CN212931196U - Packing box body suitable for filling missiles with different diameters - Google Patents
Packing box body suitable for filling missiles with different diameters Download PDFInfo
- Publication number
- CN212931196U CN212931196U CN202020969802.4U CN202020969802U CN212931196U CN 212931196 U CN212931196 U CN 212931196U CN 202020969802 U CN202020969802 U CN 202020969802U CN 212931196 U CN212931196 U CN 212931196U
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- CN
- China
- Prior art keywords
- rod
- outer barrel
- barrel body
- strip
- packing box
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a packing box body suitable for filling missiles with different diameters, which comprises an outer barrel body and a base plate, and has the structural key points that a damping part is arranged in the outer barrel body, the damping part comprises a damping rod and a positioning part, the positioning part is formed by arranging at least three arc rods fixed with the damping rod around the central axis of the outer barrel body, the three arc rods are positioned on the same plane, a gap is formed between the end parts of the two adjacent arc rods, the outer barrel body is provided with strip-shaped openings which correspond to the gap and are parallel to the central axis of the outer barrel body, and the number of the strip-shaped openings is the same as that of the arc rods; the utility model has the advantages that: the guided missile of multiple diameter can be placed, the stability of placing of guided missile is not influenced simultaneously to need not to prepare the packing box of multiple specification, very big reduction packing cost.
Description
Technical Field
The utility model belongs to the equipment for packing field, concretely relates to be applicable packing box who loads different diameter guided missiles.
Background
The missile is a dangerous military product, and after being produced and manufactured by military factories, the general missile is put into a packaging box with a protection function and then is transported to a required unit.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a can be suitable for the packing box who loads different diameter guided missiles.
In order to realize the purpose, the technical proposal adopted by the utility model is that the packing box body suitable for filling missiles with different diameters comprises an outer barrel body and a base plate, and has the structural key points that a damping part is arranged in the outer barrel body, the damping part comprises a damping rod and a positioning part, the positioning part is composed of at least three arc rods fixed with the damping rod around the central axis of the outer barrel body, the three arc rods are positioned on the same plane, a gap is arranged between the end parts of the two adjacent arc rods, the outer barrel body is provided with strip-shaped openings which correspond to the gap and are parallel to the central axis of the outer barrel body, the number of the strip-shaped openings is the same as the number of the arc rods, each strip-shaped opening is internally and axially connected with a pressing rod which passes through the outer barrel body, the end part of the pressing rod positioned in the outer barrel body is hinged with a pressing plate, the outer end of the pressing rod positioned in the outer, the adjusting disc is provided with a threaded sleeve fixed with the lower end of the pull rod, a central hole is formed in the adjusting disc, and an adjusting rod which penetrates through the base plate and rotates to enable the adjusting disc to move longitudinally is matched in the central hole.
Furthermore, the outer end of the pressing rod is provided with extension plates positioned on two sides of the pull rod, and the extension plates are provided with strip-shaped sliding openings.
Furthermore, a sliding rod which is penetrated through by the strip-shaped sliding opening is arranged on the pull rod, and a blocking piece with the diameter larger than the width of the strip-shaped sliding opening is arranged at the tail end of the sliding rod.
Furthermore, the inner wall of the outer barrel body is provided with limiting baffle plates positioned at two sides of the pressing rod, and a limiting rod positioned above the pressing rod is arranged between the two limiting baffle plates.
Furthermore, a supporting column which is penetrated by the adjusting disc is arranged between the base plate and the lower end surface of the outer barrel body, and a central threaded hole which is used for matching the adjusting rod is arranged on the base plate.
Furthermore, the pressing plate is a strip plate with a curved section, and a silica gel layer is fixed on the curved surface of the pressing plate.
Further, the adjusting rod includes the screw rod body and clamping part, and the upper end of the screw rod body is equipped with the handheld dish that is located the top of adjusting disk, and the clamping part is including the pressure disk and the lower nut that hold in the palm of the top that are located the adjusting disk and below, pressure disk and the fixed connection of screw rod body.
Compared with the prior art, the beneficial effects of the utility model are that: the guided missile of multiple diameter can be placed, the stability of placing of guided missile is not influenced simultaneously to need not to prepare the packing box of multiple specification, very big reduction packing cost.
Drawings
Fig. 1 is a schematic sectional structure of the present invention;
FIG. 2 is a schematic top view of the outer tub of the present invention;
FIG. 3 is a schematic view of the structure of the pull rod of the present invention;
FIG. 4 is a schematic view of the shock-absorbing rod of the present invention;
FIG. 5 is a schematic view of the adjusting rod of the present invention;
the device comprises an outer barrel body 1, a base plate 2, a damping rod 3, a positioning part 4, an arc rod 5, an outer sleeve 6, an inserted rod 7, a compression spring 8, a strip-shaped opening 10, a compression rod 11, a compression plate 12, a silica gel layer 13, a pull rod 14, an adjusting plate 15, a threaded sleeve 16, a snap ring 17, a nut 18, a central hole 19, an adjusting rod 20, an extension plate 21, a strip-shaped sliding opening 22, a sliding rod 23, a baffle plate 24, a limit baffle 25, a limit rod 26, a support column 27, a central threaded hole 28, a plane protruding foot 29, a screw rod body 29, a hand-held plate 30, a pressure plate 31 and a lower support nut 32.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the protection scope of the present invention based on the embodiments of the present invention.
