CN214620893U - Support assembly for guided missile and bomb - Google Patents
Support assembly for guided missile and bomb Download PDFInfo
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- CN214620893U CN214620893U CN202120025303.4U CN202120025303U CN214620893U CN 214620893 U CN214620893 U CN 214620893U CN 202120025303 U CN202120025303 U CN 202120025303U CN 214620893 U CN214620893 U CN 214620893U
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- hasp
- missile
- plate
- bomb
- support
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Abstract
The utility model relates to a support component for guided missiles and bombs, which comprises a bomb support, wherein a shaft end clamping plate is fixed above the bomb support through a roller shaft and a bearing, and a bomb seat adapter plate is arranged at the bottom of the bomb support; the two sides of the bullet support are respectively connected with a bullet hook plate and a third hasp lock through a canvas press plate, and a hasp adapter plate is arranged behind the third hasp lock; an anti-static rubber is arranged in the middle of the canvas bag pressing plate; the middle part of the elastic support is connected with the first/second hasp lock through a square through hole, the bottom part of the elastic support is connected with a fixed frame beam, and a fixed hook plate is arranged on the fixed frame beam. The first/second hasp locks are fixed on the hasp base, and the hasp handle is fixed on the hasp base through a spring pin. The upper part of the elastic support is provided with a U-shaped opening which is connected with the roller shaft and a clamping plate at the end of the roller shaft and is used for fixing the movement of the roller shaft in the left, right and lower directions; the roller shaft end clamping plate is used for limiting the axial movement and the upward movement of the roller shaft. The utility model has the advantages that, simple to operate is swift, and safe and reliable effectively improves work efficiency.
Description
Technical Field
The utility model belongs to the technical field of the guided missile transportation is fixed, concretely relates to guided missile and for bomb support subassembly is applicable to simple, convenient, the fixed subassembly of efficient of transportation work platform and guided missile in the guided missile transportation.
Background
Missile weaponry needs to be transported from production to arming troops, combat training and battlefield application, the transport environment influences the performance of the missile weaponry, and the quality of the equipment transport performance is necessarily related to the equipment reliability; the missile support in the prior art is supported by bolts, and runs on a bumpy road surface in different environments due to uncontrollable transportation road conditions, the rigid connection is connected by bolts, so that the phenomenon of screw loosening is easy to occur for a long time, potential safety hazards are caused to transported products, and damage to missiles or other parts is possible; the utility model discloses a hasp fixed connection, safeties adopt quick-release spring catch, have improved in the transportation not hard up of part, have come off. The device can also be applied to aviation missile-carrying guarantee equipment applied by the applicant (ZL 201921213057.4), and can accurately, quickly and efficiently position the fulcrum position.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the above problem, providing a support subassembly for guided missile and bomb, its simple to operate is swift, safe and reliable, effectual improvement work efficiency.
In order to achieve the above object, the utility model provides a following technical scheme:
a support assembly for guided missiles and bombs comprises a bomb support and is characterized in that a shaft end clamping plate is fixed above the bomb support through a roller shaft and a bearing, and a bomb base adapter plate is arranged at the bottom of the bomb support; the two sides of the bullet support are respectively connected with a bullet hook plate and a third hasp lock through a canvas press plate, and a hasp adapter plate is arranged behind the third hasp lock; an anti-static rubber is arranged in the middle of the canvas bag pressing plate;
the middle part of the elastic support is connected with the first/second hasp lock through a square through hole, the bottom of the elastic support is connected with a fixed frame beam, and a fixed hook plate is arranged on the fixed frame beam.
Furthermore, the first/second buckle locks are fixed on the buckle base, and the buckle handle is fixed on the buckle base through a spring pin.
Further, 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 hasp ring nut is connected below the hook T-shaped stud.
Furthermore, one end of the spring pin is connected with a spring pin pull ring, and the other end of the spring pin is provided with a limiting telescopic ball; the spring pin pull ring is connected with the hasp handle through a steel wire rope.
Furthermore, a roller damping ring is arranged between the shaft end clamping plate and the elastic support.
