CN209427378U - A kind of guided missile Quick clamping bracket suitable in missile packing box - Google Patents
A kind of guided missile Quick clamping bracket suitable in missile packing box Download PDFInfo
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- CN209427378U CN209427378U CN201822199964.XU CN201822199964U CN209427378U CN 209427378 U CN209427378 U CN 209427378U CN 201822199964 U CN201822199964 U CN 201822199964U CN 209427378 U CN209427378 U CN 209427378U
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- guided missile
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Abstract
It includes pedestal and briquetting that the utility model, which discloses a kind of guided missile Quick clamping bracket suitable in missile packing box, and briquetting is divided into the first briquetting and the second briquetting；Pedestal top is provided with first end face structure and second end face structure；The first bottom surface structure and first end face structure of first briquetting are hinged by the first bindiny mechanism；The second bottom surface structure and second end face structure of second briquetting are hinged by the second bindiny mechanism；First briquetting is fixedly connected with the second briquetting by third bindiny mechanism；First briquetting, the second briquetting and pedestal form a cylindrical cavity for accommodating guided missile.Guided missile can be firmly secured in missile packing box by the bracket；And the supporting structure is simple, provides convenience to place guided missile and taking out the operation of guided missile.
Description
Technical field
The utility model relates to missile packaging field more particularly to a kind of fast quick-mountings of guided missile suitable in missile packing box
Press from both sides bracket.
Background technique
As shown in Figure 1 to Figure 2, the guided missile Quick clamping bracket in existing missile packing box includes pedestal and briquetting, pressure
The thickness of block is less than the thickness of pedestal, and the middle part that briquetting is mounted on pedestal forms symmetrical four boss all around, each convex
A fixed block is provided on platform.It is logical that a fixed block through fixed block upper and lower surface is provided on each fixed block
Hole, threaded hole is provided on base top surface, and bolt passes through the threaded hole on fixed block through-hole and pedestal, fixed block is fixed on bottom
On seat.The sidewall bottom of fixed block towards briquetting has a groove corresponding with the protrusion of briquetting bottom, so that briquetting and fixed block
It is connected together, so that briquetting and pedestal are secured together.
The shortcomings that above structure is first, and fixed block is easily lost, and causes briquetting that can not securely connect with pedestal；Second,
The connection structure of briquetting and pedestal is complicated, increases the operation activity duration placed guided missile and take out guided missile, it is difficult to reach quick
The target call for ensureing, fighting；The connection needs of third, briquetting and pedestal are tightened or are loosered a bolt by tool, are unfavorable for
Guided missile is taken anywhere or anytime.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of guided missile quick-clampings suitable in missile packing box
Guided missile can be firmly secured in missile packing box by bracket, the bracket；And the supporting structure is simple, to place guided missile and taking
The operation of guided missile is provided convenience out.
In order to solve the above-mentioned technical problem, a kind of guided missile quick-clamping suitable in missile packing box of the utility model
Bracket includes pedestal and briquetting, and briquetting is divided into the first briquetting and the second briquetting；Pedestal top is provided with first end face structure and
Biend structure；The bottom end of first briquetting is provided with the first bottom surface structure；The bottom end of second briquetting is provided with the second bottom surface structure；
First bottom surface structure and first end face structure are hinged by the first bindiny mechanism；Second bottom surface structure and second end face structure pass through
Second bindiny mechanism is hinged；First briquetting and the second briquetting pass through the sealed connection of third bindiny mechanism；First briquetting, the second briquetting
A cylindrical cavity is surrounded for accommodating guided missile with pedestal.
Further, concave in the middle part of first end face structure, for accommodating the first bottom surface structure, the first bottom surface structure is first
The protrusion of briquetting center bottom, the top of protrusion are semicircle；It is concave in the middle part of second end face structure, for accommodating the second bottom surface knot
Structure, the second bottom surface structure are the protrusion of the second briquetting center bottom, and the top of protrusion is semicircle；First bindiny mechanism is first
Bolt, the first bolt passes through first end face structure and the first bottom surface structure carries out hingedly, so that can between the first briquetting and pedestal
It relatively rotates；Second bindiny mechanism is the second bolt, and the second bolt passes through second end face structure and the second bottom surface structure is cut with scissors
It connects, so that can be relatively rotated between the second briquetting and pedestal.
