CN106197146A - A kind of rocket model and the adjustable rocket launch platform of attitude - Google Patents
A kind of rocket model and the adjustable rocket launch platform of attitude Download PDFInfo
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- CN106197146A CN106197146A CN201610664148.4A CN201610664148A CN106197146A CN 106197146 A CN106197146 A CN 106197146A CN 201610664148 A CN201610664148 A CN 201610664148A CN 106197146 A CN106197146 A CN 106197146A
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- motor
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- side chain
- revolute pair
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
Abstract
A kind of rocket model of present invention proposition and the adjustable rocket launch platform of attitude, belong to rocket projector technical field, including launching framework, moving platform, support platform, fixed platform, supporting leg, the first side chain to the 9th side chain；Wherein, first, second, and third side chain is the most uniform is fastened on transmitting framework；4th and the 5th side chain is connected to launch between framework and support platform, and with launch framework and support platform Special composition close loop mechanism；6th side chain is connected between support platform and moving platform；Seven, the 8th and the 9th side chain is connected to move, between fixed platform, and with dynamic, fixed platform Special composition close loop mechanism；Three supporting legs are positioned at bottom fixed platform the most uniform, and each supporting leg one end is fastened by bolt and fixed platform, the other end is anchored on transmitting ground by ground nail；The present invention has compact conformation, and operating mode is adaptable, and pose adjustment is flexible, controls the features such as relatively easy, can realize the transmitting of different model rocket.
Description
Technical field
The invention belongs to rocket projector technical field, particularly to a kind of rocket model and the adjustable rocket of attitude
Flat pad.
Background technology
Along with weather modification engineering and the development of model spacecraft sports, rocket launching is the most distant from us
Far, rocket projector and transmitting technique have become as raising emission effciency, affect the important technology of launching effect.
Weather modification, refers to as avoiding or alleviate meteorological disaster, Appropriate application climate resources, under proper condition
By technological means, physics, the chemical process of local atmosphere are carried out artificial affecting, it is achieved increase sleet, hail suppression, the rain that disappears, fog dispersal,
The activity of the purposes such as frost prevention.Specific to implementation process, the chemical reagent affecting weather is loaded in aircraft or rocket etc. by people
On aircraft, aircraft is utilized to bring reagent into target cloud layer.Owing to aircraft loads relatively costly, the most most of areas select
Rocket is utilized to complete loading task.When needs weather modification, operator need to take out launcher from warehouse, use vapour
Car traction is to depletion region, and owing to depletion region landform majority is uneven, therefore operator need to take time constantly for sending out
Penetrate frame centering, the most not only affect emission effciency, and launching time may be delayed.In addition, for different
Weather modification purpose, required rocket model is different, and therefore, relevant departments need to equip many moneys launcher, increases
Launch cost.
On the other hand, the rise of model spacecraft sports, provide to more teenager and start to put into practice and theoretical
The platform of innovation, " the Aero-Space model championship of the scientific research class whole nation " held such as General Administration of Sport just has " model spacecraft
Project ".This project itself has a hard requirement, and the rocket i.e. launched needs to reach 30 meters of plumb heights, and games results just have
Effect.So needing " the chasing after wind " according to rocket to adjust rocket launching attitude when meeting with strong wind weather.Further, since each competition
Can register three groups of matches in side, so having been resolved for the different model rocket launching problem needs under different schemes.
At present in weather modification engineering field, most of launcher function singlenesses, i.e. can only realize launching pitching
The regulation of angle.In model spacecraft sports, most launchers only realize the effect that perpendicular positioning is launched.
Summary of the invention
It is an object of the invention to the demand in view of two above field and the deficiencies in the prior art, it is proposed that a kind of rocket type
Number and the adjustable rocket launch platform of attitude, in the case of this flat pad can realize complicated landform, different model rocket
Launch, there is the features such as pose adjustment is flexible, the switching of rocket model is simple.
