CN112696994A - Support assembly for guided missile and bomb - Google Patents
Support assembly for guided missile and bomb Download PDFInfo
- Publication number
- CN112696994A CN112696994A CN202110013270.6A CN202110013270A CN112696994A CN 112696994 A CN112696994 A CN 112696994A CN 202110013270 A CN202110013270 A CN 202110013270A CN 112696994 A CN112696994 A CN 112696994A
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- Prior art keywords
- hasp
- support
- plate
- missile
- bomb
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- 229920001971 elastomer Polymers 0.000 claims abstract description 15
- 238000003825 pressing Methods 0.000 claims abstract description 13
- 238000013016 damping Methods 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 239000000806 elastomer Substances 0.000 description 4
- 230000005611 electricity Effects 0.000 description 3
- 230000003068 static effect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to a support assembly 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 invention has the advantages of convenient and fast installation, safety and reliability and effectively improves the working efficiency.
Description
Technical Field
The invention belongs to the technical field of missile transportation process fixing, and particularly relates to a missile and a support assembly for a bomb, which is a simple, convenient and efficient fixing assembly suitable for a transportation working platform and a missile in a missile transportation process.
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 invention adopts the hasp for fixed connection, and the safety device adopts the quick-release spring pin, so that the looseness and the falling off of parts in the transportation process are improved. The device can also be applied to aviation missile-carrying guarantee equipment applied by the applicant (ZL201921213057.4), and can accurately, quickly and efficiently position the fulcrum position.
Disclosure of Invention
The invention aims to solve the problems and provides a support assembly for missiles and bombs, which is convenient and quick to install, safe and reliable and effectively improves the working efficiency.
In order to achieve the purpose, the invention provides the 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.
Further, the projectile hook plate is connected with a support side sailcloth bag pressing plate through a sailcloth bag, one end of the sailcloth bag pressing plate presses the sailcloth bag to be fixed on the side face of the support, and the other end of the projectile hook plate is mutually fastened and 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 invention has the beneficial effects that:
the invention has the advantages of convenient and fast installation, safety and reliability, and effectively improves the working 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 needed 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 creative efforts.
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 representation of the use 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 solutions of the present invention better understood and implemented by those skilled in the art, the present invention is further described with reference to the following specific examples, which are provided for 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 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, and the projectile hook plate 7 at the other end 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 invention has the advantages of convenient and fast installation, safety and reliability, and effectively improves the working 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 details of the present invention not described in detail are prior art.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
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 support assembly for missiles and bombs as claimed in claim 1, wherein the projectile hooking plate (7) is connected with the 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 the projectile hooking plate (7) at the other end is tightly connected with the hasp adapter plate (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110013270.6A CN112696994A (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 |
|---|---|---|---|
| CN202110013270.6A CN112696994A (en) | 2021-01-06 | 2021-01-06 | Support assembly for guided missile and bomb |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112696994A true CN112696994A (en) | 2021-04-23 |
Family
ID=75514891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110013270.6A Pending CN112696994A (en) | 2021-01-06 | 2021-01-06 | Support assembly for guided missile and bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112696994A (en) |
-
2021
- 2021-01-06 CN CN202110013270.6A patent/CN112696994A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
Address after: Workshop 2, Beiyuan Road, the intersection of Tianqu East Road and Chongde Sixth Avenue, Yuanqiao Town, Dezhou Economic Development Zone, Shandong Province Applicant 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 Applicant before: Shandong Jukai Civil Air Defense Engineering Co.,Ltd. |
|
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20210423 |