Further, third bindiny mechanism is located at the top of the first briquetting and the top of the second briquetting；Third bindiny mechanism
Stroke for hasp, hasp is adjustable, by controlling the stroke of hasp, adjusts the distance between the first briquetting and the second briquetting.
Further, pedestal includes bottom plate and base plate ontology；Bottom plate is rectangle；Base body is centrally positioned in bottom plate
On, the width of bottom plate is greater than the width of base body, forms the first flange and the second flange, the first flange and the second flange are opposite
It is symmetrical in the central axis of bottom plate；The both ends of first flange and the second flange are provided with fixation hole.
Further, the top surface of pedestal is recessed semi-cylindrical recesses, and semi-cylindrical recesses are for accommodating guided missile；Semicircle
Trapezoidal groove is further recessed in the middle part of the top surface of cylindrical groove, trapezoidal groove runs through pedestal, ladder along the width direction of pedestal
The cross section of connected in star is inverted isosceles trapezoid.
Further, it is provided with cushion on the contact surface of guided missile and guided missile Quick clamping bracket, cushion is fast with guided missile
Quick-mounting folder rack surface fits；There are four cushion is total, wherein two cushions are located on the concave surface of pedestal, other two
Cushion is located on the concave surface of the first briquetting on the concave surface of the second briquetting, and four cushions circumferentially divide along cylindrical cavity
Cloth.
Further, pedestal includes base shell；Base shell is shaped by polythene material rotational moulding, and pedestal is hollow；Alternatively,
Base shell is shaped by polythene material rotational moulding, and the inside of pedestal is filled with polyethylene foamed material.
Further, 3 millimeters to 15 millimeters of base shell wall thickness.
Further, the first briquetting includes the first briquetting shell, and the second briquetting includes the second briquetting shell；Outside first briquetting
Shell and the second briquetting shell are shaped by polythene material rotational moulding, and the first briquetting and the second briquetting are hollow；Alternatively, the first briquetting shell
It is shaped with the second briquetting shell by polythene material rotational moulding, the inside of the first briquetting and the second briquetting is filled with polyethylene foamed material
Material.
Further, 3 millimeters to 15 millimeters of the first briquetting shell wall thickness, and 3 millimeters of the second briquetting shell wall thickness is to 15 millis
Rice.
A kind of guided missile Quick clamping bracket suitable in missile packing box of the utility model has compared with prior art
There is following beneficial effect.
1, the technical program includes pedestal and briquetting due to using guided missile Quick clamping bracket, and briquetting is divided into the first briquetting
With the second briquetting；Pedestal top is provided with first end face structure and second end face structure；The bottom end of first briquetting is provided with first
Bottom surface structure；The bottom end of second briquetting is provided with the second bottom surface structure；First bottom surface structure and first end face structure pass through first
Bindiny mechanism is hinged；Second bottom surface structure and second end face structure are hinged by the second bindiny mechanism；First briquetting and the second pressure
Block passes through the sealed connection of third bindiny mechanism；First briquetting, the second briquetting and pedestal surround a cylindrical cavity for accommodate lead
The technological means of bullet；So the first briquetting can turn down outward with respect to pedestal and the second briquetting is also turned down with respect to pedestal outward, shape
At larger open, provide convenience for guided missile and being rapidly assembled and disassembled for missile packing box；Meanwhile third bindiny mechanism is fixed
The first briquetting and the second briquetting are connected, is conducive to guided missile and is tightly secured in missile packing box.
