CN201476718U - Limit mechanism for missile packing box - Google Patents
Limit mechanism for missile packing box Download PDFInfo
- Publication number
- CN201476718U CN201476718U CN2009201615900U CN200920161590U CN201476718U CN 201476718 U CN201476718 U CN 201476718U CN 2009201615900 U CN2009201615900 U CN 2009201615900U CN 200920161590 U CN200920161590 U CN 200920161590U CN 201476718 U CN201476718 U CN 201476718U
- Authority
- CN
- China
- Prior art keywords
- locating rack
- crossbeam
- missile
- packing box
- limit mechanism
- Prior art date
- 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 - Lifetime
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Abstract
The utility model belongs to the technical field of missile packing and particularly relates to a limit mechanism for a missile packing box. The utility model aims at providing the limit mechanism for the missile packing box which has simple and convenient operation. The limit mechanism for the missile packing box comprises a locating rack (4), at least two beams (5) and two limit frames (8), wherein the locating rack (4) and the beams (5) take the metal rod shapes; the two beams (5) are vertically arranged at the two ends of the locating rack (4) to form the I-shaped integrated structure; the other beams (5) are vertically arranged on the locating rack (4); the limit frames (8) take the metal cube shapes; and the two limit frames (8) are arranged on the locating rack (4). The limit mechanism for the missile packing box has the benefits that the structure is simple; when in operation, as a missile body can be operated above a missile, the operation is simple, convenient and fast.
Description
Technical field
The utility model belongs to the missile packaging technical field, is specifically related to a kind of missile packing box position-limit mechanism.
Background technology
Guided missile is after packing case is advanced in lifting, and packing case all needs guided missile is carried out reliably spacing and fixing.Missile packing box was to the spacing form of guided missile in the past, the forms that adopt fastening bolt or fastening bolt to add band more, because the installation site of fastening bolt generally all is positioned at the body below, be to guarantee the fixing reliable of guided missile, cause in the design of position limiting structure complicated, during operation, need earlier guided missile to be installed on the supported cart, then supported cart is shifted onto in the case, the packing case remaining part is installed again, operation sequence is loaded down with trivial details.
The utility model content
The purpose of this utility model provides a kind of missile packing box position-limit mechanism easy and simple to handle.
The utility model is achieved in that
A kind of missile packing box position-limit mechanism, it comprises locating rack, at least two crossbeams and two limitting casings, it is shaft-like that locating rack and crossbeam are metal system; Wherein, two beam vertical are installed in the two ends of locating rack, form the integrative-structure of " worker " font, and remaining beam vertical is installed on the locating rack; Limitting casing is a metal system square or rectangular-shaped, and two limitting casings are installed on the locating rack.
It also comprises the rectangular-shaped metal system reinforcement of the top, position that is installed in locating rack upper limit frame.
It also comprises the rectangular lamellar metal system stiffener of the installed position that is installed in crossbeam entablature and locating rack.
It comprises reinforcement, stiffener and sleeve pipe; Respectively there is a locating hole at the crossbeam two ends, be used for being spirally connected fastening with the missile packing box box side, middle part at crossbeam is welded with stiffener, in the middle of crossbeam, be welded with a sleeve pipe, there is a through hole at the sleeve pipe middle part, be used to make the bolt on the locating rack to pass, and be connected fastening two crossbeams with locating rack with the attaching nut; Crossbeam is vertically mounted on the two ends of locating rack by attaching nut and bolt, forms the integrative-structure of " worker " font; Two limitting casings are welded on the locating rack, one of them limitting casing is installed in the position of crossbeam and locating rack installation, specifically be installed in the locating rack downside, another limitting casing is installed in the position of locating rack downside, close another crossbeam, and particular location is determined by the size of the hanging joint of guided missile; Reinforcement is installed in position, the locating rack upside of locating rack upper limit frame; After locating rack and crossbeam linked into an integrated entity, the locating hole by the crossbeam two ends was installed on the double-screw bolt of packing case box side, and is connected and fixed with securing member.
Aforesaid locating rack and crossbeam are quarter bend or square tube or I-steel or channel-section steel or steel pipe or round steel.
The material of aforesaid locating rack and crossbeam is made by Q235 or 20# steel or Q345 or 30CrMnSiA.
The material of aforesaid reinforcement is section bar or steel plate.
The material of aforesaid stiffener is section bar or steel plate.
The beneficial effects of the utility model are:
Missile packing box position-limit mechanism of the present utility model is simple in structure, above guided missile body is operated during operation, and is simple and efficient to handle.
Description of drawings
Fig. 1 is a stereogram of using a kind of missile packing box of the present utility model;
Fig. 2 is the vertical view of a kind of missile packing box position-limit mechanism of the present utility model;
Fig. 3 is the front view of a kind of missile packing box position-limit mechanism of the present utility model;
Among the figure: 1. missile packing box position-limit mechanism, 2. double-screw bolt, 3. missile packing box box side, 4. locating rack, 5. crossbeam, 6. attaching nut, 7. bolt, 8. limitting casing, 9. reinforcement, 10. stiffener, 11. sleeve pipes, 12. locating holes.
