CN106428655B - A kind of carrier rocket plays vertical frame and adaptively pushes away dress system - Google Patents
A kind of carrier rocket plays vertical frame and adaptively pushes away dress system Download PDFInfo
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- CN106428655B CN106428655B CN201510496618.6A CN201510496618A CN106428655B CN 106428655 B CN106428655 B CN 106428655B CN 201510496618 A CN201510496618 A CN 201510496618A CN 106428655 B CN106428655 B CN 106428655B
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Abstract
Vertical frame, which is played, the invention discloses a kind of carrier rocket adaptively pushes away dress system, including overturning docking facilities and transport vehicle, transport vehicle has been equipped with vertical frame, it plays vertical frame two sides and is separately installed with several lateral micro-adjusting mechanisms, transport vehicle top surface is equipped with several universal turning mechanisms, universal turning mechanism offsets with vertical frame bottom face is played, it rises to be connected in vertical frame and pushes away dress support, it pushes away dress support to be hinged with the output end for pushing away charge of oil cylinder, pushes away charge of oil cylinder end and be hinged on the tailstock front end for being fixed on top of transport vehicle by hinged seat A；It overturns and is equipped with positioning guide rail at the top of docking facilities, it plays vertical frame front bottom end and is connected with and match with positioning guide rail bottom end and in inverted universal turning mechanism, it plays vertical frame front end and is connected with positioning support, positioning guide rail left end is connected with the positioning pin to match with positioning support, is equipped with position-sensing switch by positioning pin.The present invention effectively reduces pushing away for carrier rocket and dresses up this and improve accuracy and efficiency.
Description
Technical field
The present invention relates to Launch Vehicle Ground supports guarantee technical fields, and in particular to a kind of carrier rocket vertical frame
Adaptively push away dress system.
Background technique
With the development of space technology, require emitter region site facility simple under the new situation, emission system has certain
Survival ability can be realized rapid fire.Traditional emission system is generally fixed launching tower, and fixed launching tower
The disadvantage that the infrastructure period is long, maintenance cost is costly gradually reveals.For this problem, current foreign countries occur one
The novel radiation pattern of kind, i.e. " three flat one is perpendicular " (perpendicular launch scenario is transported and vertically risen to horizontal assembling, horizontal checkout, level) are square
Formula.This launch scenario is mainly characterized by: in " three flat one erect " (vertical assembling, vertical checkout, vertical transhipment and remote survey
Examination launch scenario) fixation pylon on launching site is eliminated on launch scenario, and replaced with movable vertical frame, vertical frame was both
Play bearing of the rocket in horizontal transport process, at the same play again as rocket integrally rise it is perpendicular and face penetrate before play a vertical frame and rewind, and
For realize penetrate preceding azimuth aiming, air-conditioning, filling and for the demands such as distribution provide ground supports guarantee act on.The radiation pattern
Survey launch mission that is simple, fast and automatically changing can be carried out in the simple place of facility.Perpendicular, transmitting quickly can be integrally played, together
When have the ability and survival ability for adapting to fixed pylon transmitting and relying on minimum facility transmitting.
The characteristics of " three flat one perpendicular " radiation pattern based on carrier rocket under the new situation, playing a vertical frame band arrow it is found that be transported to
After launching site, an important link before erecting at vertical has been exactly that vertical frame load arrow is docked with the fixed overturning on launching site
Device carries out horizontal docking, and due to different launching sites the case where is different, after it will overturn docking facilities fixation, if the ground at launching site
Face is uneven, will lead to and pushes away dress failure, this is because carrier rocket is transported by transport vehicle, and site factors will lead to transport vehicle cannot
Keep horizontality, i.e. carrier rocket can not accurately be docked with overturning docking facilities, need to expend a large amount of manpower be the time into
Row adjustment.And at present there is no relevant technology, no design experiences are used for reference, therefore there is an urgent need to develop a kind of novel docking system
To have solved the problems, such as that vertical frame is docked with overturning the horizontal of docking facilities.