Referring to fig. 1 to 5, a packing box suitable for packing missiles of different diameters comprises an outer barrel body 1 and a base plate 2, wherein a damping part is arranged in the outer barrel body 1, the damping part comprises a damping rod 3 and a positioning part 4, the positioning part 4 is formed by arranging at least three arc rods 5 fixed with the damping rod 3 around the central axis of the outer barrel body 1, the three arc rods 5 are positioned on the same plane, a gap is formed between the end parts of two adjacent arc rods 5, the damping rod 3 comprises an outer sleeve 6 fixed with the inner wall of the outer barrel body 1, an inserting rod 7 fixed with the arc rods 5 is arranged in the outer sleeve 6, the tail end of the inserting rod 7 is connected with a compression spring 8 arranged in the outer sleeve 6, after the missiles are placed in the outer barrel body 1, the three arc rods 5 firstly carry out primary limiting, the outer barrel body 1 is provided with a bar-shaped opening 9 which corresponds to the gap and is parallel to the central axis of the outer barrel body, the number of the strip-shaped openings 9 is the same as that of the arc-shaped rods 5, a pressing rod 10 penetrating through the outer barrel body 1 is connected in each strip-shaped opening 9 in a shaft mode, a pressing plate 11 is hinged to the end portion, located in the outer barrel body 1, of each pressing rod 10, the section of each pressing plate 11 is a strip plate with a curved surface, a silica gel layer 12 is fixed on the curved surface of each pressing plate 11, the missile can be in a hoop holding state through the corresponding pressing plate 11, placing stability is improved, a pull rod 13 is hinged to the outer end, located at the outer barrel body 1, of each pressing rod 10, an adjusting disc 14 is arranged between each base plate 2 and the outer barrel body 1, a thread sleeve 15 fixed with the lower end of each pull rod 13 is arranged on each adjusting disc 14, external threads are arranged on the outer wall of each thread sleeve 15, a clamping ring 16 arranged close to the lower end is arranged on each pull rod 13, a nut 17 located above each, the adjusting disc 14 is provided with a central hole 18, the adjusting rod 19 which penetrates through the base plate 2 and rotates to enable the adjusting disc 14 to move longitudinally is matched in the central hole 18, when the adjusting disc 14 is controlled to move downwards through the adjusting rod 19, downward pulling force is applied to the pull rod 13, then the outer end of the pressing rod 10 moves downwards, the pressing rod 10 forms lever motion, the inner end of the pressing rod 10 moves upwards, so that the distance between the pressing plate 11 and the central axis of the outer barrel body 1 is gradually reduced, because the number of the strip-shaped openings 9 is the same as that of the arc-shaped rods 5, the number of the strip-shaped openings 9 is at least three, the pressing rod 10 penetrating through the outer barrel body 1 is axially connected in each strip-shaped opening 9, after the three pressing rods 10 are turned over simultaneously, the missile can be stably clamped through the pressing plate 11 at the inner end, and thus, even if the diameter of the missile is smaller than the inner diameter of the outer, the stability of the missile can be maintained.
The outer end of the pressing rod 10 is provided with extension plates 20 located on two sides of the pull rod 13, the extension plates 20 are provided with strip-shaped sliding openings 21, the pull rod 13 is provided with a sliding rod 22 penetrating through the strip-shaped sliding openings 21, the tail end of the sliding rod 22 is provided with a blocking piece 23 with a diameter larger than the width of the strip-shaped sliding openings 21, when the adjusting disc 14 moves up and down, the pulling rod 13 is driven to move up and down simultaneously, the sliding rod 22 moves in the strip-shaped sliding openings 21 at the moment, when the shaft joint of the sliding rod 22 and the pressing rod 10 and the strip-shaped opening 9 are located on the same horizontal plane, the pressing rod 10 is in a horizontal state, and the sliding rod 22 is higher than or lower than the shaft joint of the pressing rod 10, so that two ends of the pressing rod 10 can be moved, and the.
In addition, be equipped with the limit baffle 24 that is located the both sides of compressing tightly pole 10 on the inner wall of outer staving 1, be equipped with the gag lever post 25 that is located the top that compresses tightly pole 10 between two limit baffle 24, can restrict the motion track of compressing tightly pole 10 when the upset through limit baffle 24's setting, avoid taking place the condition of incline upset, and the setting of gag lever post 25 can form the biggest flip angle who compresses tightly pole 10, when compressing tightly pole 10 and gag lever post 25 counterbalance, compressing tightly pole 10 is the horizontality, and when compressing tightly pole 10 is the horizontality, the distance of the central axis of the outer staving 1 of pressure strip 11 is the minimum diameter of the guided missile who is suitable for promptly.
