CN205228282U - Can lock formula precipitation of hail of rockets launcher - Google Patents
Can lock formula precipitation of hail of rockets launcher Download PDFInfo
- Publication number
- CN205228282U CN205228282U CN201520987539.0U CN201520987539U CN205228282U CN 205228282 U CN205228282 U CN 205228282U CN 201520987539 U CN201520987539 U CN 201520987539U CN 205228282 U CN205228282 U CN 205228282U
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- locking
- gyroaxis
- steering wheel
- launcher
- locking plate
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- Withdrawn - After Issue
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Abstract
The utility model provides a can lock formula precipitation of hail of rockets launcher adopts wireless remote control communication and current wired connection operation to compare between its rocket launcher and the handheld machine, saved the link of unwrapping wire, plug wire, and the operating efficiency improves greatly, and time of preparation shortens 1 minute at least before the operation, have gesture locking device, drive mechanism is by the locking, can effectual elimination transmission clearance, avoid the rocket launching in the twinkling of an eye the launcher that arouses of transmission clearance rock, has improved the rocket launching precision and has protected drive mechanism, the revolving axle is a hollow shaft, the interior threading that conceals of hollow shaft, and when having avoided the operation of emitter direction, the cable winding is dragged and is caused the damage, and the while also avoids the cable to expose to the sun and rain for a long time and the ablation of rocket wake flame causes damage, increase of service life, has the automatic re -setting function. The utility model discloses after the operation, manual operation and judgement have been saved to the automatic resetting of zero of emitter meeting, and degree of automation is high.
Description
Technical field
The utility model belongs to Weather modification operation technical field of tools, and being specifically related to one can locking type rain-increasing hail suppression rocket launcher.
Background technology
Current rainfall-increasing and anti-hail rocket (being called for short afterwards: rocket) has become the main tool of Weather modification operation, and rocket pod, as the flat pad of rocket, plays an important role in drinking water project.Existing launcher demarcates directive by manual drive, manually, site layout project launches cable, operation sequence very complicated, and all there is drive gap in launcher, rocket launching moment wake flame impacts launcher, drive gap can cause launcher to rock, and affects rocket launching precision, and when launcher rocks, gear in transmission mechanism can collide mutually, affects service life.
Utility model content
In view of this, the purpose of this utility model is to provide one can locking type rain-increasing hail suppression rocket launcher, improves rocket launching precision.
Of the present utility model can locking type rain-increasing hail suppression rocket launcher, it comprises: electronic compass, finder, elevating mechanism, rotary disk, steering wheel, base, battery and hand-held set; Ancillary equipment is rainfall-increasing and anti-hail rocket, and this rainfall-increasing and anti-hail rocket is installed in finder;
Base is supported on ground; Battery and steering wheel are fixed on above base; Rotary disk is installed on steering wheel, and the gyroaxis of steering wheel is connected with rotary disk; Elevating mechanism is installed on rotary disk, and finder is arranged on the telescopic shaft of elevating mechanism, and electronic compass is arranged on the top of finder, and electronic compass is measured the attitude information of whole launcher and fed back on hand-held set by this attitude information; Wherein establish locking device and gyroaxis in steering wheel, by the locking plate hoop locking of locking device by gyroaxis and locking device, eliminate drive gap.
Further, steering wheel comprises: gyroaxis, locking device, pedestal, axle sleeve, decelerator and motor;
Wherein, pedestal is section bar weldment, and centre is provided with through hole; Axle sleeve is a torus, and upper and lower end face is all flange face; Gyroaxis is a hollow rotary body, and head is a mounting flange, and neck is locking mating surface, and tailing axle place has long keyway;
Pedestal is fixed on base; Axle sleeve is arranged in the through hole of pedestal; Gyroaxis is arranged in axle sleeve by two secondary taper roll bearings; Locking device is enclosed within gyroaxis upper end neck, and is arranged on the upper surface of axle sleeve; Delivery outlet on decelerator is placed on the lower end of gyroaxis, and is coupled together by key; The motor shaft of motor is connected with decelerator.