Summary of the invention
The present invention is intended to provide a kind of carrier rocket, which plays vertical frame, adaptively pushes away dress system, to solve conventional fixed-type launching tower
The infrastructure period of frame is long, maintenance cost is costly and transmitter site causes carrier rocket can not be with overturning docking facilities essence
Really the problem of docking.
The present invention is achieved by following technical solution:
A kind of carrier rocket plays vertical frame and adaptively pushes away dress system, including overturning docking facilities and transport vehicle, the transport vehicle
It has been equipped with vertical frame, vertical frame two sides has been played and is separately installed with several lateral micro-adjusting mechanisms, transport vehicle top surface is equipped with several universal times
Rotation mechanism, universal turning mechanism offset with vertical frame bottom face is played, and play to be connected with pushing away dress support in vertical frame, push away dress support and push away charge of oil
The output end of cylinder is hinged, and pushes away charge of oil cylinder end and is hinged on the tailstock front end for being fixed on top of transport vehicle by hinged seat A；It is described
It overturns and is equipped with positioning guide rail at the top of docking facilities, described vertical frame front bottom end, which is connected with, to match with positioning guide rail bottom end and be in
Inverted universal turning mechanism plays vertical frame front end and is connected with positioning support, and the positioning guide rail left end is connected with and positioning support
The positioning pin to match is equipped with position-sensing switch by positioning pin.
The lateral micro-adjusting mechanism includes slide, and sliding axle is slidably fitted in slide, and sliding axle front end is pacified by bearing
Equipped with the pin shaft arranged vertically, pin shaft outer wall is socketed with limited roller, and limited roller outer wall is socketed with rubber wheel, and pin shaft top is logical
Retainer ring spacing is crossed, rubber wheel end offsets with vertical frame two sides outer wall is played, and sliding axle right end is connected with hinged seat B, passes through hinged seat B
It is hinged with the output end of a fine tuning oil cylinder.
The universal turning mechanism includes shell, and bottom is equipped with pedestal in shell, and pedestal top end face is provided with hemispheric
Slot, is uniformly laid with one layer of secondary ball in slot, is equipped with main ball by pressing plate on secondary ball.
Described push away is equipped with auxiliary support bar between charge of oil cylinder and transport vehicle.
The transport vehicle two sides are mounted on hydraulic leg.
The positioning guide rail front end is tubaeform.
The beneficial effects of the present invention are:
Compared with prior art, carrier rocket provided by the invention plays vertical frame and adaptively pushes away dress system, by pushing away charge of oil cylinder
It has realized that the level of vertical frame pushes away dress, then lateral fine tuning has been realized by the lateral micro-adjusting mechanism of two sides, and realize by hydraulic leg
Vertical frame vertical adjusting is played, three axis for finally having realized vertical frame are adjusted, and can carry out carrier rocket at the launching site of varying environment
It quickly pushes away dress and transmitting prepares, be adjusted without expending a large amount of manpower and time and push away dress, compared to traditional fixed hair
Assembling device is penetrated and pushes away, the present invention effectively reduces cost and improves accuracy, trueness error≤1mm, and time-consuming short, when pushing away dress
Between be less than 15min.