2, the technical program due to use first end face structure in the middle part of it is concave, for accommodate the first bottom surface structure, first
Bottom surface structure is the protrusion of the first briquetting center bottom, and the top of protrusion is semicircle；It is concave in the middle part of second end face structure, it is used for
The second bottom surface structure is accommodated, the second bottom surface structure is the protrusion of the second briquetting center bottom, and the top of protrusion is semicircle；First
Bindiny mechanism is the first bolt, and the first bolt passes through first end face structure and the first bottom surface structure carries out hingedly, so that the first pressure
It can be relatively rotated between block and pedestal；Second bindiny mechanism is the second bolt, and the second bolt passes through second end face structure and second
Bottom surface structure carries out hingedly, so that relatively turnable technical solution between the second briquetting and pedestal；So connecting machine in third
When structure is opened, the first briquetting can turn down counterclockwise using the first bolt as axis, and the second briquetting can turn over clockwise using the second bolt as axis
Folding, so that it is unobstructed above pedestal, be conducive to the quick access of guided missile；When needing for guided missile to be fixed in the bracket, only need
Guided missile is first put into pedestal, then the first briquetting is rotated clockwise as axis using the first bolt and is bonded up to the first briquetting with guided missile,
Second briquetting is rotated counterclockwise using the second bolt as axis until the second briquetting is bonded with guided missile, and fixed third of then pressurizeing connects machine
Structure, so that the first briquetting and the second briquetting that are connected with third bindiny mechanism and guided missile secured fit, so that it is tight to be conducive to guided missile
Admittedly be fixed in missile packing box.
3, the technical program is located at the top of the first briquetting and the top of the second briquetting due to using third bindiny mechanism；
Third bindiny mechanism is hasp, and the stroke of hasp is adjustable, by controlling the stroke of hasp, adjusts the first briquetting and the second briquetting
Between distance technical solution, so hasp is conducive to the quick access of guided missile.
4, the technical program includes bottom plate and base plate ontology due to using pedestal；Bottom plate is rectangle；Base body occupies
Middle to be arranged on bottom plate, the width of bottom plate is greater than the width of base body, forms the first flange and the second flange, the first flange and
Second flange is symmetrical relative to the central axis of bottom plate；The both ends of first flange and the second flange are provided with the technology of fixation hole
Scheme, so the bracket can be securely fixed in missile packing box by fixation hole；It is led simultaneously compared to integrally formed
It plays packing case and bracket, bracket and missile packing box and dismountable connection is reached by using fixation hole, facilitate the bracket
Maintenance, improves the service life of missile packing box.
5, the technical program is recessed semi-cylindrical recesses due to using the top surface of pedestal, and semi-cylindrical recesses are used for
Accommodate guided missile；It is further recessed trapezoidal groove in the middle part of the top surface of semi-cylindrical recesses, trapezoidal groove is along the width side of pedestal
To pedestal is run through, the cross section of trapezoidal groove is the technological means of inverted isosceles trapezoid, so guided missile can be placed on semicircle
In cylindrical groove, and trapezoidal groove provides for the attachment on guided missile side wall and places region, is conducive to the card of guided missile He the bracket
It closes.
6, it is provided with cushion on contact surface of the technical program due to using guided missile and guided missile Quick clamping bracket, delayed
Punching pad fits with guided missile Quick clamping bracket surface；There are four cushion is total, wherein two cushions are located at the concave surface of pedestal
On, other two cushion is located on the concave surface of the first briquetting on the concave surface of the second briquetting, and four cushions are along cylinder
The circumferentially distributed technological means of shape cavity is conducive to lead so cushion improves the frictional force between guided missile and pedestal or briquetting
Bullet is tightly secured in the bracket；Simultaneous buffering pad protects guided missile side wall, avoids pedestal or briquetting abrasion guided missile side wall；
In addition cushion can mitigate the vibration of guided missile, be conducive to protect guided missile.
7, the technical program includes base shell due to using pedestal；Base shell is shaped by polythene material rotational moulding,
Pedestal is hollow；Alternatively, base shell is shaped by polythene material rotational moulding, the inside of pedestal is filled with the skill of polyethylene foamed material
Art means are conducive to mitigate weight and realize lightweight application, and polyethylene foamed so pedestal uses low density material
Material further mitigates weight under the conditions of same mechanical property while increasing product wall thickness.