A kind of rocket model of present invention proposition and the adjustable rocket launch platform of attitude, it is characterised in that this rocket
Flat pad include launch framework, moving platform, support platform, fixed platform, supporting leg, the first side chain, the second side chain, the 3rd
Chain, the 4th side chain, the 5th side chain, the 6th side chain, the 7th side chain, the 8th side chain and the 9th side chain；Wherein, first, second He
3rd side chain is the most uniform to be fastened on transmitting framework；4th and the 5th side chain is connected to launch framework and support platform
Between, and with launch framework and support platform Special composition close loop mechanism；6th side chain be connected to support platform and moving platform it
Between；Seven, the 8th and the 9th side chain is connected between moving platform and fixed platform, and with moving platform and fixed platform Special composition
Close loop mechanism；Three supporting legs are positioned at bottom fixed platform the most uniform, and each supporting leg one end is tight with fixed platform by bolt
Gu, the other end by ground nail be anchored on transmitting ground.
The feature of the present invention and beneficial effect:
A kind of rocket model and the adjustable rocket launch platform of attitude that the present invention relates to can apply to artificial affecting
Weather engineering and model spacecraft sports, it is possible in the case of realizing complicated landform, the transmitting of different model rocket, have knot
The features such as structure is compact, operating mode is adaptable, pose adjustment is flexible, the switching of rocket model is simple.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention 1；
Fig. 2 is the first side chain I of the embodiment of the present invention 1, the second side chain II, the 3rd side chain III schematic diagram；
Fig. 3 is the partial enlarged drawing of the embodiment of the present invention 1；
Fig. 4 is the structural representation of the embodiment of the present invention 2；
Fig. 5 is the first side chain I of the embodiment of the present invention 2, the second side chain II, the 3rd side chain III schematic diagram；
Detailed description of the invention
It is detailed that a kind of rocket model of present invention proposition and the adjustable rocket launch platform of attitude combine drawings and Examples
Carefully it is described as follows:
Embodiment 1:
A kind of overall structure such as Fig. 1 institute of the rocket model of the implementation case and the adjustable rocket launch platform of attitude
Show, including launch framework 5, moving platform 27, support platform 28, fixed platform 21, supporting leg the 20, first side chain, the second side chain, the 3rd
Side chain, the 4th side chain, the 5th side chain, the 6th side chain, the 7th side chain, the 8th side chain and the 9th side chain (described first to the 9th
I to IX in side chain i.e. Fig. 1)；The annexation of each parts is: the first side chain I, the second side chain II, the 3rd side chain III circumference are equal
Cloth is fastened on transmitting framework 5；4th side chain IV, the 5th side chain V are connected to launch between framework 5 and support platform 28,
And with launch framework 5 and support platform 28 Special composition close loop mechanism；6th side chain VI is connected to support platform 28 and moving platform
Between 27；7th side chain VII, the 8th side chain VIII, the 9th side chain IX are connected between moving platform 27 and fixed platform 21, and
With moving platform 27 and fixed platform 21 Special composition close loop mechanism；Article three, supporting leg 20 is positioned at bottom fixed platform 21 the most uniform,
Each supporting leg 20 one end is fastened by bolt and fixed platform 21, the other end is anchored on transmitting ground by ground nail.
Described first side chain I, the second side chain II, the 3rd side chain III structure are identical, as in figure 2 it is shown, all include: upper end is shaken
Bar 1, upper end guide rail 2, upper end motor 3, expansion link 4, lowermost guide rail 6, lower end rocking bar 7, lower end motor 8 and kinematic pair；Each portion
The assembly relation of part is: upper end motor 3 and lower end motor 8 are fastened by bolts respectively in the motor slot launched on framework 5, on
End motor 3 output shaft is bonded with upper end rocking bar 1 and lower end motor 8 output shaft with lower end rocking bar 7, upper end rocking bar 1 and
Upper end guide rail 2 and lower end rocking bar 7 are all connected by pivot pin with lowermost guide rail 6, and upper end guide rail 2 and expansion link 4 pass through the face of cylinder
Cooperatively forming axial moving sets, expansion link 4 is tightened together by radial screw with lowermost guide rail 6；Described kinematic pair has 5
Individual, a revolute pair being between upper end motor 3 output shaft and upper end rocking bar 1, one is in upper end rocking bar 1 and upper end
Revolute pair between guide rail 2, a moving sets being between upper end guide rail 2 and expansion link 4, one is in lowermost guide rail
Revolute pair between 6 and lower end rocking bar 7, another is in the revolute pair between lower end rocking bar 7 and lower end motor 8 output shaft；
Described 5 kinematic pairs are in same plane, wherein, and the revolute pair between upper end motor 3 output shaft and upper end rocking bar 1
And the revolute pair between lower end rocking bar 7 and lower end motor 8 output shaft is powered；Upper end motor 3 and lower end motor 8
Synchronous backward drives so that upper end guide rail 2 and lowermost guide rail 6 form straight line guide rail, and this line slideway is parallel to by upper end
The plane that motor 3 and lower end motor 8 axis are constituted.