Detailed description of the invention
Fig. 1 is main view of the invention；
Fig. 2 is the top view of Fig. 1；
Fig. 3 is the structure chart of the invention pushed away after the completion of dress；
Fig. 4 is the enlarged drawing of dotted portion I in Fig. 3；
Fig. 5 is the structure chart of lateral micro-adjusting mechanism in the present invention；
Fig. 6 is lateral micro-adjusting mechanism operation schematic diagram in the present invention；
Fig. 7 is the structure chart of universal turning mechanism in the present invention；
Fig. 8 is to push away to reinstall road hydraulic schematic diagram in the present invention；
Fig. 9 is that the present invention plays vertical frame band arrow state diagram；
In figure: 1- overturning docking facilities, 2- transport vehicle, 3- vertical frames, 4- universal turning mechanism, 5- hydraulic leg, 6- are pushed away
Support is filled, 7- pushes away charge of oil cylinder, 8- auxiliary support bar, 9- hinged seat A, 10- positioning pin, 11- positioning seat, 12- tailstock, 13- wheel,
The side 14- is to micro-adjusting mechanism, 15- positioning guide rail, 16- position-sensing switch, 17- limited roller, 18- rubber wheel, 19- pin shaft, 20- axis
It holds, 21- retaining ring, 22- sliding axle, 23- finely tunes oil cylinder, 24- hinged seat B, 25- slide, the main ball of 26-, 27- shell, the rolling of 28- pair
Pearl, 29- pedestal, 30- carrier rocket.
Specific embodiment
Technical solution of the present invention is described further with reference to the accompanying drawings and embodiments, but required protection scope
It is not limited to described；
As shown in Figs. 1-2, carrier rocket provided by the invention plays vertical frame and adaptively pushes away dress system, including overturning docking facilities
1 and transport vehicle 2, the transport vehicle 2 be equipped with vertical frame 3, rise 3 two sides of vertical frame be separately installed with several lateral micro-adjusting mechanisms 14,
2 top surface of transport vehicle is equipped with several universal turning mechanisms 4, and universal turning mechanism 4 offsets with 3 bottom face of vertical frame is played, and rises in vertical frame 3
It is connected with and pushes away dress support 5, push away dress support 6 and be hinged with the output end for pushing away charge of oil cylinder 7, push away 7 end of charge of oil cylinder and pass through hinged seat A9
It is hinged on 12 front end of tailstock for being fixed on 2 top of transport vehicle；Positioning guide rail 15 is equipped at the top of the overturning docking facilities 1, it is described
It plays 3 front bottom end of vertical frame and is connected with and match with 15 bottom end of positioning guide rail and be in inverted universal turning mechanism 4, before playing vertical frame 3
End is connected with positioning support 11, and 15 left end of positioning guide rail is connected with the positioning pin 10 to match with positioning support 11, positioning
Position-sensing switch 16 is installed by pin 10.
As seen in figs. 5-6, the lateral micro-adjusting mechanism 14 includes slide 25, is slidably fitted with sliding axle 22 in slide 25,
22 front end of sliding axle is equipped with the pin shaft 19 arranged vertically by bearing 20, and 19 outer wall of pin shaft is socketed with limited roller 17, limit
17 outer wall of idler wheel is socketed with rubber wheel 18, and 19 top of pin shaft is limited by retaining ring 21, outside 18 end of rubber wheel and 3 two sides of vertical frame
Wall offsets, and 22 right end of sliding axle is connected with hinged seat B24, is hinged by hinged seat B24 and the output end of a fine tuning oil cylinder 23.
The lateral fine tuning to vertical frame 3 is played is realized by lateral micro-adjusting mechanism 14.
As shown in fig. 7, the universal turning mechanism 4 includes shell 27, bottom is equipped with pedestal 29, pedestal 29 in shell 27
Top end face is provided with hemispheric slot, is uniformly laid with one layer of secondary ball 28 in slot, is equipped with main ball by pressing plate on secondary ball 28
26。
In order to improve the stability for pushing away charge of oil cylinder 7, avoid the occurrence of offset or fall, it is described push away charge of oil cylinder 7 and transport vehicle 2 it
Between auxiliary support bar 8 is installed.
In order to guarantee to push away the stability of dress process, 2 liang of the transport vehicle while having realized the adjustment of 3 vertical height of vertical frame
Side is mounted on hydraulic leg 5.
For the ease of playing the insertion of 3 front end of vertical frame, 15 front end of positioning guide rail is tubaeform.