8, the technical program is due to the technological means using 3 millimeters to 15 millimeters of base shell wall thickness, so pedestal has
Guided missile is supported to effect, avoids pedestal collapsing, while being conducive to mitigate weight and realizing lightweight application.
9, the technical program includes the first briquetting shell due to using the first briquetting, and the second briquetting includes outside the second briquetting
Shell；First briquetting shell and the second briquetting shell are shaped by polythene material rotational moulding, and the first briquetting and the second briquetting are hollow；Or
Person, the first briquetting shell and the second briquetting shell are shaped by polythene material rotational moulding, and the inside of the first briquetting and the second briquetting is filled out
Technological means filled with polyethylene foamed material；So the first briquetting and the second briquetting use low density material, be conducive to subtract
Light weight and realization lightweight application；And polyethylene foamed material is while increasing product wall thickness, in same mechanical property item
Further mitigate weight under part.
10, the technical program is due to using 3 millimeters to 15 millimeters of the first briquetting shell wall thickness, and the second briquetting shell wall
Thick 3 millimeters to 15 millimeters of technological means so avoiding briquetting collapsing, while being conducive to mitigate weight and realizing that lightweight is answered
With.
Detailed description of the invention
With reference to the accompanying drawings and detailed description to a kind of guided missile suitable in missile packing box of the utility model
Quick clamping bracket is described in further detail.
Fig. 1 is the schematic diagram of the missile packing box and guided missile clamping bracket therein in background technique.
Fig. 2 is the partial enlarged view of region A in Fig. 1.
Fig. 3 is the schematic front view of the utility model guided missile Quick clamping bracket.
Fig. 4 is the stereoscopic schematic diagram of the utility model guided missile Quick clamping bracket.
Fig. 5 is the schematic front view of the pedestal of the utility model.
Fig. 6 is the stereoscopic schematic diagram of the pedestal of the utility model.
Fig. 7 is the stereoscopic schematic diagram of first briquetting of the utility model.
Fig. 8 is the stereoscopic schematic diagram of second briquetting of the utility model.
Fig. 9 is the diagrammatic cross-section of the pedestal of the utility model.
Figure 10 is the diagrammatic cross-section of first briquetting of the utility model.
Figure 11 is the diagrammatic cross-section of second briquetting of the utility model.
The reference numerals are as follows.
1, pedestal；
1-1, first end face structure；
1-2, second end face structure；
1-3, bottom plate；
1-3-1, the first flange；
1-3-2, the second flange；
1-3-3, fixation hole；
1-4, base body；
1-5, trapezoidal groove；
1-6, base shell；
2, the first briquetting；
2-1, the first bottom surface structure；
2-2, the first briquetting shell；
3, the second briquetting；
3-1, the second bottom surface structure；
3-2, the second briquetting shell；
4, the first bindiny mechanism；
5, the second bindiny mechanism；
6, third bindiny mechanism；
7, cushion.
Specific embodiment
As shown in Fig. 3 to Figure 11, the utility model provides a kind of guided missile quick-clamping branch suitable in missile packing box
Frame includes pedestal 1 and briquetting, and briquetting is divided into the first briquetting 2 and the second briquetting 3；1 top of pedestal is provided with first end face structure 1-
1 and second end face structure 1-2；The bottom end of first briquetting 2 is provided with the first bottom surface structure 2-1；The bottom end of second briquetting 3 is provided with
Second bottom surface structure 3-1；First bottom surface structure 2-1 and first end face structure 1-1 is hinged by the first bindiny mechanism 4；Second bottom
Face structure 3-1 and second end face structure 1-2 are hinged by the second bindiny mechanism 5；First briquetting 2 and the second briquetting 3 pass through third
The sealed connection of bindiny mechanism 6；First briquetting 2, the second briquetting 3 and pedestal 1 surround a cylindrical cavity for accommodating guided missile.
