawings required to be used in the description of the embodiment will be briefly introduced below, it is obvious that the drawings in the following description are only for more clearly illustrating the embodiment of the present invention or the technical solution in the prior art, and for those skilled in the art, other drawings can be obtained according to the drawings without any creative effort.
Fig. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of the present invention;
fig. 3 is a schematic structural view of the adapter plate of the cartridge holder of the present invention;
in the figure: 1-elastic support, 2-elastic body, 3-spring pin, 4-canvas press plate, 5-canvas, 6-roller component, 8-hook plate, 9-hasp lock, 10-antistatic rubber, 11-hasp handle, 12-frame beam, 13-positioning hole, 14-connecting piece, 15-positioning pin, 16-second hook plate, 17-hook T-shaped stud, 18-hasp base, 19-elastic base adapter plate and 20-hasp ring nut.
Detailed Description
In order to make the technical solution of the present invention better understood by those skilled in the art, the present invention will be further described with reference to the following specific embodiments, which are provided as illustration only and are not intended to limit the present invention.
The missile and bomb supporting and fixing device shown in fig. 1-3 comprises a bomb support 1 and a frame-type beam 12, wherein a positioning hole 13 is formed in the frame-type beam 12, the bomb support 1 is integrally fixed in the positioning hole 13, a bomb seat adapter plate 19 and a plurality of positioning pins 15 are arranged at the bottom of the bomb support 1, the positioning pins 15 are inserted into the frame-type beam 12, and the bottom of the bomb seat adapter plate 19 is connected with the frame-type beam 12 through a connecting piece 14; the two sides of the bullet support 1 are provided with a bullet support hook plate 8 and a hasp lock 9 which are mutually matched and connected, and the bullet support hook plate and the hasp lock 9 are used for fixing the bullet bodies 2 placed at the top of the bullet support roller assembly 6; the elastic seat hook plate 8 and the hasp lock 9 are respectively fixed on two sides of the elastic support 1 through the canvas press plate 4 and the canvas 5. An anti-static rubber 10 is arranged in the middle of the canvas bag pressing plate 4; the hasp lock 9 is provided with a hasp handle 11 and a spring pin 3.
The front surface and the rear surface of the elastic support seat 1 are respectively provided with a hasp lock, the hasp lock comprises a hasp base 18 and a hasp handle 11 fixed on the hasp base 18, and the hasp base 18, the hasp handle 11 and a hook T-shaped stud 17 are coaxially connected through a fastening bolt below the hasp base 18; and a hook ring nut 20 and a second hook plate 16 are sequentially connected below the hook T-shaped stud 17.
The hook T-shaped stud 17 is connected with the pin shaft gasket and the hasp handle 11 through a pin shaft, and the hook T-shaped stud 17 rotates within an effective range. The hasp base 18 is connected with a hasp adapter plate or a door plate fixing plate through countersunk screws, and a canvas adapter plate is additionally arranged in the middle of the hasp base 18 and the hasp adapter plate when the hasp base is fixed.
Preferably, the connecting member 14 is a bolt and a self-locking nut or a double nut which are connected in a matching manner.
The utility model discloses application method does:
according to the known fulcrum distance L, a positioning hole 13 is processed on a frame type cross beam 12, the elastic support 1 assembly is integrally fixed and inserted into the corresponding positioning hole 13, an elastic support hook plate 8 is fixed on the side surface of the elastic support 1, a hasp handle 11 is pulled off, a hasp ring nut 20 is adjusted to a proper length and is buckled on the hook plate 8, the hasp handle 11 is pushed upwards until the front surface and the rear surface of the elastic support are close to each other, and a quick-release spring pin 3 is inserted into a hasp base 18, so that the hasp handle 11 is prevented from falling off due to stress. Bolts at the bottom of the spring seat adapter plate 19 penetrate through the frame-type beam 12 and are fastened at the bottom by self-locking nuts or double nuts.
Place the projectile body 2 on the 1 subassembly of a, b two places bullet support, and the fulcrum position needs to be unanimous with the 1 fulcrum position of projectile body, because projectile body 2 directly places and can have the rotation on the 1 subassembly of bullet support, need twine sack 5 on the surface of projectile body 2, pull out quick-release spring catch 3, adjust hasp ring nut 20, make it closely detain mutually with couple board 8, promote hasp handle 11 downwards, make couple board 8 closely detain mutually with hasp ring nut 20, let antistatic rubber 10 on the sack 5 and 2 surface contact of projectile body, increase frictional force, insert quick-release spring catch 3, prevent the rotation of projectile body.
The present invention is not described in detail in the prior art.
The above description is only a preferred embodiment of the present invention, and should not be taken as limiting the invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (9)