The structure of described 4th side chain IV is as it is shown in figure 1, include: bearing block 9, carrying axle 10, bearing 11, regulating block
12 and kinematic pair；The assembly relation of described each parts is: bearing block 9 is fastened by bolts with launching framework 5, bearing block 9 with
Carrying axle 10 forms revolute pair by bearing fit, and carrying axle 10 is tightened together by radial screw with a bearing 11, supporting
Together with seat 11, regulating block 12 are fastened by bolts with support platform 28；Described kinematic pair has 1, is i.e. positioned at bearing block 9 and holds
Carry the revolute pair between axle 10.
The structure of described 5th side chain V (Fig. 3 is seen in local) as shown in Figure 1, including: connecting shaft 13, leading screw pedestal 14, supporting
Seat 15, motor 29, motor cabinet 31, shaft coupling frame 32, slide block 33, connecting rod 35, leading screw 36, a bearing 37, connecting shaft 38 and fortune
Dynamic pair；The assembly relation of described each parts is for (referring to Fig. 3, Fig. 1 is seen in local): motor cabinet 31 is with shaft coupling frame 32 by screw even
Connect, shaft coupling frame 32 with leading screw pedestal 14 is connected by screw, leading screw pedestal 14 is fastened in support platform 28 by screw, electric
Machine 29 is fastened by bolts on motor cabinet 31, and leading screw 36 forms revolute pair, slide block 33 with leading screw pedestal 14 by bearing fit
Forming moving sets with leading screw 36 by threaded engagement, slide block 33 is fastened by screw with a bearing 15, bearing 15 and connecting shaft
13 are fastened by radial screw, and connecting shaft 13 forms revolute pair with connecting rod 35 by bearing fit, and connecting rod 35 leads to connecting shaft 38
Crossing bearing fit and form revolute pair, connecting shaft 38 is fastened by radial screw with a bearing 37, and a bearing 37 is by bolt and sends out
Penetrate framework 5 to tighten together；Described kinematic pair has 4, a revolute pair being between leading screw pedestal 14 and leading screw 36, and one
The individual moving sets being between leading screw 36 and slide block 33, a revolute pair being between connecting shaft 13 and connecting rod 35, separately
One revolute pair being between connecting rod 35 and connecting shaft 38；In described 4 kinematic pairs, it is positioned at leading screw pedestal 14 and leading screw 36
Between revolute pair driven by motor 29.
The structure of described 6th side chain VI (Fig. 3 is seen in local) as shown in Figure 1, including: motor 34, gear 30, upper thrust ring
16, ring gear 17 and lower thrust ring 18 and kinematic pair；The assembly relation of described each parts is: upper thrust ring 16 and support platform 28
Being fastened by screw, upper thrust ring 16 inner cylinder face forms revolute pair, upper thrust ring 16 following table with ring gear 17 by floating bearing
Face forms revolute pair with lower thrust ring 18 upper surface by end face bearing, and ring gear 17 is tight by radial screw with lower thrust ring 18
Gu, lower thrust ring 18 is fastened by screw with moving platform 27, and motor 34 is fastened by bolts the motor slot in support platform 28
In, motor 34 output shaft and gear 30 are by bonded, and gear 30 engages with ring gear 17；Described kinematic pair has 4, and one is position
Revolute pair between gear 30 and motor 34 output shaft, one is in being formed by engagement between gear 30 and ring gear 17
Higher pair, a revolute pair formed by end face bearing being between thrust ring 16 and lower thrust ring 18, another is
The revolute pair formed by floating bearing between upper thrust ring 16 and ring gear 17；In described 4 kinematic pairs, only it is positioned at
Revolute pair that the face of cylinder in throw-out collar 16 is formed by floating bearing with ring gear 17 and upper thrust ring 16 lower surface and lower thrust
Ring 18 upper surface is overlapped by the revolute pair that end face bearing is formed and is equivalent to same revolute pair, and the rotation of gear 30 is by motor
34 drivings.
