CN218764907U - Bullet support frame suitable for different model guided missiles - Google Patents

Bullet support frame suitable for different model guided missiles Download PDF

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Publication number
CN218764907U
CN218764907U CN202222936327.2U CN202222936327U CN218764907U CN 218764907 U CN218764907 U CN 218764907U CN 202222936327 U CN202222936327 U CN 202222936327U CN 218764907 U CN218764907 U CN 218764907U
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slide rail
jack
missiles
layer board
lifting
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CN202222936327.2U
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Chinese (zh)
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杨发开
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Chengdu Meilan Electronic Instrument Co ltd
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Chengdu Meilan Electronic Instrument Co ltd
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Abstract

The utility model discloses a support bullet frame suitable for different model guided missiles, including holding in the palm bullet frame body, it includes bar slide rail, two layer boards, jack, connecting seat and lift adjustment mechanism to hold in the palm bullet frame body, two layer boards and bar slide rail sliding connection, two layer board opposite sides are equipped with curved support groove, two layer board below are equipped with the jack, the flexible end and the layer board bottom surface of jack are connected, the stiff end and another layer board bottom surface of jack are connected, two layer board intervals of the flexible adjustment of jack, bar slide rail both ends are equipped with the bracing piece, the bracing piece lower extreme is connected with the connecting seat, the connecting seat is fixed in on the lift adjustment mechanism, the lift adjustment mechanism lower extreme is fixed with the base. The utility model discloses can adjust the interval of two layer boards through the jack, this interval can be adjusted according to the guided missile overall dimension, can be used for depositing of different model guided missiles.