Embodiment:
As shown in figure 9, transport vehicle 2 is self-propelled whole rocket transport vehicle, realizes and carries arrow, bracket navigator fix and fixed high leveling,
2 tail portion of transport vehicle is required to be lower than headstock when leveling, anterior-posterior horizontal precision is not more than 20 points, after leveling, passes through lateral micro-adjusting mechanism
14 pairs are played vertical frame 3 and carry out lateral Displacement, under the impetus for pushing away charge of oil cylinder 7, are realized through hydraulic control system as shown in Figure 8
Vertical frame 3 is played on overturning docking facilities 1 by coarse positioning to fine positioning process, braking, has finally realized after the completion of pushing away dress
Purpose of the vertical frame 3 to the flat-pushing dress docking of overturning 1 automatic water of docking facilities.
Detailed process are as follows: when needing to push away dress docking to a 3 carry out level of vertical frame, transport vehicle 2 is made to have delivered vertical frame 3 first
Navigator fix is carried out on the position of overturning docking facilities 1, when vehicle navigation and positioning accuracy is met the requirements, transport can be started
The hydraulic leg 5 of vehicle 2 makes vehicle carry out fixed high leveling.Guarantee that 3 bottom surface of vertical frame is higher than on overturning docking facilities 1 when leveling
Plane a certain distance, distance are 5-10mm, and hydraulic leg 5 or so levels precision after transport vehicle 2 and front and back hydraulic leg 5 is adjusted
Flat precision reaches certain precision (headstock is higher than tailstock 8-12mm).Make to push away charge of oil cylinder 7 later and connect with dress support 6 is pushed away, when connection
Click step progress: push away charge of oil cylinder 7 by hinged seat A9 rotate upwards 10-30 ° → push away 7 piston rod of charge of oil cylinder stretch out 10-
25cm → pushing away the piston rod on charge of oil cylinder 7 to drop in the card slot for pushing away dress support 6 → is finally limited with pressing plate and is fixed.Push away charge of oil cylinder
7 start to have carried out vertical frame 3 and push away to fill to limit work with pushing away after the completion of dress support 6 connect, when limit makes micro-adjusting mechanism 14 before transport vehicle 2
18 end face of rubber wheel with rise 3 side clearance of vertical frame meet the requirements after stopping act, rise a vertical frame 3 push away dress limit movement complete.
Rise vertical frame 3 push away dress docking preparation after the completion of, the flat-pushing dress work of 3 automatic water of vertical frame can have been carried out, level pushes away
Start when dress and push away dress hydraulic control system automatically on transport vehicle 2, hydraulic control system control pushes away the development of charge of oil cylinder 7, and to push away dress dynamic
Make, under the action of pushing away charge of oil cylinder 7, has realized vertical frame 3 in several universal turning mechanisms 4 on transport vehicle 2 slowly to solid
Overturning docking facilities 1 on position are scheduled on to slide, due to 15 front end of positioning guide rail on overturning docking facilities 1 be it is tubaeform, rise
It is coarse positioning when vertical frame 3 initially enters, it is accurate fixed then to start under the effect of the positioning pin 10 of 15 middle section of positioning guide rail and tail end
The inversion universal turning mechanism of 3 front bottom end of vertical frame is played when playing vertical frame 3 and will slide on overturning docking facilities 1 in position
4 are rolled in the groove of overturning docking facilities 1, play 3 bottom surface of vertical frame and are bonded with plane on overturning docking facilities 1, fill with pushing away
Progress, the positioning support 11 for playing 3 front end of vertical frame gradually draws close with positioning pin 10, and final positioning pin 10 is inserted into positioning support 11
Interior, as shown in Figure 3-4, the position-sensing switch 16 for being mounted on overturning 1 tail portion of docking facilities at this time has sensed that vertical frame 3 pushes away and has been attached to position letter
Number, program stopped pushes away the movement of charge of oil cylinder 7, to reach mesh of the vertical frame 3 to the flat-pushing dress docking of overturning 1 automatic water of docking facilities
's.