Described 7th side chain VII, the 8th side chain VIII, the 9th side chain IX structure are identical, as it is shown in figure 1, all include: ball pivot
26, connecting rod 25, slide block 23, gear 19, rack bar 22 and motor 24 and kinematic pair；The assembly relation of described each parts is: ball
Hinge 26 is connected with moving platform 27 ball pair, and ball pivot 26 is fastened by screw with connecting rod 25, and connecting rod 25 is connected by pivot pin with slide block 23
Forming revolute pair, slide block 23 and rack bar 22 cooperatively form moving sets by cylinder, and rack bar 22 one end is anchored on by welding
On fixed platform 21 and the most uniform, motor 24 is fastened by bolts in the motor slot on slide block 23, motor 24 output shaft with
Gear 19 is by bonded, and gear 19 engages with rack bar 22；Described kinematic pair has 5, and one is in moving platform 27 and ball
Ball between hinge 26 is secondary, and a revolute pair being between connecting rod 25 and slide block 23, one is in slide block 23 and rack bar
Moving sets between 22, a revolute pair being between gear 19 and motor 24 output shaft, another is in gear 19
And the higher pair formed by rack and pinion engagement between rack bar 22；In described 5 kinematic pairs, the rotation of gear 19 is by electric
Machine 24 drives.
The rocket launch platform of the present embodiment has four basic functions: 1. rocket model (diameter) is adjustable；2. launch and bow
Face upward adjustable angle；3. gantry angle of rotation is adjustable；4. plateau levels pose ensures.It is described in detail below:
Function is 1.: rocket model (diameter) is adjustable
Described function 1. (rocket model is adjustable) is realized by with lower component: launch framework the 5, first side chain I, the second side chain II
With the 3rd side chain III.
Operation principle is: described first side chain I, the second side chain II, the 3rd side chain III action simultaneously, forms three straight lines
Guide rail, thus envelope becomes a face of cylinder, this face of cylinder is the containment surfaces of rocket external cylindrical surface；Control the motor of three side chains
Operating angle, can control the diameter of described containment surfaces, and then realize rocket model adjustable control.
Function is 2.: launch luffing angle adjustable
2. described function (is launched luffing angle adjustable) and is realized by with lower component: launch framework 5, support platform the 28, the 4th
Side chain IV and the 5th side chain V.
Operation principle is: described 4th side chain IV, five kinematic pairs of the 5th side chain V are in same plane；Control
The rotation of motor 29, can realize launching framework 5 and rotate around carrying axle 10, thus realize the regulation control of rocket launching luffing angle
System.
Function is 3.: gantry angle of rotation is adjustable
Described function 3. (gantry angle of rotation is adjustable) is realized by with lower component: support platform the 28, the 6th side chain VI and dynamic
Platform 27.
Operation principle is: controls motor 34 and rotates, it is possible to achieve gear 30 rotates around ring gear 17, and wherein, gear 30 can carry
Dynamic support platform 28 rotates, and moving platform 27 is static relative to ring gear 17, thus realizes support platform 28 and rotate relative to moving platform 27
The regulation of angle controls.
Function is 4.: plateau levels pose ensures
Described function 4. (guarantee of plateau levels pose) is realized by with lower component: moving platform 27, fixed platform 21, three support
Lower limb 20 and the seven, the eight, the 9th side chains.