1. A supporting and fixing device for guided missiles and bombs comprises a missile support (1) and a frame-type beam (12), and is characterized in that the frame-type beam (12) is provided with a positioning hole (13), the missile support (1) is integrally fixed in the positioning hole (13), the bottom of the missile support (1) is provided with a missile seat adapter plate (19) and a plurality of positioning pins (15), the positioning pins (15) are inserted into the frame-type beam (12), and the bottom of the missile seat adapter plate (19) is connected with the frame-type beam (12) through a connecting piece (14);
the bullet support (1) both sides are equipped with bullet seat couple board (8) and hasp lock (9) of mutually supporting connection for fix place bullet body (2) at bullet support roller components (6) top.
2. A missile and bomb supporting and fixing device as claimed in claim 1, wherein the missile seat hook plate (8) and the hasp lock (9) are respectively fixed on both sides of the missile support seat (1) through a canvas pressing plate (4) and a canvas (5).
3. A missile and bomb supporting and fixing device as claimed in claim 2, wherein the canvas bag pressing plate (4) is provided with an antistatic rubber (10) at the middle position.
4. A missile and bomb supporting and fixing device as claimed in claim 1, characterised in that the hasp lock (9) is provided with a hasp handle (11) and a spring pin (3).
5. Missile and bomb supporting and fixing device according to claim 1, characterised in that the connecting piece (14) is a bolt and a self-locking nut or a double nut which are connected in a matching way.
6. A missile and bomb support fixing device in accordance with any one of claims 1 to 5 characterised in that the missile support (1) is provided with snap locks on both the front and back sides.
7. The missile and bomb supporting and fixing device as claimed in claim 6, wherein the hasp lock comprises a hasp base (18) and a hasp handle (11) fixed on the hasp base (18), and the hasp base (18), the hasp handle (11) and a hook T-shaped stud (17) are coaxially connected through a fastening bolt below the hasp base (18); and a hook ring nut (20) and a second hook plate (16) are sequentially connected below the hook T-shaped stud (17).
8. A missile and bomb supporting and fixing device as claimed in claim 7, wherein the hook T-shaped stud (17) is connected with the pin washer and the hasp handle (11) through a pin shaft, and the hook T-shaped stud (17) rotates within an effective range.
9. The missile and bomb supporting and fixing device as claimed in claim 7, wherein the hasp base (18) is connected with a hasp adapter plate or a door plate fixing plate through a countersunk screw, and a canvas bag adapter plate is additionally arranged in the middle of the hasp base (18) and the hasp adapter plate when the hasp base is fixed.
CN202120025330.1U 2021-01-06 2021-01-06 Supporting and fixing device for guided missile and bomb Active CN214470421U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120025330.1U CN214470421U (en) 2021-01-06 2021-01-06 Supporting and fixing device for guided missile and bomb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120025330.1U CN214470421U (en) 2021-01-06 2021-01-06 Supporting and fixing device for guided missile and bomb

Publications (1)

Publication Number Publication Date
CN214470421U true CN214470421U (en) 2021-10-22

Family

ID=78138525

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120025330.1U Active CN214470421U (en) 2021-01-06 2021-01-06 Supporting and fixing device for guided missile and bomb

Country Status (1)

Country Link
CN (1) CN214470421U (en)

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GR01 Patent grant
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CP03 Change of name, title or address

Address after: 253000 workshop 2, north yard, intersection of Tianqu East Road and Chongde Sixth Avenue, Yuanqiao Town, Dezhou Economic Development Zone, Shandong Province

Patentee after: Shandong Jukai New Material Co.,Ltd.

Address before: 253000 workshop 2, north yard, intersection of Tianqu East Road and Chongde Sixth Avenue, Yuanqiao Town, Dezhou Economic and Technological Development Zone, Shandong Province

Patentee before: Shandong Jukai Civil Air Defense Engineering Co.,Ltd.

CP03 Change of name, title or address