CN204630479U - Dual-purpose type hail-proof rain-increasing rocket launching trajectory - Google Patents
Dual-purpose type hail-proof rain-increasing rocket launching trajectory Download PDFInfo
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- CN204630479U CN204630479U CN201520273095.4U CN201520273095U CN204630479U CN 204630479 U CN204630479 U CN 204630479U CN 201520273095 U CN201520273095 U CN 201520273095U CN 204630479 U CN204630479 U CN 204630479U
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- lower guideway
- upper rail
- cushion block
- movable cushion
- rocket
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Abstract
The utility model relates to hail-proof rain-increasing rocket launching trajectory technical field, is a kind of dual-purpose type hail-proof rain-increasing rocket launching trajectory; It comprises rocket bomb transmitting cylinder, upper rail movable cushion block, upper rail, lower guideway movable cushion block and lower guideway; Be installed with upper rail movable cushion block in the inner upper end of rocket bomb transmitting cylinder, upper rail through before and after being provided with in the lower end of upper rail movable cushion block installs lower bayonet slot, installs lower bayonet slot internal fixtion be provided with upper rail at upper rail; Lower guideway movable cushion block is installed with in the interior lower end of rocket bomb transmitting cylinder.The utility model reasonable and compact in structure, easy to use; By formal dress with instead load guide rail movable cushion block and upper rail movable cushion block, the launching trajectory of two kinds of different in width can be formed, can the object of double-purpose to reach; Launching trajectory width can being selected to be applicable to according to the actual demand of user in each rocket bomb transmitting cylinder on rocket pod, improves the utilization rate of rocket pod, economizes on resources.
Description
Technical field
the utility model relates to hail-proof rain-increasing rocket launching trajectory technical field, is a kind of dual-purpose type hail-proof rain-increasing rocket launching trajectory.
Background technology
weather modification refers under suitable weather condition, by manual intervention, makes synoptic process meet the change of mankind's hope.By rocket projector, the rocket projectile of catalyst will be housed, the predetermined position be transmitted in target cloud carries out artificial catalysis, is maximum, the economic and efficient a kind of operation technique means used at present; Rocket projector comprises rocket pod and adding rocket launching controller, and rocket combination shoe is the composition core of rocket pod; Rocket projectile to be launched will be loaded in launching trajectory, and when after rocket projectile igniting, rocket projectile is overstepped the limit along track accelerated slip; But the hail-proof rain-increasing rocket that the existing launching trajectory used can only be used for a kind of model is launched, and use single, greatly constrain the service efficiency of rocket pod, utilization rate is low; Waste resource.
Summary of the invention
the utility model provides a kind of dual-purpose type hail-proof rain-increasing rocket launching trajectory, overcome the deficiency of above-mentioned prior art, the hail-proof rain-increasing rocket that its launching trajectory that effectively can solve existing use rocket pod can only be used for a kind of model is launched, use single, service efficiency and utilization rate low, waste resource problem.
the technical solution of the utility model is realized by following measures: a kind of dual-purpose type hail-proof rain-increasing rocket launching trajectory, comprises rocket bomb transmitting cylinder, upper rail movable cushion block, upper rail, lower guideway movable cushion block and lower guideway; Be installed with upper rail movable cushion block in the inner upper end of rocket bomb transmitting cylinder, upper rail through before and after being provided with in the lower end of upper rail movable cushion block installs lower bayonet slot, installs lower bayonet slot internal fixtion be provided with upper rail at upper rail; Lower guideway movable cushion block is installed with in the interior lower end at rocket bomb transmitting cylinder, lower guideway movable cushion block top be provided with lower guideway and install draw-in groove, install draw-in groove internal fixtion at lower guideway and lower guideway is installed, between lower guideway and upper rail, form launching trajectory; Be provided with and groove depth corresponding with guide rail to be greater than the lower guideway that lower guideway installs draw-in groove in the bottom of lower guideway movable cushion block lower bayonet slot is installed.
here is the further optimization and/or improvements to above-mentioned utility model technical scheme:
the top of above-mentioned upper rail movable cushion block can be provided with and groove depth corresponding with guide rail and be more than or equal to the upper rail that upper rail installs lower bayonet slot and install draw-in groove.
two ends, left and right on the downside of above-mentioned lower guideway movable cushion block can be respectively equipped with can strengthen lower guideway movable cushion block bottom area widen footing.