Further, locking device comprises: locking plate, catch, locking stud, manual locking bar, electric pushrod;
Locking plate is open circles loop configuration, and outer ring is ring flange, and locking plate opening part side is labeled as A opposite side and is labeled as B, and size two through holes are respectively opened in A, B both sides, and wherein A side aperture is screwed hole; Locking stud is the studs of an Intermediate Gray shaft shoulder, and shaft shoulder both sides thread segment length is not etc.; Catch is the sequin of a central aperture;
Locking plate is arranged on the axle sleeve upper surface of steering wheel by outer ring flange, and locking plate is enclosed within the neck of the gyroaxis of steering wheel, and locking plate and gyroaxis do matched in clearance; Manual locking bar is through locking plate opening part B side aperture, and A side screwed hole does threaded engagement; Electric pushrod is arranged on locking plate opening part A side, and manual locking pole pair claims to install; The short thread head of locking stud is arranged on the telescopic shaft head of electric pushrod, and long thread head is through locking plate opening part B side; Catch passes through middle circle borehole jack on the long thread segment of locking stud, and is fixed on locking stud by two nuts.
The utility model has following beneficial effect:
Wireless remote control communication is adopted between 1 rocket projector and hand-held set, compare with existing wired connection operation, eliminate the link of unwrapping wire, plug wire, operating efficiency improves greatly, before operation, time at least shortens 1 minute (illustrating: because the spatial domain time is short, so General Requirements operating speed wants fast).
2 have attitude locking device, and transmission mechanism, by locking, effectively can eliminate drive gap, and the launcher avoiding rocket launching moment drive gap to cause rocks, and improves rocket launching precision and protects transmission mechanism.
3 gyroaxises are a hollow shaft, hidden threading in hollow shaft, and when avoiding the running of emitter direction, cable winds is pullled and caused damage, simultaneously also avoid cable chronic sun exposure to drench with rain and the ablation of rocket wake flame causes damage, increase the service life.
4 have auto-reset function.After the end of job, emitter can automatically return to zero-bit, and eliminate manual operation and judgement, automaticity is high.
Accompanying drawing explanation
Fig. 1 general construction schematic diagram of the present utility model;
Fig. 2 direction mechanism schematic diagram;
Fig. 3 base construction schematic diagram;
Fig. 4 axle sleeve structure schematic diagram;
Fig. 5 gyroaxis structural representation;
Fig. 6 direction locking structural scheme of mechanism;
Fig. 7 locking plate structural representation;
Fig. 8 locking screw rod structure schematic diagram.
1-electronic compass, 2-finder, 3-elevating mechanism, 4-rotary disk, 5-steering wheel, 6-base, 7-battery, 8-hand-held set, 9-gyroaxis, 10-locking device, 11-pedestal, 12-axle sleeve, 13-decelerator, 14-motor, 15-locking plate, 16-catch, 17-lock stud, 18-manual locking bar, 19-electric pushrod.
Detailed description of the invention
To develop simultaneously embodiment below in conjunction with accompanying drawing, the utility model is described in detail.
See accompanying drawing 1, can comprise by locking type rain-increasing hail suppression rocket launcher: electronic compass 1, finder 2, elevating mechanism 3, rotary disk 4, steering wheel 5, base 6, battery 7, hand-held set 8.Base 6 is positioned at the bottom of whole launcher, battery 7 and steering wheel 5 are arranged on above base 6, battery 7 provides electric energy for whole launcher, the gyroaxis of steering wheel 5 is connected with rotary disk 4, and elevating mechanism 3 is installed based on rotary disk 4, and finder 2 is arranged on elevating mechanism 3, for installing, firing a rocket, electronic compass 1 is arranged on the top of finder 2, measures the attitude information of whole launcher, and feeds back on hand-held set 8 by this attitude information; Wherein establish locking device 10 and gyroaxis 9 in steering wheel 5, by the locking plate 15 hoop locking of locking device 10 by gyroaxis 9 and locking device 10, eliminate drive gap; Hand-held set 8 is an independent integers, and launcher wireless remote control communication, for the motion of operation issue frame and display launcher status information.