A supporting column 26 penetrated by the adjusting disc 14 is arranged between the base plate 2 and the lower end surface of the outer barrel body 1, a central threaded hole 27 matched with the adjusting rod 19 is arranged on the base plate 2, and a plane protruding foot 28 in an annular array is arranged on the lower surface of the base plate 2, so that the base plate 2 can form a certain interval with the ground when being placed, the adjusting rod 19 comprises a screw rod body 29 and a clamping part, after the screw rod body 29 penetrates through a central hole 18 on the adjusting disc 14, the lower end of the screw rod body 29 is screwed with the central threaded hole 27 on the base plate 2, a hand-holding disc 30 positioned above the adjusting disc 14 is arranged at the upper end of the screw rod body 29, the screw rod body 29 can be driven to rotate by the rotation of the hand-holding disc 30, the clamping part comprises a pressure disc 31 and a lower support nut 32 positioned above and below the adjusting disc 14, the pressure disc 31 is fixedly connected with the screw rod body 29, and the adjusting disc 14, there is also a gap between the lower supporting nut 32 and the adjusting disk 14, so that when the screw body 29 rotates, the adjusting disk 14 can be driven to move up and down, and the pressing plate 11 at the inner end of the pressing rod 10 can clamp missiles with different diameters.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein, and any reference signs in the claims are not intended to be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (7)
1. The utility model provides an applicable packing box who loads different diameter missiles, includes outer staving and bed plate, its characterized in that: the damping part is arranged in the outer barrel body and comprises damping rods and a positioning part, the positioning part is formed by arranging at least three arc-shaped rods fixed with the damping rods around the central axis of the outer barrel body, the three arc-shaped rods are positioned on the same plane, a gap is formed between the end parts of two adjacent arc-shaped rods, the outer barrel body is provided with strip-shaped openings which correspond to the gaps and are parallel to the central axis of the outer barrel body, the number of the strip-shaped openings is the same as that of the arc-shaped rods, each strip-shaped opening is internally and axially connected with a pressing rod which penetrates through the outer barrel body, the end part of the pressing rod, which is positioned in the outer barrel body, is hinged with a pressing plate, the outer end of the pressing rod, which is positioned in the outer barrel body, is hinged with a pull rod, the base plate and the outer barrel body between be equipped with the adjustment disk, be equipped with the thread bush fixed with the lower extreme of pull rod on the adjustment disk, be equipped with the centre bore on the adjustment disk and in the centre bore match have with the base plate pass and rotate the back make the adjustment disk carry out longitudinal movement's adjusting lever.
2. A packing box suitable for loading missiles of different diameters as claimed in claim 1, wherein: the outer end of the pressing rod is provided with extension plates positioned on two sides of the pull rod, and the extension plates are provided with strip-shaped sliding openings.
3. A packing box suitable for loading missiles of different diameters as claimed in claim 2, wherein: the pull rod is provided with a slide rod which is penetrated through by the strip-shaped sliding opening, and the tail end of the slide rod is provided with a baffle sheet with the diameter larger than the width of the strip-shaped sliding opening.
4. A packing box suitable for loading missiles of different diameters as claimed in claim 1, wherein: the inner wall of the outer barrel body is provided with limiting baffle plates positioned at two sides of the pressing rod, and a limiting rod positioned above the pressing rod is arranged between the two limiting baffle plates.
5. A packing box suitable for loading missiles of different diameters as claimed in claim 1, wherein: the support column that is passed by the adjustment disk is equipped with between the lower terminal surface of bedplate and outer staving, be equipped with the central screw hole that is used for matcing the adjusting lever on the bedplate.
6. A packing box suitable for loading missiles of different diameters as claimed in claim 1, wherein: the pressing plate is a strip plate with a curved section, and a silica gel layer is fixed on the curved surface of the pressing plate.
7. A packing box suitable for loading missiles of different diameters as claimed in claim 1, wherein: the adjusting rod comprises a screw rod body and a clamping part, a hand-held disc located above the adjusting disc is arranged at the upper end of the screw rod body, the clamping part comprises a pressure plate and a lower support nut located above and below the adjusting disc, and the pressure plate is fixedly connected with the screw rod body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020969802.4U CN212931196U (en) | 2020-06-01 | 2020-06-01 | Packing box body suitable for filling missiles with different diameters |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020969802.4U CN212931196U (en) | 2020-06-01 | 2020-06-01 | Packing box body suitable for filling missiles with different diameters |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212931196U true CN212931196U (en) | 2021-04-09 |
Family
ID=75318911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020969802.4U Expired - Fee Related CN212931196U (en) | 2020-06-01 | 2020-06-01 | Packing box body suitable for filling missiles with different diameters |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212931196U (en) |
-
2020
- 2020-06-01 CN CN202020969802.4U patent/CN212931196U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210409 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |