CN105910494A - Stable erection and rapid back-falling electrical control system of rocket erection device - Google Patents
Stable erection and rapid back-falling electrical control system of rocket erection device Download PDFInfo
- Publication number
- CN105910494A CN105910494A CN201610493149.7A CN201610493149A CN105910494A CN 105910494 A CN105910494 A CN 105910494A CN 201610493149 A CN201610493149 A CN 201610493149A CN 105910494 A CN105910494 A CN 105910494A
- Authority
- CN
- China
- Prior art keywords
- rocket
- erection
- electrical control
- oil pump
- plays
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B21/00—Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
- F15B21/08—Servomotor systems incorporating electrically operated control means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
Abstract
The invention provides a stable erection and rapid back-falling electrical control system of a rocket erection device. The electrical control system comprises the erection device, the erection device is provided with a rocket clamping mechanism, and an erection oil cylinder and a limiting switch are mounted on the lower portion of the erection device; the erection oil cylinder is connected with an oil pump motor, and the oil pump motor is controlled through an oil pump motor control cabinet; and the oil pump motor control cabinet is connected to an electrical control combination; and according to the system, the erection device can be made to clamp a rocket to carry out full-automatic erection, and the rocket can be made to safely and reliably fall on a launching pad; the whole erection time does not exceed 10 min; according to the system, the rocket clamping mechanism on the erection device can carry out rapid opening, and before the rocket is launched, the erection device can be subject to itself rapid back falling; and according to the system, in the erection and back-falling process, self-adaptation control over the erection device can be achieved, and safety and reliability are achieved.
Description
Technical field
The present invention relates to a kind of rocket play perpendicular device and stably play perpendicular and quick rewind electrical control system
System.
Background technology
Along with the development of space technology, the appearance of various new model carrier rockets, abroad occur in that
A kind of novel radiation pattern, i.e. " three flat one erect " (level assembling, horizontal checkout, water
Flat turn fortune and vertical perpendicular launch scenario) mode.Being mainly characterized by of this launch scenario:
" three hang down one remote " (vertical assemblings, vertical checkout, vertically transport and Distance Test launch party
Case) eliminate the fixing pylon on launching site on launch scenario, and with movable vertical frame generation
Replace, play perpendicular device and both played rocket supporting in horizontal transport process, play again as fire simultaneously
Arrow entirety rise perpendicular and face penetrate before quick rewind, and for realization penetrate front azimuth aiming, air-conditioning,
Fill and provide ground supports guarantee effect for demands such as distributions.This radiation pattern can be in facility letter
Single place, the survey launch mission carry out simply, changed fast and automatically.Can quickly overall rise
Perpendicular, launch, be provided simultaneously with adapting to fixing pylon launch and rely on ability that minimum facility launches and
Survival ability.
The feature of based on carrier rocket under the new situation " three flat one erect " radiation pattern understands,
After a perpendicular device band arrow is transported to launching site, need to carry out whole by a perpendicular device with rocket
Body rises perpendicular, is steadily put on transmitting station by rocket, needs to play perpendicular dress before rocket faces and penetrates simultaneously
Putting hold-fast body and carry out opening and rising the quick rewind of perpendicular device self, this technology is at present in state
There is no application precedent on interior carrier rocket, use for reference without design experiences, therefore in the urgent need to developing
A kind of novel perpendicular apparatus control system realizes rocket and steady the rising playing perpendicular device is erected and faced
Penetrate the quick rewind quickly opening and rising perpendicular device of front hold-fast body.
Summary of the invention
For solving above-mentioned technical problem, the invention provides a kind of rocket and play perpendicular device and stably rise perpendicular
And quick rewind electric control system, this rocket rise perpendicular device stably rise perpendicular and quickly rewind electric
Control system is passed through
The present invention is achieved by the following technical programs.
A kind of rocket that the present invention provides plays perpendicular device and stably plays perpendicular and quickly rewind electrical control
System, including playing perpendicular device；Rise, on perpendicular device, rocket hold-fast body is installed, play perpendicular device
Bottom is provided with Erecting oil cylinder and limit switch, and Erecting oil cylinder is connected with Oil pump electrical machinery, oil pump electricity
Machine is controlled by Oil pump electrical machinery switch board, and Oil pump electrical machinery switch board is connected to electrical control combination.
Between described Erecting oil cylinder and Oil pump electrical machinery, proportioning valve is installed.
Pressure transmitter it is additionally provided with also on pipeline between described Erecting oil cylinder and Oil pump electrical machinery
Access electrical control is combined.
The junction of described perpendicular device is additionally provided with angular transducer and accesses electrical control group
Close.
Described angular transducer accesses in electrical control combination, gathers rising in electrical control combination
The support angle parameter of perpendicular device.
Described pressure transmitter accesses in electrical control combination, and the pressure gathered in Erecting oil cylinder does
Pressure parameter for electrical control combination.
The beneficial effects of the present invention is: the present invention can make perpendicular device hold rocket tightly to carry out entirely
Automatically rising perpendicular and can make rocket land safely and reliably on transmitting station, whole perpendicular time does not surpasses
Cross 10min.The present invention can make rocket hold-fast body on perpendicular device quickly open energy of the present invention
Perpendicular device has enough been made to play the quick rewind of perpendicular device self before rocket faces and penetrates.The present invention can make
Play perpendicular device and realize Self Adaptive Control during playing perpendicular and rewind, reach safe and reliable.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the control principle drawing of the present invention；
Fig. 3 is control software composition diagram of the present invention；
In figure: 1-plays perpendicular device, 2-rocket hold-fast body, 3-angular transducer, and 4-plays perpendicular oil
Cylinder, 5-proportioning valve, 6-Oil pump electrical machinery, 7-Oil pump electrical machinery switch board, 8-electrical control combination,
9-pressure transmitter, 10-limit switch.
Detailed description of the invention
Technical scheme is described further below, but claimed scope is not limited to
In described.
A kind of rocket plays perpendicular device and stably plays perpendicular and quick rewind electric control system, perpendicular including rising
Device 1；Rising and be provided with rocket hold-fast body 2 on perpendicular device 1, the bottom playing perpendicular device 1 is provided with
Erecting oil cylinder 4 and limit switch 10, Erecting oil cylinder 4 is connected with Oil pump electrical machinery 6, Oil pump electrical machinery 6
Being controlled by Oil pump electrical machinery switch board 7, Oil pump electrical machinery switch board 7 is connected to electrical control combination 8.
Between described Erecting oil cylinder 4 and Oil pump electrical machinery 6, proportioning valve 5 is installed.
It is additionally provided with pressure transmitter on pipeline between described Erecting oil cylinder 4 and Oil pump electrical machinery 6
9 and access electrical control combination 8.
The junction of described perpendicular device 1 is additionally provided with angular transducer 3 and accesses electrical control
Combination 8.
Described angular transducer 3 accesses in electrical control combination 8, gathers in electrical control combination 8
Rise perpendicular device 1 support angle parameter.
Described pressure transmitter 9 accesses in electrical control combination 8, gathers the pressure in Erecting oil cylinder 4
Power is as the pressure parameter of electrical control combination 8.
The control flow of the present invention is, is playing the angular transducer 3 being provided with on perpendicular device 11,
In real time the angle value playing perpendicular device 1 is fed back to electrical control combination 8, electrical control combination 8
In control software receipt to after angle value, after algorithm process, according to playing a perpendicular device
The practical situation of 1, is converted into electricity electrichydraulic control proportioning valve 5 control signal, and output controls electro-hydraulic
Control proportioning valve 5 action, it is achieved play stablize to erect and face and penetrating front rocket and hold machine tightly of perpendicular device 1
The quick rewind quickly opening and rising perpendicular device 1 of structure 2, by pressure transmitter 9 force value
The stress of monitoring left and right Erecting oil cylinder 4, limit switch 10 has limited the limit of perpendicular device
Position wherein provides the power source of perpendicular device 1 action from Oil pump electrical machinery 6, control oil pump electricity
Machine 6 starts and stops and State Transferring is Oil pump electrical machinery switch board 7, has promoted 1, perpendicular device
Perpendicular and rewind is Erecting oil cylinder 4.By the button on operation electrical control assembled panel
Realize carrier rocket stably rise perpendicular and play the quick rewind of perpendicular device, it is possible to controlled by far-end
System, and whole control process data is stored, transfer data to far-end simultaneously.From
And realized automatically controlling of perpendicular device 1.
The operating process of the present invention is, when rise perpendicular device and rocket need to carry out vertical erect time,
It is necessary to ensure that perpendicular device has connected with upset docking facilities, has then started electrical control group
Close 8, connect Oil pump electrical machinery switch board 7380V power supply, and be placed on remote control state, press
" Oil pump electrical machinery opens/stops " button on 8 guidance panels is combined in electrical control, treats Oil pump electrical machinery 6
After starting well, press " rising perpendicular " button that electrical control is combined on 8 guidance panels, control soft
Part controls electrichydraulic control proportioning valve 5 action, under the effect of hydraulic control system, Erecting oil cylinder
4 stretch out, and have promoted 1, perpendicular device to erect.Rise during erecting, control software collection pressure inverting
The force value of left and right Erecting oil cylinder is monitored by the force value of device 9, receiving angle sensor 3
Angle value carried out perpendicular device and played the conversion of perpendicular rate controlling amount, and be converted into electrichydraulic control ratio
The opening controlled quentity controlled variable of example valve 5, it is achieved whole perpendicular process is the most reliable.