above-mentioned upper rail can adopt the grooved track that Open Side Down; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of upper rail and upper rail movable cushion block, the upper end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with upper rail fixing hole, in mutually corresponding connecting hole and upper rail fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that upper rail, upper rail movable cushion block can be fixed on rocket bomb transmitting cylinder inner upper end; Lower guideway adopts the grooved track of opening upwards; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of lower guideway and lower guideway movable cushion block, the lower end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with lower guideway fixing hole, in mutually corresponding connecting hole and lower guideway fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that lower guideway, lower guideway movable cushion block can be fixed on rocket bomb transmitting cylinder interior lower end.
the groove depth difference that above-mentioned lower guideway installation lower bayonet slot and lower guideway install draw-in groove can be less than or equal to 16 millimeters.
the utility model reasonable and compact in structure, easy to use; By formal dress with instead load guide rail movable cushion block and upper rail movable cushion block, the launching trajectory of two kinds of different in width can be formed, can the object of double-purpose to reach; Launching trajectory width can being selected to be applicable to according to the actual demand of user in each rocket bomb transmitting cylinder on rocket pod, improves service efficiency and the utilization rate of rocket pod, economizes on resources.
Accompanying drawing explanation
accompanying drawing 1 is main TV structure schematic diagram the utility model most preferred embodiment being installed φ 66 hail-proof rain-increasing rocket.
accompanying drawing 2 is main TV structure schematic diagram the utility model most preferred embodiment being installed φ 82 hail-proof rain-increasing rocket.
coding in accompanying drawing is respectively: 1 is rocket bomb transmitting cylinder, and 2 is upper rail movable cushion block, and 3 is upper rail, 4 is lower guideway movable cushion block, 5 is attaching nut, and 6 install draw-in groove for lower guideway, and 7 is lower guideway, 8 is lower guideway installation lower bayonet slot, 9 install draw-in groove for upper rail, and 10 for widening footing, and 11 is connecting bolt, 12 is the explosion-proof rain-increasing rocket of φ 66, and 13 is the explosion-proof rain-increasing rocket of φ 83.
Detailed description of the invention
the utility model by the restriction of following embodiment, can not determine concrete embodiment according to the technical solution of the utility model and actual conditions.
in the utility model, for convenience of description, the description of the relative position relation of each parts is all be described according to the Butut mode of Figure of description 1, as: the position relationship of upper and lower, left and right etc. determines according to the Butut direction of Figure of description 1.
below in conjunction with embodiment and accompanying drawing, the utility model is further described:
as shown in Figure 1, this dual-purpose type hail-proof rain-increasing rocket launching trajectory comprises rocket bomb transmitting cylinder 1, upper rail movable cushion block 2, upper rail 3, lower guideway movable cushion block 4 and lower guideway 7; Be installed with upper rail movable cushion block 2 in the inner upper end of rocket bomb transmitting cylinder 1, upper rail through before and after being provided with in the lower end of upper rail movable cushion block 2 installs lower bayonet slot, installs lower bayonet slot internal fixtion be provided with upper rail 3 at upper rail; Lower guideway movable cushion block 4 is installed with in the interior lower end at rocket bomb transmitting cylinder 1, lower guideway movable cushion block 4 top be provided with lower guideway and install draw-in groove 6, install draw-in groove 6 internal fixtion at lower guideway and lower guideway 7 is installed, between lower guideway 7 and upper rail 3, form launching trajectory; Be provided with and groove depth corresponding with guide rail to be greater than the lower guideway that lower guideway installs draw-in groove 6 in the bottom of lower guideway movable cushion block 4 lower bayonet slot 8 is installed.
during installation, lower guideway movable cushion block 4 can positive and negatively use; , lower guideway installs draw-in groove 6 upward during formal dress as shown in Figure 1, and lower guideway 7 lower end is fixed on lower guideway and installs in draw-in groove 6; During anti-dress as shown in Figure 2, lower guideway installs lower bayonet slot 8 upward, the groove depth installing draw-in groove 6 compared to lower guideway due to lower guideway installation lower bayonet slot 8 is larger, it is lower that lower guideway 7 is fixed compared to formal dress lower guideway movable cushion block 4 in the anti-position loading the fixing lower guideway 7 of guide rail movable cushion block 4, thus form the launching trajectory of two kinds of different in width, the hail-proof rain-increasing rocket that simultaneously can be applicable to two kinds of different-diameters uses, can the object of double-purpose to reach; In actual use, rocket pod is equipped with multiple rocket bomb transmitting cylinder 1 usually, the launching trajectory that user can select width to be applicable at each rocket bomb transmitting cylinder 1 according to the actual demand of oneself, improves the utilization rate of rocket pod, service efficiency is high, economizes on resources.