See accompanying drawing 2, in the utility model, steering wheel 5 comprises: gyroaxis 9, locking device 10, pedestal 11, axle sleeve 12, decelerator 13, motor 14.Pedestal 11 is section bar weldment, in stool shape (see accompanying drawing 3), is the foundation of whole launcher, is arranged on base 6.Axle sleeve 12 (see accompanying drawing 4) is a torus, upper and lower end face is all flange face, be arranged in pedestal 11, gyroaxis 9 (see accompanying drawing 5) is a hollow rotary body, head is a mounting flange, neck is locking mating surface, tailing axle place has long keyway, gyroaxis 9 is arranged in axle sleeve 12 by two secondary taper roll bearings, locking device 10 is enclosed within gyroaxis 9 upper end neck, and be arranged on the upper surface of axle sleeve 12, delivery outlet on decelerator 13 is placed on the lower end of gyroaxis 9, and coupled together by key, for transmitting torque, motor 14 is arranged on the input of decelerator 13, for steering wheel 5 provides power.
The working procedure of steering wheel 5 is: motor 14 powers on rotation, and by decelerator 13, power augmentation is delivered to gyroaxis 9, gyroaxis 9 is connected with elevating mechanism 3 above, and elevating mechanism 3 is connected with finder again, so finally driving finder 2 rotates.Because decelerator 13 is worm type of reduction gearing, between worm gear and worm screw, there is drive gap, gyroaxis 9 can be caused axially to rock, finally cause finder 2 to rock on direction, affect launch accuracy.So after treating azimuth adjustment, locking device 10 starts action, by the locking of gyroaxis 9 hoop, play locking attitude, eliminate the effect of drive gap.
See accompanying drawing 6, locking device 10 comprises: locking plate 15, catch 16, locking stud 17, manual locking bar 18, electric pushrod 19.Locking plate 15 (see accompanying drawing 7) is open circles loop configuration, and outer ring is ring flange, and opening part is " duckbilled " shape structure, locking plate 15 opening part side is labeled as A, opposite side is labeled as B, and size two through holes are respectively opened in A, B both sides, and wherein A side aperture is screwed hole.Locking plate 15 is arranged on the upper surface of axle sleeve 12 by outer ring flange, and is enclosed within the neck of gyroaxis 9, does matched in clearance.Manual locking bar 18 is through locking plate 15 opening part B side aperture, and A side screwed hole does threaded engagement.Electric pushrod 19 is arranged on locking plate 15 opening part A side, and manual locking bar 18 symmetry is installed.Locking stud 17 (see accompanying drawing 8) is the studs of an Intermediate Gray shaft shoulder, and not etc., short thread head is not arranged on the telescopic shaft head of electric pushrod 19 to shaft shoulder both sides thread segment length, and long thread head is then through locking plate 15 opening part B side.Catch 16 is the sequin of a central aperture, by middle circle borehole jack on the long thread segment of locking stud 17, then installs two nuts below on locking stud 17 at catch 16, the slippage of anti-stop tab 16.
Locking device 10 operation principle is: electric pushrod 19 be energized telescopic shaft head shrink, locking stud 17 is driven to shrink together, because two nut restriction catch 16 of locking stud 17 end move backward, so the contraction clamping force between electric pushrod 19 and catch 16 puts on keyboard 15 opening part A, B both sides, along with the distance of A, B both sides reduces gradually, locking plate 15 annulus place diameter can slowly diminish, until consistent with gyroaxis 9 recess diameter, then continue force, thus play the effect of holding tightly.During unblock, electric pushrod 19 telescopic shaft stretches out, and discharges the enclasping force to locking plate 15, and locking plate 15 is by the elasticity of itself, and affranchise state.Manual locking bar 18 uses when launcher electricity deficiency, its action principle is: turn clockwise handle, check lock lever head threads section is advanced forward, the check lock lever back segment shaft shoulder is locked dish 15 opening part B side block firmly, while screw thread is advanced, the shaft shoulder can push in locking plate 15 opening part B side direction and move, thus forms clamping force.During release clamping force, be rotated counterclockwise handle.
In sum, these are only preferred embodiment of the present utility model, be not intended to limit protection domain of the present utility model.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (3)
1. one kind can locking type rain-increasing hail suppression rocket launcher, it is characterized in that, comprising: electronic compass (1), finder (2), elevating mechanism (3), rotary disk (4), steering wheel (5), base (6), battery (7) and hand-held set (8); Ancillary equipment is rainfall-increasing and anti-hail rocket, and this rainfall-increasing and anti-hail rocket is installed in finder (2);
Base (6) is supported on ground; Battery (7) and steering wheel (5) are fixed on above base (6); Rotary disk (4) is installed on steering wheel (5), and the gyroaxis of steering wheel (5) is connected with rotary disk (4); Elevating mechanism (3) is installed on rotary disk (4), finder (2) is arranged on the telescopic shaft of elevating mechanism (3), electronic compass (1) is arranged on the top of finder (2), and electronic compass (1) is measured the attitude information of whole launcher and fed back to by this attitude information on hand-held set (8); Wherein establish locking device (10) and gyroaxis (9) in steering wheel (5), by locking plate (15) the hoop locking of locking device (10) by gyroaxis (9) and locking device (10), eliminate drive gap.