The specific embodiment
Below in conjunction with drawings and Examples being introduced to a kind of missile packing box position-limit mechanism of the present utility model:
As shown in Figure 1, a kind of missile packing box comprises missile packing box and missile packing box position-limit mechanism 1, and missile packing box comprises missile packaging box body and missile packing box case lid, and the missile packaging box body is the rectangular box of opening, and case lid is that rectangle is lamellar; Missile packing box position-limit mechanism 1 comprises locating rack 4, at least two crossbeams 5 and two limitting casings 8, it is shaft-like that locating rack 4 and crossbeam 5 are metal system, the quantity of crossbeam 5 is by the actual conditions decision of guided missile, generally length, weight and the concrete movement requirement by guided missile determines, wherein, two crossbeams 5 are vertically mounted on the two ends of locating rack 4, form the integrative-structure of " worker " font, remaining crossbeam 5 is vertically mounted on the locating rack 4, and the particular location of installation is by the actual conditions decision of guided missile; Limitting casing 8 is that metal system is cube-shaped, and two limitting casings 8 are installed on the locating rack 4, and its installation site determined by the size of the hanging joint of guided missile, and the position that generally requires limitting casing 8 and missile hoisting be the location matches of hanging joint when interior to case.For the intensity of strengthening locating rack 4, the weight that reduces locating rack 4, can rectangular-shaped metal system reinforcement 9 be installed in the position above the locating rack 4 upper limit frames 8, be used to strengthen the local strength of locating rack 4, the length of reinforcement 9 is calculated the requirement of strength of locating rack 4 according to the guided missile transportation and is determined.For the intensity of web beam 5, can rectangular lamellar metal system stiffener 10 be installed at the installed position of crossbeam 5 entablatures 5 and locating rack 4, the length of stiffener 10 is calculated the requirement of strength of crossbeam 5 according to the guided missile transportation and is determined.
Above-mentioned locating rack 4 and crossbeam 5 can be quarter bend, square tube, I-steel, channel-section steel, steel pipe, round steel and the channel-section steel, quarter bend or the square tube that form with steel plate, equal leg angle, unequal angle welding.
The material of above-mentioned locating rack 4 and crossbeam 5 is Q235,20# steel, Q345 or 30CrMnSiA.
Above-mentioned limitting casing 8 also can be rectangular-shaped, and its shape is determined according to actual conditions.
Above-mentioned missile packing box position-limit mechanism 1 is installed in the missile packing box, and its installation site and missile hoisting are to the interior location matches of case.
Below in conjunction with a specific embodiment a kind of missile packing box position-limit mechanism 1 of the present invention is introduced:
As shown in Figures 2 and 3, a kind of missile packing box position-limit mechanism 1 comprises locating rack 4, two crossbeams 5, attaching nut 6, bolt 7, limitting casing 8, reinforcement 9, stiffener 10 and sleeve pipes 11;
Respectively there is a locating hole 12 at crossbeam 5 two ends, be used for being spirally connected fastening with missile packing box box side 3, be welded with stiffener 10 at the middle part of crossbeam 5, in the middle of crossbeam 5, be welded with a sleeve pipe 11, there is a through hole at sleeve pipe 11 middle parts, be used to make the bolt 7 on the locating rack 4 to pass, and be connected fastening two crossbeams 5 with locating rack 4 with attaching nut 6; Crossbeam 5 is vertically mounted on the two ends of locating rack 4 by attaching nut 6 and bolt 7, forms the integrative-structure of " worker " font; Two limitting casings 8 are welded on the locating rack 4, one of them limitting casing 8 is installed in the position of crossbeam 5 and locating rack 4 installations, specifically be installed in locating rack 4 downsides, another limitting casing 8 is installed in the position of locating rack 4 downsides, close another crossbeam 5, and particular location is determined by the size of the hanging joint of guided missile; Reinforcement 9 is installed position, locating rack 4 upsides of locating rack 4 upper limit frames 8.
After locating rack 4 and crossbeam 5 link into an integrated entity, locating hole 12 by crossbeam 5 two ends is installed on the double-screw bolt 2 of packing case box side 3, and be connected and fixed with securing member, guided missile in 8 pairs of missile packing boxes of while limitting casing carries out spacing, and more than operation can be with the guided missile secure fixation in missile packing box.
All available section bar of limitting casing 8, reinforcement 9, stiffener 10 and sleeve pipe 11 or steel plate processing.
The course of work: at first the assigned address of missile hoisting in the missile packing box, with 8 alignings of the limitting casing on the missile packing box position-limit mechanism 1 and after compressing the forward and backward hanging joint of guided missile, again with the double-screw bolt 2 on the 12 aligning box sides 3 of the locating hole on the crossbeam 5, put down missile packing box position-limit mechanism 1 back with securing member with the position-limit mechanism secure fixation in casing, then, cover case lid, finish encapsulation.When a year bullet packing case transports,, guarantee the safety of guided missile transportation by the displacement that limits the guided missile all directions that compresses of 8 pairs of forward and backward hanging joints of guided missile of the limitting casing on the position-limit mechanism.