Rise after perpendicular device plays perpendicular putting in place, unclamp rocket hold-fast body 2, allow the steady land of rocket exist
On transmitting station.Before rocket faces and penetrates, it is first turned on rocket hold-fast body 2, connects Oil pump electrical machinery
Switch board 380V power supply, and it is placed on remote control state, then open electrical control combination 8,
And it being placed on remote control state, instruction of falling after being sent by far-end has realized before perpendicular device faces and penetrate
Quickly rewind.During rewind, control the force value of software collection pressure transmitter 9 to left and right
The force value of Erecting oil cylinder is monitored, and the angle value of receiving angle sensor 3 has carried out perpendicular dress
Put the conversion of perpendicular rate controlling amount, and be converted into the opening controlled quentity controlled variable of electrichydraulic control proportioning valve 5.
Claims (6)
1. rocket plays perpendicular device and stably plays a perpendicular and quick rewind electric control system, including
Play perpendicular device (1), it is characterised in that: rise, on perpendicular device (1), rocket hold-fast body is installed
(2), the bottom playing perpendicular device (1) is provided with Erecting oil cylinder (4) and limit switch (10),
Erecting oil cylinder (4) is connected with Oil pump electrical machinery (6), and Oil pump electrical machinery (6) passes through Oil pump electrical machinery
Switch board (7) controls, and Oil pump electrical machinery switch board (7) is connected to electrical control combination (8).
2. rocket as claimed in claim 1 plays perpendicular device and stably plays perpendicular and quick rewind electric-controlled
System processed, it is characterised in that: install between described Erecting oil cylinder (4) and Oil pump electrical machinery (6)
Proportional valve (5).
3. rocket as claimed in claim 1 plays perpendicular device and stably plays perpendicular and quick rewind electric-controlled
System processed, it is characterised in that: between described Erecting oil cylinder (4) and Oil pump electrical machinery (6)
It is additionally provided with pressure transmitter (9) on pipeline and accesses electrical control combination (8).
4. rocket as claimed in claim 1 plays perpendicular device and stably plays perpendicular and quick rewind electric-controlled
System processed, it is characterised in that: the junction of described perpendicular device (1) is additionally provided with angle and passes
Sensor (3) also accesses electrical control combination (8).
5. rocket as claimed in claim 1 plays perpendicular device and stably plays perpendicular and quick rewind electric-controlled
System processed, it is characterised in that: described angular transducer (3) accesses electrical control combination (8)
In, gather the support angle parameter playing perpendicular device (1) in electrical control combination (8).
6. rocket as claimed in claim 1 plays perpendicular device and stably plays perpendicular and quick rewind electric-controlled
System processed, it is characterised in that: described pressure transmitter (9) accesses electrical control combination (8)
In, gather the pressure parameter as electrical control combination (8) of the pressure in Erecting oil cylinder (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610493149.7A CN105910494A (en) | 2016-06-29 | 2016-06-29 | Stable erection and rapid back-falling electrical control system of rocket erection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610493149.7A CN105910494A (en) | 2016-06-29 | 2016-06-29 | Stable erection and rapid back-falling electrical control system of rocket erection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105910494A true CN105910494A (en) | 2016-08-31 |
Family
ID=56759940
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610493149.7A Pending CN105910494A (en) | 2016-06-29 | 2016-06-29 | Stable erection and rapid back-falling electrical control system of rocket erection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105910494A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107524660A (en) * | 2017-08-21 | 2017-12-29 | 北京航天发射技术研究所 | A kind of large-sized structural parts play the control method and control system of perpendicular straightening |
| CN107816913A (en) * | 2017-09-22 | 2018-03-20 | 北京机械设备研究所 | One kind quickly plays perpendicular method |
| CN110262214A (en) * | 2019-07-22 | 2019-09-20 | 北京航天发射技术研究所 | Play perpendicular control system |
| CN110966890A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Bundled rocket withdrawing method |
| CN111023898A (en) * | 2019-12-30 | 2020-04-17 | 湖北航天技术研究院总体设计所 | Limit protection control system and method of missile erecting equipment |
| CN112061980A (en) * | 2018-03-28 | 2020-12-11 | 蓝箭航天技术有限公司 | Erecting device and crane for rocket erecting |
| CN114261924A (en) * | 2021-11-24 | 2022-04-01 | 蓝箭航天空间科技股份有限公司 | Device for installing erecting oil cylinder and rocket erecting system |
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| US5191162A (en) * | 1991-09-05 | 1993-03-02 | Newport News Shipbuilding And Dry Dock Company | Method and apparatus for a ship-based rocket launching structure |
| WO2010113171A1 (en) * | 2009-03-30 | 2010-10-07 | Director General, Defence Research & Development Organisation | A mobile missile launch system and method thereof |
| CN102269191A (en) * | 2011-07-08 | 2011-12-07 | 北京机械设备研究所 | Dynamic compensation control method based on multi-stage oil cylinder erecting system |
| CN103090749A (en) * | 2011-11-01 | 2013-05-08 | 北京航天发射技术研究所 | Connecting device and connecting method used for disconnecting or connecting launcher with erecting hydraulic cylinder |
| CN105277049A (en) * | 2015-10-27 | 2016-01-27 | 贵州航天天马机电科技有限公司 | Perpendicular positioning device for carrier rocket and use method of perpendicular positioning device |
| CN205138343U (en) * | 2015-11-27 | 2016-04-06 | 贵州航天天马机电科技有限公司 | Play to erect hydraulic control system that diversion is stabilized to frame |
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2016
- 2016-06-29 CN CN201610493149.7A patent/CN105910494A/en active Pending
Patent Citations (6)
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| US5191162A (en) * | 1991-09-05 | 1993-03-02 | Newport News Shipbuilding And Dry Dock Company | Method and apparatus for a ship-based rocket launching structure |
| WO2010113171A1 (en) * | 2009-03-30 | 2010-10-07 | Director General, Defence Research & Development Organisation | A mobile missile launch system and method thereof |
| CN102269191A (en) * | 2011-07-08 | 2011-12-07 | 北京机械设备研究所 | Dynamic compensation control method based on multi-stage oil cylinder erecting system |
| CN103090749A (en) * | 2011-11-01 | 2013-05-08 | 北京航天发射技术研究所 | Connecting device and connecting method used for disconnecting or connecting launcher with erecting hydraulic cylinder |
| CN105277049A (en) * | 2015-10-27 | 2016-01-27 | 贵州航天天马机电科技有限公司 | Perpendicular positioning device for carrier rocket and use method of perpendicular positioning device |
| CN205138343U (en) * | 2015-11-27 | 2016-04-06 | 贵州航天天马机电科技有限公司 | Play to erect hydraulic control system that diversion is stabilized to frame |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107524660A (en) * | 2017-08-21 | 2017-12-29 | 北京航天发射技术研究所 | A kind of large-sized structural parts play the control method and control system of perpendicular straightening |
| CN107524660B (en) * | 2017-08-21 | 2019-08-30 | 北京航天发射技术研究所 | A kind of large-sized structural parts play the control method and control system of perpendicular straightening |
| CN107816913A (en) * | 2017-09-22 | 2018-03-20 | 北京机械设备研究所 | One kind quickly plays perpendicular method |
| CN107816913B (en) * | 2017-09-22 | 2019-11-08 | 北京机械设备研究所 | One kind quickly playing perpendicular method |
| CN112061980A (en) * | 2018-03-28 | 2020-12-11 | 蓝箭航天技术有限公司 | Erecting device and crane for rocket erecting |
| CN110966890A (en) * | 2018-12-20 | 2020-04-07 | 中国人民解放军63921部队 | Bundled rocket withdrawing method |
| CN110966890B (en) * | 2018-12-20 | 2022-04-05 | 中国人民解放军63921部队 | Bundled rocket withdrawing method |
| CN110262214A (en) * | 2019-07-22 | 2019-09-20 | 北京航天发射技术研究所 | Play perpendicular control system |
| CN110262214B (en) * | 2019-07-22 | 2022-08-05 | 北京航天发射技术研究所 | Erecting control system |
| CN111023898A (en) * | 2019-12-30 | 2020-04-17 | 湖北航天技术研究院总体设计所 | Limit protection control system and method of missile erecting equipment |
| CN114261924A (en) * | 2021-11-24 | 2022-04-01 | 蓝箭航天空间科技股份有限公司 | Device for installing erecting oil cylinder and rocket erecting system |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160831 |