Operation principle is: controls motor 24 and rotates, it is possible to achieve gear 19 moves along rack bar 22, wherein, and gear 19
Can move by band movable slider 23, rack bar 22 is static relative to fixed platform 21；Described seven, the eight, the 9th side chains are flat with dynamic respectively
Platform 27 and fixed platform 21 connect and form a Spatial Parallel close loop mechanism, this Spatial Parallel close loop mechanism by the 7th, the 8th, the
The input motion of nine three motors 24 of side chain drives moving platform 27 to move, and can realize two rotational freedoms of moving platform 27, from
And the regulation realizing relative fixed platform 21 horizontal attitude of moving platform 27 controls；Fixed platform 21 and supporting leg 20 are fastened by bolts, and 3
The end of bar supporting leg 20 determines a plane, can be anchored on transmitting ground by ground nail, therefore can realize moving platform 27 phase
Regulation to launching ground horizontal attitude controls.
Embodiment 2:
The overall structure of the present embodiment as shown in Figure 4, the difference with embodiment 1 be the first side chain I, the second side chain II and
The structure of the 3rd side chain III.
Described first side chain I, the second side chain II, the 3rd side chain III structure are identical, as it is shown in figure 5, all include: upper end is shaken
Bar 1, guide rail 02, support shaft 03, lower end rocking bar 7, lower end motor 8 and kinematic pair；The assembly relation of described each parts is: supporting
Axle 03 and upper end rocking bar 1 connect formation revolute pair, upper end rocking bar 1 and guide rail 02 and guide rail 02 and lower end rocking bar 7 by bearing
All being connected by pivot pin, lower end rocking bar 7 and lower end motor 8 output shaft are by bonded, and lower end motor 8 is fastened by bolts to be sent out
Penetrate in the motor slot on framework 5；Described kinematic pair has 4, a rotation being between support shaft 03 and upper end rocking bar 1
Pair, a revolute pair being between upper end rocking bar 1 and guide rail 02, one is between guide rail 02 and lower end rocking bar 7
Revolute pair, another is in the revolute pair between lower end rocking bar 7 and lower end motor 8 output shaft；Described 4 kinematic pairs are in
In same plane, wherein, the revolute pair being connected between lower end rocking bar 7 and lower end motor 8 output shaft is powered, by under
The driving of end motor 8 makes guide rail 02 do planar movement.
The all parts forming rocket launch platform of the present invention is conventional parts, can enter according to concrete use demand
Row selects.
Claims (10)
1. a rocket model and the adjustable rocket launch platform of attitude, it is characterised in that this rocket launch platform includes sending out
Penetrate framework, moving platform, support platform, fixed platform, supporting leg, the first side chain, the second side chain, the 3rd side chain, the 4th side chain, the 5th
Side chain, the 6th side chain, the 7th side chain, the 8th side chain and the 9th side chain；Wherein, first, second, and third side chain is the most equal
Cloth is fastened on transmitting framework；4th and the 5th side chain is connected to launch between framework and support platform, and with launch frame
Frame and support platform Special composition close loop mechanism；6th side chain is connected between support platform and moving platform；7th, the 8th and
Nine side chains are connected between moving platform and fixed platform, and with moving platform and fixed platform Special composition close loop mechanism；Three
Support leg is positioned at bottom fixed platform the most uniform, and each supporting leg one end is fastened by bolt and fixed platform, the other end passes through ground
Clench and be fixed in transmitting ground.
2. rocket launch platform as claimed in claim 1, it is characterised in that described first, second, and third branched structure phase
With, all include upper end rocking bar, upper end guide rail, upper end motor, expansion link, lowermost guide rail, lower end rocking bar, lower end motor and motion
Secondary；Wherein, described upper end motor and lower end motor are fastened by bolts respectively in the motor slot launched on framework, expansion link with
Lowermost guide rail is tightened together by radial screw；Described kinematic pair has 5, and one is in upper end motor output shaft and upper end
By the revolute pair of bonded formation between rocking bar, one is between upper end rocking bar and upper end guide rail connecting shape by pivot pin
The revolute pair become, one is between upper end guide rail and expansion link cooperatively forming axial moving sets by the face of cylinder, one
Be between lowermost guide rail and lower end rocking bar by pivot pin connect formed revolute pair, another be in lower end rocking bar and under
By the revolute pair of bonded formation between end motor output shaft.