Since the first bottom surface structure 2-1 of the first briquetting 2 and the first end face structure 1-1 of pedestal 1 pass through the first connection machine
Structure 4 is hinged, so the first briquetting 2 can be rotated relative to pedestal 1；Due to the second bottom surface structure 3-1 and pedestal 1 of the second briquetting 3
Second end face structure 1-2 is hinged by the second bindiny mechanism 5, so the second briquetting 3 can be rotated relative to pedestal 1.It is put by guided missile
When entering the bracket or taking out guided missile from the bracket, the first briquetting 2 and the overturning of the second briquetting 3 are to 1 outside of pedestal, so that pedestal 1
Top clear, is conducive to fast operating.
As shown in Figures 3 to 8, concave in the middle part of the first end face structure 1-1 of present embodiment, for accommodating the first bottom surface knot
Structure 2-1, the first bottom surface structure 2-1 are the protrusion of 2 center bottom of the first briquetting, and the top of protrusion is semicircle；Second end face knot
It is concave in the middle part of structure 1-2, it is the prominent of 3 center bottom of the second briquetting for accommodating the second bottom surface structure 3-1, the second bottom surface structure 3-1
It rises, the top of protrusion is semicircle；First bindiny mechanism 4 is the first bolt, and the first bolt passes through first end face structure 1-1 and the
One bottom surface structure 2-1 is carried out hingedly, so that can relatively rotate between the first briquetting 2 and pedestal 1；Second bindiny mechanism 5 is second
Bolt, the second bolt pass through second end face structure 1-2 and the second bottom surface structure 3-1 and carry out hingedly, so that the second briquetting 3 and pedestal
It can be relatively rotated between 1.
Since the first bottom surface structure 2-1 of the first briquetting 2 and the first end face structure 1-1 of pedestal 1 are cut with scissors by the first bolt
It connects, so the first briquetting 2 can be rotated using the first bolt as axis relative to pedestal 1；Similarly, due to the second bottom surface of the second briquetting 3
The second end face structure 1-2 of structure 3-1 and pedestal 1 is by the second bolted splice, so the second briquetting 3 can be using the second bolt as axis
It is rotated relative to pedestal 1.Since the first briquetting 2 and the second briquetting 3 with flexible rotating can be conducive to that guided missile is quickly fixed on guided missile
Quickly take out in packing case or out of missile packing box guided missile.
As shown in Figure 3 to Figure 4, the third bindiny mechanism 6 of present embodiment is located at top and the second briquetting of the first briquetting 2
3 top；Third bindiny mechanism 6 is hasp, and the stroke of hasp is adjustable, by controlling the stroke of hasp, adjusts the first briquetting 2
And the second distance between briquetting 3.Hasp setting is at 3 top of the first briquetting 2 and the second briquetting.The hasp is given birth to by Kuai Lang company
It produces, model KL-4003.By adjusting the stroke of hasp, to adjust the size of fastening force between briquetting and guided missile, thus avoiding
Guided missile avoids briquetting while falling off from the bracket and weighs guided missile wounded.
As shown in Figure 5 and Figure 6, the pedestal 1 of present embodiment includes bottom plate 1-3 and base body 1-4；Bottom plate 1-3 is length
It is rectangular；Base body 1-4 is centrally positioned on bottom plate 1-3, and the width of bottom plate 1-3 is greater than the width of base body 1-4, forms the
One flange 1-3-1 and the second central axis of flange 1-3-2, the first flange 1-3-1 and the second flange 1-3-2 relative to bottom plate 1
Symmetrically；The both ends of first flange 1-3-1 and the second flange 1-3-2 are provided with fixation hole 1-3-3.
It is provided with fixation hole 1-3-3 on pedestal 1, pedestal 1 can be fixed in missile packing box by fixation hole 1-3-3.