Furthermore, the bullet seat keysets passes through the countersunk screw to be fixed in bullet support bottom, and the bottom is fixed a position to embedded a plurality of locating pins in bullet support and bullet seat keysets middle.
Furthermore, a plurality of first positioning pins and second positioning pins are arranged below the spring seat adapter plate.
Further, the first/second snap locks are respectively fixed in front of and behind the spring support.
Furthermore, a U-shaped opening is formed above the elastic support, is connected with the roller shaft and a clamping plate at the end of the roller shaft and is used for fixing the roller shaft to move in the left direction, the right direction and the lower direction; the roller shaft end clamping plate is used for limiting the axial movement and the upward movement of the roller shaft.
Furthermore, the projectile body hook plate is connected with the sailcloth bag pressing plate through a sailcloth bag, one end of the projectile body hook plate is tightly pressed by the sailcloth bag pressing plate and fixed on the side face of the projectile support seat, and the other end of the projectile body hook plate is mutually and fixedly connected with the hasp adapter plate; and the hasp annular nut on the third hasp lock on the right side is buckled with the elastomer hook plate, and the hasp handle is pulled downwards, so that the hasp annular nut is tightly buckled with the elastomer hook plate.
Compared with the prior art, the beneficial effects of the utility model reside in that:
the utility model discloses simple to operate is swift, safe and reliable, effectual improvement work efficiency. The missile fixing support is superior to the prior art product in disassembly and assembly replacing time, the missile fixing support is in contact with the missile body, the high-strength sailcloth bag and the anti-static rubber sheet are adopted in a combined mode to replace the prior rigid contact related technology, the transportation safety of the missile body in the transportation process is effectively guaranteed, and the anti-static rubber sheet is arranged to avoid the influence on the precision of electronic elements in the missile body due to static electricity.
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 perspective view of the present invention;
FIG. 2 is a front view of the present invention;
fig. 3 is a side view of the present invention;
FIG. 4 is a schematic view of the present invention;
in the figure: 1-elastic support, 2-roller shaft, 3-bearing, 4-shaft end clamping plate, 5-roller damping ring, 6-canvas bag pressing plate, 7-elastic hook plate, 8-hasp adapter plate, 9-third hasp lock, 10-first/second hasp lock, 11-hasp handle, 12-spring pin, 13-hook T-shaped stud, 14-hasp ring nut, 15-second locating pin, 16-fixed frame beam, 17-fixed hook plate, 18-first locating pin, 19-elastic support adapter plate and 20-antistatic rubber.
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 support assembly shown in fig. 1-3 comprises a bomb support 1, wherein a shaft end clamping plate 4 is fixed above the bomb support 1 through a roller shaft 2 and a bearing 3, and a bomb seat adapter plate 19 is arranged at the bottom of the bomb support 1; and a roller damping ring 5 is arranged between the shaft end clamping plate 4 and the elastic support 1. The two sides of the bullet support 1 are respectively connected with a bullet hook plate 7 and a third hasp lock 9 through a canvas press plate 6, and a hasp adapter plate 8 is arranged behind the third hasp lock 9; an anti-static rubber sheet 20 is arranged in the middle of the canvas bag pressing plate 6;
the middle positions of the front and the back of the elastic support 1 are connected with a first/second hasp lock 10 through square through holes, the bottom of the elastic support is connected with a fixed frame beam 16, and a fixed hook plate 17 is arranged on the fixed frame beam 16. The first/second hasp locks 10 are fixed on a hasp base, and a hasp handle 11 is fixed on the hasp base through a spring pin 12; one end of the spring pin 12 is connected with a spring pin pull ring, and the other end of the spring pin is provided with a limiting telescopic ball; the spring pin pull ring is connected with the hasp handle 11 through a steel wire rope. The hasp base, the hasp handle 11 and the hook T-shaped stud 13 are coaxially connected through a fastening bolt below the hasp base; and a hasp ring nut 14 is connected below the hook T-shaped stud 13.