3. rocket launch platform as claimed in claim 2, it is characterised in that described 5 kinematic pairs are in same plane；
Wherein, revolute pair between upper end motor output shaft and upper end rocking bar and be positioned at lower end rocking bar and lower end motor output shaft
Between revolute pair be powered；Upper end motor and lower end motor in synchrony reverse drive so that upper end guide rail and lowermost guide rail
Forming straight line guide rail, this line slideway is parallel to the plane being made up of upper end motor and lower end electrical axis.
4. rocket launch platform as claimed in claim 1, it is characterised in that described 4th side chain include bearing block, carrying axle,
Prop up bearing (11), regulating block and kinematic pair；Wherein, described bearing block is fastened by bolts with launching framework, carries axle and props up
Bearing (11) is fastened by radial screw, and a bearing (11), regulating block are fastened by bolts with support platform；Described kinematic pair has
1, the revolute pair i.e. formed by bearing fit between bearing block and carrying axle.
5. rocket launch platform as claimed in claim 1, it is characterised in that described 5th side chain includes the first connecting shaft
(13), leading screw pedestal, first bearing (15), motor (29), motor cabinet, shaft coupling frame, slide block (33), connecting rod (35), leading screw,
Second bearing (37), the second connecting shaft (38) and kinematic pair；Wherein, motor cabinet is connected by screw with shaft coupling frame, joins
Axial organ frame is with leading screw pedestal 14 is connected by screw, leading screw pedestal 14 is fastened in support platform by screw, and motor (29) leads to
Crossing bolt to be fastened on motor cabinet, slide block (33) is fastened by screw with first bearing (15), first bearing (15) and the
One connecting shaft (13) is fastened by radial screw, and the second connecting shaft (38) is fastened by radial screw with second bearing (37),
Second bearing (37) is fastened by bolts is launching on framework；Described kinematic pair has 4, and one is in leading screw pedestal and silk
The revolute pair formed by bearing fit between thick stick, one is in being formed by threaded engagement between leading screw and slide block (33)
Moving sets, one is between the first connecting shaft (13) and connecting rod (35) revolute pair formed by bearing fit, another
It is between connecting rod (35) and the second connecting shaft (38) revolute pair formed by bearing fit；Described be positioned at leading screw pedestal and
Revolute pair between leading screw is driven by motor (29).
6. rocket launch platform as claimed in claim 1, it is characterised in that described 6th side chain includes motor (34), gear
(30), upper thrust ring, ring gear, lower thrust ring and kinematic pair；Wherein, upper thrust ring is fastened by screw with support platform, tooth
Ring is fastened by radial screw with lower thrust ring, and lower thrust ring is fastened by screw with moving platform, and motor (34) is tight by bolt
Gu in the motor slot in support platform；Described kinematic pair has 4, one be in gear (30) and motor (34) output shaft it
Between by the revolute pair of bonded formation, one is between gear (30) and ring gear the higher pair formed by engagement, one
Being between thrust ring and lower thrust ring the revolute pair formed by end face bearing, another is in thrust ring
The revolute pair formed by floating bearing between the face of cylinder and ring gear (19)；The rotation of described gear (30) is driven by motor (34)
Move.
7. rocket launch platform as claimed in claim 6, it is characterised in that in described 4 kinematic pairs, be positioned at thrust ring
The revolute pair that formed by floating bearing with ring gear (30) of the face of cylinder and upper thrust ring lower surface and lower thrust ring upper surface
The revolute pair formed by end face bearing is overlapped and is equivalent to same revolute pair.
8. rocket launch platform as claimed in claim 1, it is characterised in that described seven, the 8th collection the 9th branched structure phases
With, all include ball pivot, connecting rod (25), slide block (23), gear (19), rack bar and motor (24) and kinematic pair；Wherein, ball pivot
Fastened by screw with connecting rod (25), rack bar one end by being weldingly secured on fixed platform and the most uniform, motor (24)
It is fastened by bolts in the motor slot on slide block (23)；Described kinematic pair has 5, and one is between moving platform and ball pivot
Ball secondary, a revolute pair being between connecting rod (25) with slide block (23) being slightly connected formation by axle, one is in cunning
The moving sets cooperatively formed by cylinder between block (23) and rack bar, one is in gear (19) and motor (24) output shaft
Between by the revolute pair of bonded formation, what another was between gear (19) and rack bar passes through rack and pinion engagement
The higher pair formed；The rotation of described gear (19) is driven by motor (24).