It is integrally formed relative to pedestal 1 and missile packing box, it is fixed using dismountable connection, such as screw, pedestal 1 is fixed on and is led
It plays in packing case, is conducive to the maintenance of bracket.Bracket in one missile packing box only needs to change a bracket when damaging, without
Entire missile packing box is scrapped in cause, is conducive to save the cost.
As shown in Figure 5 and Figure 6, the top surface of the pedestal 1 of present embodiment is recessed semi-cylindrical recesses, and semi-cylindrical is recessed
Slot is for accommodating guided missile；Trapezoidal groove 1-5, the edge trapezoidal groove 1-5 are further recessed in the middle part of the top surface of semi-cylindrical recesses
The width direction of pedestal runs through pedestal 1, and the cross section of trapezoidal groove 1-5 is inverted isosceles trapezoid.
When guided missile is placed in the semi-cylindrical recesses of pedestal 1, the attachment on guided missile side wall can be placed in trapezoidal groove 1-5
It is interior, so that guided missile and the bracket be made to fasten, the large rotation angle of guided missile in transit is avoided, is conducive to improve guided missile packet
The security performance of vanning.
As shown in Figures 3 to 5, buffering is provided on the contact surface of the guided missile of present embodiment and guided missile Quick clamping bracket
Pad 7, cushion 7 fit with guided missile Quick clamping bracket surface；There are four cushion 7 is total, wherein two cushions 7 are located at
On the concave surface of pedestal 1, other two cushion 7 be located on the concave surface of the first briquetting 2 and the concave surface of the second briquetting 3 on, four
A cushion 7 is circumferentially distributed along cylindrical cavity.
The arcuate surface of cushion 7 is fixedly connected with pedestal 1 or briquetting, and the inner concave of cushion 7 and the side wall of guided missile are affixed
It closes.It is directly contacted compared to bracket with guided missile, cushion 7 can effectively increase stiction, so that guided missile is not susceptible to slide
Or rotation.In addition, due to the material of cushion 7, such as silica gel, rubber etc., quality is softer, can reduce the abrasion of guided missile side wall.
Meanwhile cushion 7 be due to that can absorb vibration, so vibration damping can be played the role of.
As shown in figure 9, the pedestal 1 of present embodiment includes base shell 1-6；Base shell 1-6 is rolled by polythene material
It is moulded into shape, pedestal 1 is hollow；Alternatively, base shell 1-6 is shaped by polythene material rotational moulding, the inside of pedestal 1 is poly- filled with foaming
Vinyl material.
Since polyethylene and polyethylene foamed are low density material, be conducive to the weight for mitigating pedestal 1.And gap shape
Polyethylene foamed material increase pedestal wall thickness while, under the premise of same mechanical property, further mitigate pedestal 1
Weight.
As shown in figure 9,3 millimeters to 15 millimeters of the base shell 1-6 wall thickness of present embodiment.When the wall thickness of pedestal 1 is less than 3
Millimeter, in the transport road conditions jolted, the self weight of guided missile and acceleration may cause the collapsing of pedestal 1.When wall thickness is greater than 15 millis
The self weight of meter Shi, pedestal 1 are excessive, do not meet lightweight standard.3 millimeters to 15 millimeters of base shell 1-6 wall thickness is according to mechanics
Analytical calculation show that the calculating considers the weight and number of holders of guided missile.
As shown in Figure 10 and Figure 11, the first briquetting 2 of present embodiment includes the first briquetting shell 2-2, the second briquetting 3 packet
Include the second briquetting shell 3-2；First briquetting shell 2-2 and the second briquetting shell 3-2 are shaped by polythene material rotational moulding, the first pressure
Block 2 and the second briquetting 3 are hollow；Alternatively, the first briquetting shell 2-2 and the second briquetting shell 3-2 are shaped by polythene material rotational moulding,
The inside of first briquetting 2 and the second briquetting 3 is filled with polyethylene foamed material.
Since polyethylene and polyethylene foamed are low density material, be conducive to the weight for mitigating briquetting.And gap shape
Polyethylene foamed material increase briquetting wall thickness while, under the premise of same mechanical property, further mitigate briquetting
Weight.