The bullet seat keysets 19 pass through the countersunk screw to be fixed in bullet support 1 bottom, and inlay a plurality of locating pins in bullet support 1 and bullet seat keysets 19 middle and fix a position in the bottom. A plurality of first positioning pins 18 and second positioning pins 15 are arranged below the spring seat adapter plate 19.
The upper part of the elastic support 1 is provided with a U-shaped opening which is connected with the roller shaft 2 and a roller shaft end clamping plate 4 and used for fixing the roller shaft 2 to move in the left, right and lower directions; the roller shaft end clamping plate 4 is used for limiting the axial movement and the upward movement of the roller shaft 2.
The projectile hook plate 7 is connected with the sailcloth bag pressing plate 6 through a sailcloth bag, one end of the projectile hook plate 7 is tightly pressed by the sailcloth bag pressing plate 6 and fixed on the side surface of the projectile support 1, and the other end of the projectile hook plate 7 is mutually and fixedly connected with the hasp adapter plate 8; the snap ring nut 14 on the third snap lock 9 on the right snaps on the elastic hook plate 7, and the snap handle 11 is pulled downward, so that the snap ring nut 14 is tightly snapped on the elastic hook plate 7.
Connect bullet seat keysets 19 under the bullet support 1, use countersunk screw fastening to 4 first locating pins 18 and 1 second locating pin 15 are embedded in bullet support 1 and bullet seat keysets 19 middle, 5 locating pins play the positioning action in the bottom. The relative position size corresponds one-to-one to the fixed hole size on the fixed frame cross member 16.
As shown in fig. 4, a set of hasp locks are respectively installed on the front and back surfaces of the elastic support 1, the hasp locks are fixed by using countersunk screws, the quick-release spring pins 12 are taken down, the hasp handles 11 are rotated to buckle the hasp ring nuts 14 on the fixed hook plates 17, then the hasp handles 11 are pushed upwards to ensure that the hasp ring nuts 14 are firmly buckled with the fixed hook plates 17 in the process of pushing the hasp upwards, if the hasp ring nuts 14 are loosened, the hasp ring nuts 14 are rotated clockwise to reduce the distance between the hasp ring nuts and the T-shaped studs 13 of the hooks, and vice versa, the hasp handles 11 are pushed upwards again, at the moment, the hasp ring nuts 14 are firmly buckled with the fixed hook plates 17, the quick-release spring pins 12 are inserted into corresponding holes of the hasp bases, and the hasp handles 11 are ensured not to fall off reversely due to the jolt of the road surface.
The U-shaped opening on the elastic support 1 is connected with the roller shaft 2 and the roller shaft end clamping plate 4, and the roller shaft end clamping plate 4 limits the axial movement and the upward movement of the roller shaft 2 in order to fix the three-direction movement of the roller shaft 2, namely, the left, right and lower directions. The roller is internally provided with a needle bearing 3, so that the roller shaft 2 can only rotate along the axis.
As shown in fig. 4, the contact between the projectile body and the seat assembly is point contact, i.e. tangential contact, and the projectile body can rotate without being bound.
In the upper part of the support assembly, a projectile hook plate 7 is connected with a support side sailcloth bag pressing plate 6 through a sailcloth bag, the sailcloth bag pressing plate 6 at one end is tightly pressed on the side surface of the support and is fixed on the side surface of the support, the projectile hook plate 7 at the other end is mutually and fixedly connected with a hook plate adapter plate (namely a hasp adapter plate 8), the sailcloth bag is mixed in the projectile hook plate, and an anti-static rubber sheet 20 with a certain size is placed in the middle of the sailcloth bag to prevent static electricity; the snap ring nut 14 on the third snap lock 9 on the right snaps on the elastomer hook plate 7, and the snap handle 11 is pulled downward, so that the snap ring nut 14 is tightly snapped on the elastomer hook plate 7. The friction force of the bullet body due to the antistatic rubber 20 is increased, and the rotation freedom degree of the bullet body is limited.