Description

Bullet support frame suitable for different model guided missiles
Technical Field
The utility model relates to a guided missile holds in palm bullet frame technical field, concretely relates to hold in palm bullet frame suitable for different model guided missiles.
Background
The missile bracket belongs to ground guarantee equipment special for a missile weapon system and is used for temporarily storing missiles, and the existing missile bracket generally comprises a support 1', a lifting adjusting mechanism 2' and a connecting seat 3', as shown in figure 3. The support 1 'is manufactured according to the shape of the missile, when the missile lifting device works, the missile is lifted to a missile bracket, and the missile supporting surface is arranged on the support 1'. According to the size of the missile, 2-3 brackets shown in figure 3 are usually needed for supporting one missile, and because the front and back shapes of the missile are different, the shape of a bracket 1' for supporting the same missile is changed, so that the shapes of the front bracket, the middle bracket and the back bracket for supporting the same missile are different. The missile bracket in the form has low utilization rate, the shapes of different types of missiles are different, and the missile bracket must be independently developed for each type of missile. Therefore, it is necessary to provide a new technical solution to solve the above problems
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a hold in palm bullet frame suitable for different model guided missiles, this holds in palm bullet frame and supplies the guided missile of different models general.
In order to solve the technical problem, the utility model discloses a following scheme:
the utility model provides a hold in palm bullet frame suitable for different model missiles, including holding in the palm bullet frame body, it includes bar slide rail, two layer boards, the jack, connecting seat and lifting adjusting mechanism to hold in the palm bullet frame body, two layer boards and bar slide rail sliding connection, two layer board opposite sides are equipped with curved support groove, two layer board below are equipped with the jack, the flexible end and the layer board bottom surface of jack are connected, the stiff end and another layer board bottom surface of jack are connected, the two layer board intervals of the flexible adjustment of jack, bar slide rail both ends are equipped with the bracing piece, the bracing piece lower extreme is connected with the connecting seat, the connecting seat is fixed in on the lifting adjusting mechanism, the lifting adjusting mechanism lower extreme is fixed with the base.
Optionally, the cross section of the bar-shaped slide rail is rectangular, a rectangular through hole allowing the bar-shaped slide rail to pass through is formed in the side face of the supporting plate along the length direction of the supporting plate, the bar-shaped slide rail penetrates through the rectangular through hole, and the telescopic end of the jack stretches and retracts to enable the two supporting plates to move on the bar-shaped slide rail, so that a space meeting the appearance of a guided missile is formed.
Optionally, the strip-shaped slide rail is arranged in a hollow manner.
Optionally, the surface of the strip-shaped slide rail is coated with a wear-resistant layer made of polytetrafluoroethylene.
Optionally, the bottom surfaces of the two supporting plates are provided with mounting plates for fixing the jack.
Optionally, the support rod is arranged obliquely, and the support rod and the strip-shaped slide rail form a triangular structure.
Optionally, the lifting adjusting mechanism comprises an adjusting hand wheel, a lifting outer tube and a lifting inner tube, the adjusting hand wheel is fixed on the lifting outer tube, and the lifting outer tube is in threaded connection with the lifting inner tube.
Optionally, the connecting seat is fixed in the center of an adjusting hand wheel of the lifting adjusting mechanism.
The utility model discloses beneficial effect who has:
1. the utility model discloses the commonality is high, does not need to develop new support missile rack specially to the guided missile of different models, and guided missile in the certain overall dimension within range can general this support missile rack. The adjusting mode of the distance between the supporting plates is simple and reliable, the whole structure is simple, and the practicability is high.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a pallet;
fig. 3 is a schematic structural diagram of the prior art.
Reference numerals: 1-supporting plate, 2-strip-shaped sliding rail, 3-supporting rod, 4-connecting seat, 5-adjusting hand wheel, 6-adjusting outer tube, 7-adjusting inner tube, 8-base, 9-jack, 10-mounting plate, 11-bracket and 12-rectangular through hole.
Detailed Description
The present invention will be described in further detail with reference to the following examples and drawings, but the present invention is not limited thereto.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "longitudinal", "lateral", "horizontal", "inner", "outer", "front", "rear", "top", "bottom", and the like indicate the position or positional relationship based on the position or positional relationship shown in the drawings, or the position or positional relationship which is usually placed when the product of the present invention is used, and the terms are only for convenience of description of the present invention and simplifying the description, but do not indicate or imply that the device or element to which the term refers must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.
In the description of the present invention, it should be further noted that, unless otherwise explicitly specified or limited, the terms "disposed," "opened," "mounted," "connected," and "connected" are to be construed broadly, e.g., as either a fixed connection, a detachable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood as a specific case by those skilled in the art.
Example 1
The utility model provides a hold in palm bullet frame suitable for different model missiles, including holding in the palm bullet frame body, it includes bar slide rail 2 to hold in the palm bullet frame body, two layer boards 1, jack 9, connecting seat 4 and lift adjustment mechanism, two layer boards 1 and 2 sliding connection of bar slide rail, 1 opposite side of two layer boards is equipped with curved support groove 11, 1 below of two layer boards is equipped with jack 9, jack 9's flexible end is connected with 1 bottom surface of a layer board, jack 9's stiff end is connected with 1 bottom surface of another layer board, two layer board 1 intervals of the flexible adjustment of jack 9, 2 both ends of bar slide rail are equipped with bracing piece 3, 3 lower extremes of bracing piece are connected with connecting seat 4, connecting seat 4 is fixed in on the lift adjustment mechanism, the lift adjustment mechanism lower extreme is fixed with base 8.
As shown in figure 1, the utility model discloses carry out the change of plane design to former guided missile bracket, design the support of guided missile bracket into adjustable, adjust the distance between two layer boards 1 through the flexible end of jack 9, this distance can be adjusted according to guided missile overall dimension, can be used for depositing of multiple model guided missile, carry out the adaptability according to different guided missile appearances and sizes and adjust to reach the purpose that same support missile rack is applicable to multiple model guided missile; the bracket 11 on the supporting plate 1 is in a quarter arc shape, and because the missile is basically in a cylindrical structure, the arc-shaped bracket 11 can be matched with the side surface of the missile better, so that the stability of the missile when the missile is placed on the missile supporting frame is higher, and sponge or rubber pads can be arranged in the bracket 11 to prevent the missile from playing a role in protection.
Furthermore, the cross section of the bar-shaped slide rail 2 is rectangular, a rectangular through hole 12 allowing the bar-shaped slide rail 2 to pass through is formed in the side face of the supporting plate 1 along the length direction of the supporting plate, the bar-shaped slide rail 2 penetrates through the rectangular through hole 12, and the telescopic end of the jack 9 stretches to enable the two supporting plates 1 to move on the bar-shaped slide rail 2, so that a space meeting the appearance of a guided missile is formed. Specifically, as shown in fig. 1 and 2, a rectangular bar-shaped slide rail 2 is adopted, so that the support plate 1 cannot rotate when sliding on the bar-shaped slide rail 2, a limiting effect is achieved, in order to adjust the distance between the two support plates 1, guided missiles conforming to the sizes of all shapes are obtained, the telescopic end of the jack 9 extends out, the two support plates 1 are relatively far away from the bar-shaped slide rail 2, the distance meeting the shapes of the guided missiles is formed, and the guided missiles are placed in the support grooves 11 of the two support plates 1.
Further, the strip-shaped slide rail 2 is arranged in a hollow manner. Specifically, the strip-shaped slide rail 2 is arranged in a hollow mode, and the weight of the bullet supporting frame can be reduced.
Furthermore, the surface of the strip-shaped slide rail 2 is coated with a wear-resistant layer made of polytetrafluoroethylene. The wearing layer can strengthen the wear resistance of the strip-shaped slide rail 2 and prolong the service life of the strip-shaped slide rail 2.
Further, the bottom surfaces of the two supporting plates 1 are provided with mounting plates 10 for fixing the jacks 9. Specifically, the mounting plates 10 are vertically and vertically welded on the bottom surface of the supporting plate 1, one mounting plate 10 at the telescopic end of the jack 9 is fixedly connected, and the fixed end of the jack 9 is connected with the other mounting plate 10 through a bolt.
Furthermore, the support rod 3 is obliquely arranged, and the support rod 3 and the strip-shaped slide rail 2 form a triangular structure. Bracing piece 3 is equipped with two, and two bracing pieces 3 are V-arrangement structural distribution, and the upper end and the welding of bar slide rail 2 of bracing piece 3, lower extreme and connecting seat 4 welding, the vertical bearing capacity of bullet frame can be improved to three horn shaped structure, and stability is higher.
Example 2
Further, lift adjustment mechanism includes adjusting hand wheel 5, lift outer tube 6 and lift inner tube 7, adjusting hand wheel 5 is fixed in on the lift outer tube 6, lift outer tube 6 and lift inner tube 7 threaded connection.
Furthermore, the connecting seat 4 is fixed in the center of an adjusting hand wheel 5 of the lifting adjusting mechanism.
In this embodiment, the connecting seat 4 is fixed at the center of the adjusting hand wheel 5 of the lifting adjusting mechanism, and the center of the adjusting hand wheel 5 is rotated, so that the lifting outer tube 6 and the lifting inner tube 7 can vertically move relatively, and further the height of the whole bullet supporting frame can be adjusted, and in the lifting process of the lifting adjusting mechanism, the two supporting plates 1 can be adjusted to ascend together with the strip-shaped slide rail 2, the supporting rod 3 and the jack 9, so that the requirement of supporting various missiles is met.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way, and the technical essence of the present invention is that within the spirit and principle of the present invention, any simple modification, equivalent replacement, and improvement made to the above embodiments are all within the protection scope of the technical solution of the present invention.