2. as claimed in claim 1 can locking type rain-increasing hail suppression rocket launcher, it is characterized in that, steering wheel (5) comprising: gyroaxis (9), locking device (10), pedestal (11), axle sleeve (12), decelerator (13) and motor (14);
Wherein, pedestal (11) is section bar weldment, and centre is provided with through hole; Axle sleeve (12) is a torus, and upper and lower end face is all flange face; Gyroaxis (9) is a hollow rotary body, and head is a mounting flange, and neck is locking mating surface, and tailing axle place has long keyway;
Pedestal (11) is fixed on base (6); Axle sleeve (12) is arranged in the through hole of pedestal (11); Gyroaxis (9) is arranged in axle sleeve (12) by two secondary taper roll bearings; Locking device (10) is enclosed within gyroaxis (9) upper end neck, and is arranged on the upper surface of axle sleeve (12); Delivery outlet on decelerator (13) is placed on the lower end of gyroaxis (9), and is coupled together by key; The motor shaft of motor (14) is connected with decelerator (13).
3. as claimed in claim 2 can locking type rain-increasing hail suppression rocket launcher, it is characterized in that,
Locking device (10) comprising: locking plate (15), catch (16), locking stud (17), manual locking bar (18), electric pushrod (19);
Locking plate (15) is open circles loop configuration, and outer ring is ring flange, and locking plate (15) opening part side is labeled as A opposite side and is labeled as B, and size two through holes are respectively opened in A, B both sides, and wherein A side aperture is screwed hole; Locking stud (17) is the studs of an Intermediate Gray shaft shoulder, and shaft shoulder both sides thread segment length is not etc.; Catch (16) is the sequin of a central aperture;
Locking plate (15) is arranged on axle sleeve (12) upper surface of steering wheel (5) by outer ring flange, and locking plate (15) is enclosed within the neck of the gyroaxis (9) of steering wheel (5), locking plate (15) and gyroaxis (9) do matched in clearance; Manual locking bar (18) is through locking plate (15) opening part B side aperture, and A side screwed hole does threaded engagement; Electric pushrod (19) is arranged on locking plate (15) opening part A side, and manual locking bar (18) symmetry is installed; The short thread head of locking stud (17) is arranged on the telescopic shaft head of electric pushrod (19), and long thread head is through locking plate (15) opening part B side; Catch (16) by middle circle borehole jack locking stud (17) long thread segment on, and by two nuts be fixed on locking stud (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520987539.0U CN205228282U (en) | 2015-12-02 | 2015-12-02 | Can lock formula precipitation of hail of rockets launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520987539.0U CN205228282U (en) | 2015-12-02 | 2015-12-02 | Can lock formula precipitation of hail of rockets launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205228282U true CN205228282U (en) | 2016-05-11 |
Family
ID=55903339
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520987539.0U Withdrawn - After Issue CN205228282U (en) | 2015-12-02 | 2015-12-02 | Can lock formula precipitation of hail of rockets launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205228282U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105466285A (en) * | 2015-12-02 | 2016-04-06 | 陕西中天火箭技术股份有限公司 | Rain enhancement hail-suppression rocket launcher capable of being locked |
| CN107064562A (en) * | 2017-04-20 | 2017-08-18 | 吉林宇恒光电仪器有限责任公司 | A kind of caliberating device of photoelectric encoder output speed error |
-
2015
- 2015-12-02 CN CN201520987539.0U patent/CN205228282U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105466285A (en) * | 2015-12-02 | 2016-04-06 | 陕西中天火箭技术股份有限公司 | Rain enhancement hail-suppression rocket launcher capable of being locked |
| CN107064562A (en) * | 2017-04-20 | 2017-08-18 | 吉林宇恒光电仪器有限责任公司 | A kind of caliberating device of photoelectric encoder output speed error |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160511 Effective date of abandoning: 20170613 |