CN204286247U - A kind of adjustable guided missile bracket - Google Patents
A kind of adjustable guided missile bracket Download PDFInfo
- Publication number
- CN204286247U CN204286247U CN201420719946.9U CN201420719946U CN204286247U CN 204286247 U CN204286247 U CN 204286247U CN 201420719946 U CN201420719946 U CN 201420719946U CN 204286247 U CN204286247 U CN 204286247U
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- Prior art keywords
- guided missile
- leading screw
- supporting plate
- lower supporting
- bracket
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Abstract
The utility model discloses a kind of adjustable guided missile bracket, this guided missile bracket comprises side shield, leading screw, lifting regulating mechanism, lower supporting plate and base, the two ends activity of lower supporting plate and leading screw arranges side shield, leading screw is positioned at the below of lower supporting plate, adjusting handle is installed in leading screw one end, regulate adjusting handle to drive leading screw to adjust the spacing of two side shields, leading screw is fixed on lifting regulating mechanism together with lower supporting plate entirety, and lifting regulating mechanism lower end is fixed on base.The utility model carries out Curve guide impeller for former guided missile bracket, is adjustable by the support Design of guided missile bracket.By the spacing regulating adjusting handle to drive leading screw adjustment side shield, this spacing can regulate according to missile overall dimensions, may be used for depositing of polytypic guided missile.Adaptability adjustment is carried out, to reach the object that same guided missile bracket is applicable to polytypic guided missile according to different guided missile profiles and size.
Description
Technical field
The utility model relates to a kind of guided missile bracket, particularly relates to a kind of adjustable guided missile bracket.
Background technology
Guided missile bracket belongs to missile weapon system dedicated ground support equipment, and temporarily its effect deposits guided missile, and existing guided missile bracket is made up of support 1 ', lifting regulating mechanism 2 ', base 3 ' usually, as shown in Figure 1.Support 1 ' is according to guided missile shape fabricating, and during work, by missile hoisting on guided missile bracket, guided missile supporting surface is placed on support 1 '.Different according to guided missile size, support one piece of guided missile needs bracket shown in 2-3 Fig. 1 usually, because profile is different before and after guided missile, the shape of the support 1 ' of support same piece of guided missile can change, therefore before, during and after supporting same piece of guided missile, bracket shape is not identical.The guided missile bracket utilization rate of this form is low, and the guided missile profile of different model is not identical, is necessary for the independent development missile bracket of guided missile of each model.Therefore, need to provide a kind of new technical scheme to solve the problems referred to above.
Utility model content
The utility model technical issues that need to address are to provide a kind of adjustable guided missile bracket, and this bracket is general for the guided missile of different profile.
For solving technical problem of the present utility model, the technical solution adopted in the utility model is:
A kind of adjustable guided missile bracket, this guided missile bracket comprises side shield, leading screw, lifting regulating mechanism, lower supporting plate and base, the two ends activity of described lower supporting plate and leading screw arranges side shield, described leading screw is positioned at the below of lower supporting plate, adjusting handle is installed in described leading screw one end, regulate adjusting handle to drive leading screw to adjust the spacing of two side shields, described leading screw is fixed on lifting regulating mechanism together with lower supporting plate entirety, and described lifting regulating mechanism lower end is fixed on base.
Described side shield bottom has two movable spans successively, and described side shield and leading screw, through this movable span, regulate adjusting handle to drive screw turns, two side shields are moved on lower supporting plate, form the spacing meeting guided missile profile.
The below of lower supporting plate is fixed in described leading screw one end by Connection Block.
Described lifting regulating mechanism comprises pipe in adjusting handle, lifting outer tube and lifting, and described adjusting handle is fixed on lifting outer tube, and described lifting outer tube is connected with pipe spiral in lifting.
Have a contiguous block in the middle part of described lower supporting plate, this contiguous block, for being flexibly connected leading screw, is fixed on the adjusting handle center of lifting regulating mechanism bottom described contiguous block.
The beneficial effects of the utility model:
1, versatility is high, the guided missile bracket that the guided missile for different model does not need special development new, and the guided missile in certain appearance and size can this guided missile bracket general;
2, utilization rate is high, and when Multiple Type guided missile works simultaneously, the quantity can considering guided missile bracket as a whole is called.
Accompanying drawing explanation
Fig. 1 is prior art guided missile bracket schematic diagram.
Fig. 2 is structural representation of the present utility model.
1, side shield, 11, movable span, 2, leading screw, 3, adjusting handle, 4, lifting regulating mechanism, 41, adjusting handle, 42, lifting outer tube, 43, pipe in lifting, 5, base, 6, lower supporting plate, 7, Connection Block, 8, contiguous block.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.Following examples, only for illustration of the utility model, are not used for limiting protection domain of the present utility model.
As shown in Figure 2, the adjustable guided missile bracket of one of the present utility model, this guided missile bracket comprises side shield 1, leading screw 2, lifting regulating mechanism 4, lower supporting plate 6 and base 5, the two ends activity of lower supporting plate 6 and leading screw 2 arranges side shield 1, leading screw 2 is positioned at the below of lower supporting plate 6, adjusting handle 3 is installed in leading screw 2 one end, adjusting handle 3 is regulated to drive leading screw 2 to adjust the spacing of two side shields 1, leading screw 2 is fixed on lifting regulating mechanism 4 together with lower supporting plate 6 entirety, and lifting regulating mechanism 4 lower end is fixed on base 5.
In order to regulate the distance between two side shields 1, make the guided missile meeting each profile size, side shield 1 bottom has two movable spans 11 successively, side shield 1 and leading screw 2 are through this movable span 11, adjusting handle 3 is regulated to drive leading screw 2 to rotate, two side shields 1 are moved on lower supporting plate 6, forms the spacing meeting guided missile profile.