Claims (8)

1. The utility model provides a hold in palm bullet frame suitable for different model guided missiles, including holding in the palm bullet frame body, a serial communication port, it includes bar slide rail (2), two layer boards (1), jack (9), connecting seat (4) and lifting adjusting mechanism to hold in the palm bullet frame body, two layer boards (1) and bar slide rail (2) sliding connection, two layer board (1) opposite sides are equipped with curved support groove (11), two layer board (1) below is equipped with jack (9), the flexible end and a layer board (1) bottom surface of jack (9) are connected, the stiff end and another layer board (1) bottom surface of jack (9) are connected, two layer board (1) interval of jack (9) flexible adjustment, bar slide rail (2) both ends are equipped with bracing piece (3), bracing piece (3) lower extreme is connected with connecting seat (4), connecting seat (4) are fixed in on the lifting adjusting mechanism, the lifting adjusting mechanism lower extreme is fixed with base (8).
2. The missile supporting frame suitable for missiles of different models as claimed in claim 1, wherein the cross section of the strip-shaped slide rail (2) is rectangular, a rectangular through hole (12) allowing the strip-shaped slide rail (2) to pass through is formed in the side surface of the supporting plate (1) along the length direction of the supporting plate, the strip-shaped slide rail (2) passes through the rectangular through hole (12), and the telescopic end of the jack (9) is telescopic to enable the two supporting plates (1) to move on the strip-shaped slide rail (2) so as to form a space meeting the appearance of a missile.
3. The cartridge holder suitable for different types of missiles as claimed in claim 2, wherein the strip-shaped slide rail (2) is hollow.
4. The support for different types of missiles as claimed in claim 3, wherein the surface of the strip-shaped slide rail (2) is coated with a wear-resistant layer made of polytetrafluoroethylene.
5. A support for different types of missiles according to claim 2, wherein the bottom surfaces of the two support plates (1) are provided with mounting plates (10) for fixing the jacks (9).
6. The missile support frame suitable for missiles of different models according to claim 1, wherein the support rods (3) are obliquely arranged, and the support rods (3) and the strip-shaped slide rails (2) form a triangular structure.
7. The missile supporting frame suitable for missiles of different models as claimed in claim 1, wherein the lifting adjusting mechanism comprises an adjusting hand wheel (5), a lifting outer tube (6) and a lifting inner tube (7), the adjusting hand wheel (5) is fixed on the lifting outer tube (6), and the lifting outer tube (6) is in threaded connection with the lifting inner tube (7).
8. The cartridge holder suitable for missiles of different models according to claim 1, wherein the connecting seat (4) is fixed at the center of an adjusting hand wheel (5) of a lifting adjusting mechanism.
CN202222936327.2U 2022-11-04 2022-11-04 Bullet support frame suitable for different model guided missiles Active CN218764907U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222936327.2U CN218764907U (en) 2022-11-04 2022-11-04 Bullet support frame suitable for different model guided missiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222936327.2U CN218764907U (en) 2022-11-04 2022-11-04 Bullet support frame suitable for different model guided missiles

Publications (1)

Publication Number Publication Date
CN218764907U true CN218764907U (en) 2023-03-28

Family

ID=85645396

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202222936327.2U Active CN218764907U (en) 2022-11-04 2022-11-04 Bullet support frame suitable for different model guided missiles

Country Status (1)

Country Link
CN (1) CN218764907U (en)

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