The utility model discloses simple to operate is swift, safe and reliable, effectual improvement work efficiency. The missile fixing support is superior to the prior art product in disassembly and assembly replacing time, the missile fixing support is in contact with the missile body, the high-strength sailcloth bag and the anti-static rubber sheet are adopted in a combined mode to replace the prior rigid contact related technology, the transportation safety of the missile body in the transportation process is effectively guaranteed, and the anti-static rubber sheet is arranged to avoid the influence on the precision of electronic elements in the missile body due to static electricity.
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 (10)
1. A support assembly for guided missiles and bombs comprises a bomb support (1) and is characterized in that a shaft end clamping plate (4) is fixed above the bomb support (1) through a roller shaft (2) and a bearing (3), and a bomb seat adapter plate (19) is arranged at the bottom of the bomb support (1); the two sides of the bullet support (1) are respectively connected with a bullet hook plate (7) and a third hasp lock (9) through a canvas press plate (6), and a hasp adapter plate (8) is arranged behind the third hasp lock (9); an anti-static rubber (20) is arranged in the middle of the canvas bag pressing plate (6);
the middle part of the elastic support (1) is connected with a first/second hasp lock (10) through a square through hole, the bottom part of the elastic support is connected with a fixed frame beam (16), and a fixed hook plate (17) is arranged on the fixed frame beam (16).
2. A missile and bomb seat assembly as claimed in claim 1 in which the first and second snap locks (10) are secured to a snap base to which a snap handle (11) is secured by a spring pin (12).
3. The missile and bomb seat assembly of claim 2, wherein the hasp base, hasp handle (11) and hook T-shaped stud (13) are coaxially connected through fastening bolt below the hasp base; and a hasp ring nut (14) is connected below the hook T-shaped stud (13).
4. The mount assembly for missiles and bombs as set forth in claim 2, wherein the spring pin (12) is connected to a spring pin pull ring at one end and provided with a limiting retractable ball at the other end; the spring pin pull ring is connected with a hasp handle (11) through a steel wire rope.
5. A missile and bomb seat assembly as claimed in claim 1 in which a roller damping ring (5) is provided between the axle end plate (4) and the missile seat (1).
6. The missile and bomb seat assembly of claim 1, wherein the missile seat adapter plate (19) is fixed at the bottom of the missile seat (1) through a countersunk head screw, and a plurality of positioning pins are embedded between the missile seat (1) and the missile seat adapter plate (19) to be positioned at the bottom.
7. Support assembly for missiles and bombs according to claim 1 or 6, characterized in that a plurality of first positioning pins (18) and second positioning pins (15) are provided below the cartridge adapter plate (19).
8. A missile and bomb seat assembly as claimed in claim 1 or claim 2 in which the first and second snap locks (10) are secured to the front and rear of the missile seat (1) respectively.
9. The missile and bomb seat assembly of claim 1, wherein a U-shaped opening is formed above the missile seat (1), connected with the roller shaft (2) and the roller shaft end clamping plate (4) and used for fixing the roller shaft (2) to move in left, right and lower directions; the roller shaft end clamping plate (4) is used for limiting the axial movement and the upward movement of the roller shaft (2).
10. The missile and bomb seat assembly of claim 1, wherein the missile hooking plate (7) is connected with the sailcloth bag pressing plate (6) through a sailcloth bag, one end of the missile hooking plate (7) is fixed on the side surface of the missile seat (1) through the sailcloth bag pressing plate (6) in a pressing mode, and the other end of the missile hooking plate (7) is mutually and fixedly connected with the hasp adapter plate (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120025303.4U CN214620893U (en) | 2021-01-06 | 2021-01-06 | Support assembly for guided missile and bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120025303.4U CN214620893U (en) | 2021-01-06 | 2021-01-06 | Support assembly for guided missile and bomb |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214620893U true CN214620893U (en) | 2021-11-05 |
Family
ID=78435629
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120025303.4U Active CN214620893U (en) | 2021-01-06 | 2021-01-06 | Support assembly for guided missile and bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214620893U (en) |
-
2021
- 2021-01-06 CN CN202120025303.4U patent/CN214620893U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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. |
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| CP03 | Change of name, title or address |