Above-described embodiment is only a preferred embodiment of the invention, is not intended to limit the scope of protection of the present invention, all
Made deformation, modification or equivalent replacement etc., should all fall into protection model of the invention on the basis of technical solution of the present invention
It encloses.
Claims (6)
1. a kind of carrier rocket plays vertical frame and adaptively pushes away dress system, including overturning docking facilities (1) and transport vehicle (2), feature
Be: the transport vehicle (2) has been equipped with vertical frame (3), plays vertical frame (3) two sides and is separately installed with several lateral micro-adjusting mechanisms
(14), transport vehicle (2) top surface is equipped with several universal turning mechanisms (4), universal turning mechanism (4) and vertical frame (3) bottom face
It offsets, plays to be connected with pushing away dress support (5) on vertical frame (3), push away dress support (6) and be hinged with the output end for pushing away charge of oil cylinder (7), push away dress
Oil cylinder (7) end is hinged on tailstock (12) front end being fixed at the top of transport vehicle (2) by hinged seat A (9)；The overturning docking
Positioning guide rail (15) are equipped at the top of device (1), described vertical frame (3) front bottom end is connected with and positioning guide rail (15) bottom end phase
Match and be in inverted universal turning mechanism (4), plays vertical frame (3) front end and be connected with positioning support (11), the positioning guide rail (15)
Left end is connected with the positioning pin (10) to match with positioning support (11), is equipped with position-sensing switch (16) by positioning pin (10).
2. carrier rocket according to claim 1 plays vertical frame and adaptively pushes away dress system, it is characterised in that: the lateral fine tuning
Mechanism (14) includes slide (25), is slidably fitted with sliding axle (22) in slide (25), sliding axle (22) front end passes through bearing
(20) pin shaft (19) arranged vertically is installed, pin shaft (19) outer wall is socketed with limited roller (17), limited roller (17) outer wall
It is socketed with rubber wheel (18), pin shaft (19) top is limited by retaining ring (21), outside rubber wheel (18) end and vertical frame (3) two sides
Wall offsets, and sliding axle (22) right end is connected with hinged seat B (24), passes through the output of hinged seat B (24) and fine tuning oil cylinder (23)
End is hinged.
3. carrier rocket according to claim 1 plays vertical frame and adaptively pushes away dress system, it is characterised in that: the universal turning
Mechanism (4) includes shell (27), and shell (27) interior bottom is equipped with pedestal (29), and pedestal (29) top end face is provided with hemispheric
Slot, is uniformly laid with one layer of secondary ball (28) in slot, is equipped with main ball (26) by pressing plate on secondary ball (28).
4. carrier rocket according to claim 1 plays vertical frame and adaptively pushes away dress system, it is characterised in that: described to push away charge of oil cylinder
(7) it is equipped between transport vehicle (2) auxiliary support bar (8).
5. carrier rocket according to claim 1 plays vertical frame and adaptively pushes away dress system, it is characterised in that: the transport vehicle
(2) two sides are mounted on hydraulic leg (5).
6. carrier rocket according to claim 1 plays vertical frame and adaptively pushes away dress system, it is characterised in that: the positioning guide rail
(15) front end is tubaeform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510496618.6A CN106428655B (en) | 2015-08-13 | 2015-08-13 | A kind of carrier rocket plays vertical frame and adaptively pushes away dress system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510496618.6A CN106428655B (en) | 2015-08-13 | 2015-08-13 | A kind of carrier rocket plays vertical frame and adaptively pushes away dress system |
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| Publication Number | Publication Date |
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| CN106428655A CN106428655A (en) | 2017-02-22 |
| CN106428655B true CN106428655B (en) | 2019-02-12 |
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| CN112902747A (en) * | 2021-03-03 | 2021-06-04 | 北京航天发射技术研究所 | Whole arrow transferring and erecting system and method |
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