9. rocket launch platform as claimed in claim 1, it is characterised in that first, second, third described branched structure phase
With, all include upper end rocking bar, guide rail (02), support shaft (03), lower end rocking bar, lower end motor and kinematic pair；Wherein, lower end electricity
Machine is fastened by bolts in the motor slot launched on framework；Described kinematic pair has 4, and one is in support shaft (03) and upper
Connecting, by bearing, the revolute pair formed between end rocking bar, one is between upper end rocking bar and guide rail (02) by pivot pin even
Connecing the revolute pair of formation, one is between guide rail (02) and lower end rocking bar being connected, by pivot pin, the revolute pair formed, another
The individual revolute pair being between lower end rocking bar and lower end motor output shaft by bonded formation.
10. rocket launch platform as claimed in claim 9, it is characterised in that 4 described kinematic pairs are in same plane
In, wherein, the revolute pair being connected between lower end rocking bar and lower end motor output shaft is powered, by driving of lower end motor
Moving makes guide rail (02) do planar movement.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610664148.4A CN106197146B (en) | 2016-08-12 | 2016-08-12 | A kind of adjustable rocket launch platform of rocket model and posture |
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| CN201610664148.4A CN106197146B (en) | 2016-08-12 | 2016-08-12 | A kind of adjustable rocket launch platform of rocket model and posture |
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| CN106197146B CN106197146B (en) | 2017-08-11 |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107560498A (en) * | 2017-10-16 | 2018-01-09 | 北京航天发射技术研究所 | A kind of rocket body propulsion plant |
| CN108128477A (en) * | 2017-12-22 | 2018-06-08 | 航天神舟飞行器有限公司 | A kind of adjustable rocket bracket of rato formula unmanned plane launcher |
| CN109764749A (en) * | 2018-12-07 | 2019-05-17 | 湖北航天飞行器研究所 | Rocket weapon or transmitter emission system and method |
| CN111811321A (en) * | 2020-07-10 | 2020-10-23 | 北京星途探索科技有限公司 | Novel simple missile launcher |
| CN113203318A (en) * | 2021-04-25 | 2021-08-03 | 北京机械设备研究所 | Portable three-leg launcher for forest fire-extinguishing cannon |
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| CN203550783U (en) * | 2013-11-01 | 2014-04-16 | 西安天伟电子系统工程有限公司 | Portable dual-mounted missile launcher |
| CN204730750U (en) * | 2015-05-26 | 2015-10-28 | 陕西华山金属材料科技有限公司 | A kind of ground type rocket pod |
| CN105538259A (en) * | 2016-01-21 | 2016-05-04 | 北京林业大学 | Three-degree-of-freedom altitude adjustment platform |
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| CN107560498B (en) * | 2017-10-16 | 2019-08-30 | 北京航天发射技术研究所 | A kind of rocket body propulsion device |
| CN108128477A (en) * | 2017-12-22 | 2018-06-08 | 航天神舟飞行器有限公司 | A kind of adjustable rocket bracket of rato formula unmanned plane launcher |
| CN109764749A (en) * | 2018-12-07 | 2019-05-17 | 湖北航天飞行器研究所 | Rocket weapon or transmitter emission system and method |
| CN109764749B (en) * | 2018-12-07 | 2022-03-25 | 湖北航天飞行器研究所 | Method for launching a rocket weapon or launcher launching system |
| CN111811321A (en) * | 2020-07-10 | 2020-10-23 | 北京星途探索科技有限公司 | Novel simple missile launcher |
| CN113203318A (en) * | 2021-04-25 | 2021-08-03 | 北京机械设备研究所 | Portable three-leg launcher for forest fire-extinguishing cannon |
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