Claims (8)
1. missile packing box position-limit mechanism, it is characterized in that: it comprises locating rack (4), at least two crossbeams (5) and two limitting casings (8), it is shaft-like that locating rack (4) and crossbeam (5) are metal system; Wherein, two crossbeams (5) are vertically mounted on the two ends of locating rack (4), form the integrative-structure of " worker " font, and remaining crossbeam (5) is vertically mounted on the locating rack (4); Limitting casing (8) is metal system square or rectangular-shaped, and two limitting casings (8) are installed on the locating rack (4).
2. a kind of missile packing box position-limit mechanism according to claim 1 is characterized in that: it also comprises the rectangular-shaped metal system reinforcement (9) of the top, position that is installed in locating rack (4) upper limit frame (8).
3. a kind of missile packing box position-limit mechanism according to claim 1 and 2 is characterized in that: it also comprises the rectangular lamellar metal system stiffener (10) of the installed position that is installed in crossbeam (5) entablature (5) and locating rack (4).
4. a kind of missile packing box position-limit mechanism according to claim 1 is characterized in that: it comprises reinforcement (9), stiffener (10) and sleeve pipe (11); Respectively there is a locating hole (12) at crossbeam (5) two ends, be used for being spirally connected fastening with missile packing box box side (3), be welded with stiffener (10) at the middle part of crossbeam (5), in the middle of crossbeam (5), be welded with a sleeve pipe (11), there is a through hole at sleeve pipe (11) middle part, be used to make the bolt (7) on the locating rack (4) to pass, and be connected fastening two crossbeams (5) with locating rack (4) with attaching nut (6); Crossbeam (5) is vertically mounted on the two ends of locating rack (4) by attaching nut (6) and bolt (7), forms the integrative-structure of " worker " font; Two limitting casings (8) are welded on the locating rack (4), one of them limitting casing (8) is installed in the position of crossbeam (5) and locating rack (4) installation, specifically be installed in locating rack (4) downside, another limitting casing (8) is installed in the position of locating rack (4) downside, close another crossbeam (5), and particular location is determined by the size of the hanging joint of guided missile; Reinforcement (9) is installed in position, locating rack (4) upside of locating rack (4) upper limit frame (8); After locating rack (4) and crossbeam (5) linked into an integrated entity, the locating hole (12) by crossbeam (5) two ends was installed on the double-screw bolt (2) of packing case box side (3), and is connected and fixed with securing member.
5. a kind of missile packing box position-limit mechanism according to claim 1 is characterized in that: described locating rack (4) and crossbeam (5) are quarter bend or square tube or I-steel or channel-section steel or steel pipe or round steel.
6. a kind of missile packing box position-limit mechanism according to claim 1 is characterized in that: the material of described locating rack (4) and crossbeam (5) is made by Q235 or 20# steel or Q345 or 30CrMnSiA.
7. a kind of missile packing box position-limit mechanism according to claim 2 is characterized in that: the material of described reinforcement (9) is section bar or steel plate.
8. a kind of missile packing box position-limit mechanism according to claim 3 is characterized in that: the material of described stiffener (10) is section bar or steel plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201615900U CN201476718U (en) | 2009-08-06 | 2009-08-06 | Limit mechanism for missile packing box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201615900U CN201476718U (en) | 2009-08-06 | 2009-08-06 | Limit mechanism for missile packing box |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201476718U true CN201476718U (en) | 2010-05-19 |
Family
ID=42412968
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201615900U Expired - Lifetime CN201476718U (en) | 2009-08-06 | 2009-08-06 | Limit mechanism for missile packing box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201476718U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112676809A (en) * | 2020-12-17 | 2021-04-20 | 北京航星机器制造有限公司 | Disassembling device and method for warhead product |
| CN116697833A (en) * | 2023-07-28 | 2023-09-05 | 北京爱思达航天科技有限公司 | Composite material packaging box and preparation method thereof |
-
2009
- 2009-08-06 CN CN2009201615900U patent/CN201476718U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112676809A (en) * | 2020-12-17 | 2021-04-20 | 北京航星机器制造有限公司 | Disassembling device and method for warhead product |
| CN112676809B (en) * | 2020-12-17 | 2022-06-10 | 北京航星机器制造有限公司 | Disassembling device and method for warhead product |
| CN116697833A (en) * | 2023-07-28 | 2023-09-05 | 北京爱思达航天科技有限公司 | Composite material packaging box and preparation method thereof |
| CN116697833B (en) * | 2023-07-28 | 2023-12-29 | 北京爱思达航天科技有限公司 | Composite material packaging box and preparation method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20100519 |