according to actual needs, above-mentioned dual-purpose type hail-proof rain-increasing rocket launching trajectory can be made further optimization and/or improvements:
as shown in Figure 1, the top of upper rail movable cushion block 2 is provided with and groove depth corresponding with guide rail and is more than or equal to the upper rail that upper rail installs lower bayonet slot and installs draw-in groove 9.With lower guideway movable cushion block 4 in like manner, can positive and negatively use; Lower guideway movable cushion block 4 is counter fill time, because of lower guideway install the groove depth of lower bayonet slot 8 do not reach the hail-proof rain-increasing rocket installation requirements in wide footpath not time, after installing by upper rail movable cushion block 2 being reversed, width compensation is carried out to launching trajectory.
as shown in Figure 1, the two ends, left and right on the downside of lower guideway movable cushion block 4 be respectively equipped with can strengthen lower guideway movable cushion block 4 bottom area widen footing 10.
as shown in Figure 1, upper rail 3 adopts the grooved track that Open Side Down; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of upper rail 3 and upper rail movable cushion block 2, the upper end barrel of the rocket bomb transmitting cylinder 1 corresponding with connecting hole is provided with upper rail 3 fixing hole, in mutually corresponding connecting hole and upper rail 3 fixing hole, connecting bolt 11 is installed, connecting bolt 11 is installed with by screw thread the attaching nut 5 that upper rail 3, upper rail movable cushion block 2 can be fixed on rocket bomb transmitting cylinder 1 inner upper end; Lower guideway 7 adopts the grooved track of opening upwards; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of lower guideway 7 and lower guideway movable cushion block 4, the lower end barrel of the rocket bomb transmitting cylinder 1 corresponding with connecting hole is provided with lower guideway 7 fixing hole, in mutually corresponding connecting hole and lower guideway 7 fixing hole, connecting bolt 11 is installed, connecting bolt 11 is installed with by screw thread the attaching nut 5 that lower guideway 7, lower guideway movable cushion block 4 can be fixed on rocket bomb transmitting cylinder 1 interior lower end.
as shown in Figure 1, lower guideway is installed the groove depth difference that lower bayonet slot 8 and lower guideway install draw-in groove 6 and is less than or equal to 16 millimeters.In actual use, the most conventional is main based on the explosion-proof rain-increasing rocket of φ 66 12 and the explosion-proof rain-increasing rocket 13 of φ 82, when lower guideway movable cushion block 4 formal dress, under the prerequisite meeting explosion-proof rain-increasing rocket 12 use of φ 66, load guide rail movable cushion block 4 by counter, just can be directly applied for the explosion-proof rain-increasing rocket 13 of φ 82, easy to use, realize dual-purpose, utilization rate is high.
above technical characteristic constitutes most preferred embodiment of the present utility model, and it has stronger adaptability and best implementation result, can increase and decrease non-essential technical characteristic according to actual needs, meet the demand of different situations.
Claims (9)
1. a dual-purpose type hail-proof rain-increasing rocket launching trajectory, is characterized in that comprising rocket bomb transmitting cylinder, upper rail movable cushion block, upper rail, lower guideway movable cushion block and lower guideway; Be installed with upper rail movable cushion block in the inner upper end of rocket bomb transmitting cylinder, upper rail through before and after being provided with in the lower end of upper rail movable cushion block installs lower bayonet slot, installs lower bayonet slot internal fixtion be provided with upper rail at upper rail; Lower guideway movable cushion block is installed with in the interior lower end at rocket bomb transmitting cylinder, lower guideway movable cushion block top be provided with lower guideway and install draw-in groove, install draw-in groove internal fixtion at lower guideway and lower guideway is installed, between lower guideway and upper rail, form launching trajectory; Be provided with and groove depth corresponding with guide rail to be greater than the lower guideway that lower guideway installs draw-in groove in the bottom of lower guideway movable cushion block lower bayonet slot is installed.
2. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 1, is characterized in that the top of upper rail movable cushion block is provided with and groove depth corresponding with guide rail and is more than or equal to the upper rail that upper rail installs lower bayonet slot and installs draw-in groove.
3. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 1 and 2, the two ends, left and right that it is characterized in that on the downside of lower guideway movable cushion block be respectively equipped with can strengthen lower guideway movable cushion block bottom area widen footing.
4. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 1 and 2, is characterized in that upper rail adopts the grooved track that Open Side Down; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of upper rail and upper rail movable cushion block, the upper end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with upper rail fixing hole, in mutually corresponding connecting hole and upper rail fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that upper rail, upper rail movable cushion block can be fixed on rocket bomb transmitting cylinder inner upper end; Lower guideway adopts the grooved track of opening upwards; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of lower guideway and lower guideway movable cushion block, the lower end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with lower guideway fixing hole, in mutually corresponding connecting hole and lower guideway fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that lower guideway, lower guideway movable cushion block can be fixed on rocket bomb transmitting cylinder interior lower end.
5. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 3, is characterized in that upper rail adopts the grooved track that Open Side Down; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of upper rail and upper rail movable cushion block, the upper end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with upper rail fixing hole, in mutually corresponding connecting hole and upper rail fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that upper rail, upper rail movable cushion block can be fixed on rocket bomb transmitting cylinder inner upper end; Lower guideway adopts the grooved track of opening upwards; Mutually corresponding connecting hole is respectively equipped with at the middle part of the middle part of lower guideway and lower guideway movable cushion block, the lower end barrel of the rocket bomb transmitting cylinder corresponding with connecting hole is provided with lower guideway fixing hole, in mutually corresponding connecting hole and lower guideway fixing hole, connecting bolt is installed, connecting bolt is installed with by screw thread the attaching nut that lower guideway, lower guideway movable cushion block can be fixed on rocket bomb transmitting cylinder interior lower end.
6. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 1 and 2, is characterized in that lower guideway is installed the groove depth difference that lower bayonet slot and lower guideway install draw-in groove and is less than or equal to 16 millimeters.
7. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 3, is characterized in that lower guideway is installed the groove depth difference that lower bayonet slot and lower guideway install draw-in groove and is less than or equal to 16 millimeters.
8. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 4, is characterized in that lower guideway is installed the groove depth difference that lower bayonet slot and lower guideway install draw-in groove and is less than or equal to 16 millimeters.
9. dual-purpose type hail-proof rain-increasing rocket launching trajectory according to claim 5, is characterized in that lower guideway is installed the groove depth difference that lower bayonet slot and lower guideway install draw-in groove and is less than or equal to 16 millimeters.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520273095.4U CN204630479U (en) | 2015-04-30 | 2015-04-30 | Dual-purpose type hail-proof rain-increasing rocket launching trajectory |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520273095.4U CN204630479U (en) | 2015-04-30 | 2015-04-30 | Dual-purpose type hail-proof rain-increasing rocket launching trajectory |
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| Publication Number | Publication Date |
|---|---|
| CN204630479U true CN204630479U (en) | 2015-09-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520273095.4U Expired - Fee Related CN204630479U (en) | 2015-04-30 | 2015-04-30 | Dual-purpose type hail-proof rain-increasing rocket launching trajectory |
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| CN (1) | CN204630479U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108398052A (en) * | 2018-05-18 | 2018-08-14 | 新余国科特种装备有限公司 | Afocal variable rocket launching finder |
| CN108534602A (en) * | 2018-05-29 | 2018-09-14 | 湖北三江航天万峰科技发展有限公司 | The adjustment method and its regulating mechanism of the small-bore double V-shaped guide rail of firing box |
| CN111442689A (en) * | 2020-05-13 | 2020-07-24 | 河南黄烨科技有限公司 | Multi-functional transmission trainer based on modular design |
| CN111765808A (en) * | 2020-07-10 | 2020-10-13 | 北京星途探索科技有限公司 | Novel storage, transportation and delivery module |
| CN112253588A (en) * | 2020-10-14 | 2021-01-22 | 四川航天拓鑫玄武岩实业有限公司 | Guide rail assembling tool and guide rail assembling method for large-scale launching box |
-
2015
- 2015-04-30 CN CN201520273095.4U patent/CN204630479U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108398052A (en) * | 2018-05-18 | 2018-08-14 | 新余国科特种装备有限公司 | Afocal variable rocket launching finder |
| CN108534602A (en) * | 2018-05-29 | 2018-09-14 | 湖北三江航天万峰科技发展有限公司 | The adjustment method and its regulating mechanism of the small-bore double V-shaped guide rail of firing box |
| CN111442689A (en) * | 2020-05-13 | 2020-07-24 | 河南黄烨科技有限公司 | Multi-functional transmission trainer based on modular design |
| CN111442689B (en) * | 2020-05-13 | 2023-06-16 | 姜暄民 | Multifunctional emission training device based on modularized design |
| CN111765808A (en) * | 2020-07-10 | 2020-10-13 | 北京星途探索科技有限公司 | Novel storage, transportation and delivery module |
| CN112253588A (en) * | 2020-10-14 | 2021-01-22 | 四川航天拓鑫玄武岩实业有限公司 | Guide rail assembling tool and guide rail assembling method for large-scale launching box |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150909 Termination date: 20160430 |