Wherein, the below of lower supporting plate 6 is fixed in leading screw 2 one end by Connection Block 7.Leading screw 2 one end is lived by support, and the other end regulates rotation by adjusting handle 3.
With reference to figure 2, lifting regulating mechanism 4 comprises pipe 43 in adjusting handle 41, lifting outer tube 42 and lifting, and adjusting handle 41 is fixed on lifting outer tube 42, and lifting outer tube 42 is connected with pipe 43 spiral in lifting.
And the top of lifting regulating mechanism 4 and the annexation of miscellaneous part are such: have a contiguous block 8 in the middle part of lower supporting plate 6, this contiguous block 8, for being flexibly connected leading screw 2, is fixed on adjusting handle 41 center of lifting regulating mechanism 4 bottom contiguous block 8.In lifting regulating mechanism 4 uphill process, two adjustable side shields 1 rise together with lower supporting plate 6, leading screw 2.Meet the demand of relying on various guided missile.
The utility model carries out Curve guide impeller for former guided missile bracket, is adjustable by the support Design of guided missile bracket.By regulating adjusting handle 3 to drive leading screw 2 to adjust the spacing of side shield 1, this spacing can regulate according to missile overall dimensions, may be used for depositing of polytypic guided missile.Adaptability adjustment is carried out, to reach the object that same guided missile bracket is applicable to polytypic guided missile according to different guided missile profiles and size.
Claims (5)
1. an adjustable guided missile bracket, it is characterized in that: this guided missile bracket comprises side shield, leading screw, lifting regulating mechanism, lower supporting plate and base, the two ends activity of described lower supporting plate and leading screw arranges side shield, described leading screw is positioned at the below of lower supporting plate, adjusting handle is installed in described leading screw one end, adjusting handle is regulated to drive leading screw to adjust the spacing of two side shields, described leading screw is fixed on lifting regulating mechanism together with lower supporting plate entirety, and described lifting regulating mechanism lower end is fixed on base.
2. the adjustable guided missile bracket of one according to claim 1, it is characterized in that: described side shield bottom has two movable spans successively, described side shield and leading screw are through this movable span, adjusting handle is regulated to drive screw turns, two side shields are moved on lower supporting plate, forms the spacing meeting guided missile profile.
3. the adjustable guided missile bracket of one according to claim 2, is characterized in that: the below of lower supporting plate is fixed in described leading screw one end by Connection Block.
4. the adjustable guided missile bracket of one according to claim 1, it is characterized in that: described lifting regulating mechanism comprises pipe in adjusting handle, lifting outer tube and lifting, described adjusting handle is fixed on lifting outer tube, and described lifting outer tube is connected with pipe spiral in lifting.
5. the adjustable guided missile bracket of one according to claim 1, is characterized in that: have a contiguous block in the middle part of described lower supporting plate, this contiguous block, for being flexibly connected leading screw, is fixed on the adjusting handle center of lifting regulating mechanism bottom described contiguous block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420719946.9U CN204286247U (en) | 2014-11-27 | 2014-11-27 | A kind of adjustable guided missile bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420719946.9U CN204286247U (en) | 2014-11-27 | 2014-11-27 | A kind of adjustable guided missile bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204286247U true CN204286247U (en) | 2015-04-22 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420719946.9U Active CN204286247U (en) | 2014-11-27 | 2014-11-27 | A kind of adjustable guided missile bracket |
Country Status (1)
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| CN (1) | CN204286247U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292490A (en) * | 2015-11-19 | 2016-02-03 | 江西洪都航空工业集团有限责任公司 | Height-adjustable bullet hanging vehicle bracket |
| CN106839905A (en) * | 2016-11-30 | 2017-06-13 | 上海机电工程研究所 | Protect the flexible carrier of body coating |
| CN110834737A (en) * | 2019-10-25 | 2020-02-25 | 江西洪都航空工业集团有限责任公司 | Multifunctional bullet carrying vehicle with variable bracket |
| CN111811321A (en) * | 2020-07-10 | 2020-10-23 | 北京星途探索科技有限公司 | Novel simple missile launcher |
| CN115060125A (en) * | 2022-07-08 | 2022-09-16 | 江西洪都航空工业集团有限责任公司 | Variable diameter becomes and supports interval guided missile support fixed establishment |
-
2014
- 2014-11-27 CN CN201420719946.9U patent/CN204286247U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292490A (en) * | 2015-11-19 | 2016-02-03 | 江西洪都航空工业集团有限责任公司 | Height-adjustable bullet hanging vehicle bracket |
| CN106839905A (en) * | 2016-11-30 | 2017-06-13 | 上海机电工程研究所 | Protect the flexible carrier of body coating |
| CN106839905B (en) * | 2016-11-30 | 2018-08-03 | 上海机电工程研究所 | Protect the flexible carrier of body coating |
| CN110834737A (en) * | 2019-10-25 | 2020-02-25 | 江西洪都航空工业集团有限责任公司 | Multifunctional bullet carrying vehicle with variable bracket |
| CN111811321A (en) * | 2020-07-10 | 2020-10-23 | 北京星途探索科技有限公司 | Novel simple missile launcher |
| CN115060125A (en) * | 2022-07-08 | 2022-09-16 | 江西洪都航空工业集团有限责任公司 | Variable diameter becomes and supports interval guided missile support fixed establishment |
| CN115060125B (en) * | 2022-07-08 | 2023-11-03 | 江西洪都航空工业集团有限责任公司 | Missile supporting and fixing mechanism with variable diameter and variable supporting distance |
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