As shown in Figure 10 and Figure 11,3 millimeters to 15 millimeters of wall thickness of the first briquetting shell 2-2 of present embodiment, and second
The outer 3-2 shell wall of briquetting is 3 millimeters to 15 millimeters thick.When the wall thickness of briquetting is less than 3 millimeters, in the transport road conditions jolted, guided missile
Self weight and acceleration, may cause the damage of briquetting.When wall thickness is greater than 15 millimeters, the self weight of briquetting is excessive, does not meet light weight
Change standard.3 millimeters to 15 millimeters of briquetting shell wall thickness are calculated according to mechanical analysis, which considers the weight of guided missile
Amount and number of holders.
Embodiment one
Guided missile is put into missile packing box and needs following steps.Firstly, hasp is made, so that the first briquetting 2 and second
Briquetting 3 separates naturally.Second step turns counterclockwise the first briquetting 2, and the second briquetting 3 is turned clockwise, so that the first briquetting
2 and second the opening of briquetting 3 reach maximum so that 1 top of pedestal is unobstructed.Guided missile is put into the semicolumn of pedestal 1 by third step
In connected in star, guided missile is adjusted, so that the attachment on guided missile side wall is located in trapezoidal groove 1-5.4th step, the first briquetting 2 is suitable
Hour hands rotation, the second briquetting 3 is rotated counterclockwise, so that the cushion 7 on briquetting is bonded with guided missile outer wall.5th step, closure
Hasp, so that cushion 7 and guided missile pressurization connect.
Embodiment two
Guided missile is taken out out of missile packing box and needs following steps.Firstly, hasp is made, so that the first briquetting 2 and
Two briquettings 3 separate naturally.Second step turns counterclockwise the first briquetting 2, and the second briquetting 3 is turned clockwise, so that the first pressure
The opening of block 2 and the second briquetting 3 reaches maximum, so that 1 top of pedestal is unobstructed.Third step takes out guided missile.
Claims (10)
1. a kind of guided missile Quick clamping bracket suitable in missile packing box, including pedestal (1) and briquetting, which is characterized in that
The briquetting is divided into the first briquetting (2) and the second briquetting (3)；Pedestal (1) top be provided with first end face structure (1-1) and
Second end face structure (1-2)；The bottom end of first briquetting (2) is provided with the first bottom surface structure (2-1)；Second briquetting
(3) bottom end is provided with the second bottom surface structure (3-1)；First bottom surface structure (2-1) and the first end face structure (1-1)
It is hinged by the first bindiny mechanism (4)；Second bottom surface structure (3-1) and the second end face structure (1-2) pass through second
Bindiny mechanism (5) is hinged；First briquetting (2) and second briquetting (3) pass through third bindiny mechanism (6) sealed connection；
First briquetting (2), second briquetting (3) and the pedestal (1) surround a cylindrical cavity for accommodating the guided missile.
2. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
It is concave in the middle part of the first end face structure (1-1), for accommodating first bottom surface structure (2-1), first bottom surface structure
(2-1) is the protrusion of the first briquetting (2) center bottom, and the top of the protrusion is semicircle；The second end face structure
Concave in the middle part of (1-2), for accommodating second bottom surface structure (3-1), second bottom surface structure (3-1) is second pressure
The protrusion of block (3) center bottom, the top of the protrusion are semicircle；First bindiny mechanism (4) is the first bolt, described
First bolt passes through the first end face structure (1-1) and first bottom surface structure (2-1) carries out hingedly, so that described first
It can be relatively rotated between briquetting (2) and the pedestal (1)；Second bindiny mechanism (5) is the second bolt, second bolt
It carries out across the second end face structure (1-2) and second bottom surface structure (3-1) hingedly, so that second briquetting (3)
It can be relatively rotated between the pedestal (1).
3. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
The third bindiny mechanism (6) is located at the top of first briquetting (2) and the top of second briquetting (3)；The third
Bindiny mechanism (6) is hasp, and the stroke of the hasp is adjustable, by controlling the stroke of hasp, adjust first briquetting and
Distance between second briquetting.
4. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
The pedestal includes bottom plate (1-3) and base body (1-4)；The bottom plate (1-3) is rectangle；The base body (1-4)
It is centrally positioned on the bottom plate (1-3), the width of the bottom plate (1-3) is greater than the width of the base body (1-4), is formed
First flange (1-3-1) and the second flange (1-3-2), first flange (1-3-1) and second flange (1-3-2) are opposite
It is symmetrical in the central axis of the bottom plate (1-3)；The two of first flange (1-3-1) and second flange (1-3-2)
End is provided with fixation hole (1-3-3).
5. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
The top surface of the pedestal (1) is recessed semi-cylindrical recesses, and the semi-cylindrical recesses are for accommodating the guided missile；Described half
It is further recessed trapezoidal groove (1-5) in the middle part of the top surface of cylinder shape groove, the trapezoidal groove (1-5) is along the pedestal
Width direction runs through the pedestal, and the cross section of the trapezoidal groove (1-5) is inverted isosceles trapezoid.
6. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
It is provided with cushion (7) on the contact surface of the guided missile and the guided missile Quick clamping bracket, the cushion (7) is led with described
Quick clamping bracket surface is played to fit；There are four the cushion (7) is total, wherein two cushions (7) are located at described
On the concave surface of pedestal (1), other two cushion (7) is located on the concave surface of first briquetting (2) and described the
On the concave surface of two briquettings (3), four cushions (7) are circumferentially distributed along the cylindrical cavity.
7. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
The pedestal (1) includes base shell (1-6)；The base shell (1-6) is shaped by polythene material rotational moulding, the pedestal
(1) hollow；Alternatively, the base shell (1-6) is shaped by polythene material rotational moulding, the inside of the pedestal (1) is filled with hair
Steep polythene material.
8. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 7, it is characterised in that:
3 millimeters to 15 millimeters of wall thickness of the base shell (1-6).
9. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 1, it is characterised in that:
First briquetting (2) includes the first briquetting shell (2-2), and second briquetting (3) includes the second briquetting shell (3-2)；Institute
It states the first briquetting shell (2-2) and the second briquetting shell (3-2) is shaped by polythene material rotational moulding, first briquetting
(2) and second briquetting (3) is hollow；Alternatively, the first briquetting shell (2-2) and the second briquetting shell (3-2) by
The inside of polythene material rotational moulding forming, first briquetting (2) and second briquetting (3) is filled with polyethylene foamed material
Material.
10. a kind of guided missile Quick clamping bracket suitable in missile packing box according to claim 9, feature exist
In: 3 millimeters to 15 millimeters of wall thickness of the first briquetting shell (2-2)；And 3 millimeters of the second briquetting shell (3-2) wall thickness is extremely
15 millimeters.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822199964.XU CN209427378U (en) | 2018-12-26 | 2018-12-26 | A kind of guided missile Quick clamping bracket suitable in missile packing box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822199964.XU CN209427378U (en) | 2018-12-26 | 2018-12-26 | A kind of guided missile Quick clamping bracket suitable in missile packing box |
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| CN209427378U true CN209427378U (en) | 2019-09-24 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110561933A (en) * | 2019-10-09 | 2019-12-13 | 龚旭云 | Synchronous securities seal machine of mud is stained with in stamping |
| CN111301828A (en) * | 2019-12-25 | 2020-06-19 | 常州中航泰克船舶装备有限公司 | Heavy article storage and transportation box |
-
2018
- 2018-12-26 CN CN201822199964.XU patent/CN209427378U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110561933A (en) * | 2019-10-09 | 2019-12-13 | 龚旭云 | Synchronous securities seal machine of mud is stained with in stamping |
| CN111301828A (en) * | 2019-12-25 | 2020-06-19 | 常州中航泰克船舶装备有限公司 | Heavy article storage and transportation box |
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