CN206450138U - Lift-off device emission system - Google Patents
Lift-off device emission system Download PDFInfo
- Publication number
- CN206450138U CN206450138U CN201720118105.6U CN201720118105U CN206450138U CN 206450138 U CN206450138 U CN 206450138U CN 201720118105 U CN201720118105 U CN 201720118105U CN 206450138 U CN206450138 U CN 206450138U
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- China
- Prior art keywords
- rocket
- carrier loader
- linear motor
- accelerated
- lift
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Abstract
The utility model provides a kind of lift-off device emission system, belongs to assist device field, including horizontal rail, arc track and the vertical rail being sequentially connected；Rocket is arranged on carrier loader, and carrier loader is travelled on horizontal rail, arc track and vertical rail；Rocket launching can be made to obtain initial velocity using ground resource, it is possible to reduce the consumption of its own energy, it is possible to reduce rocket sprays the pollution to ground environment.
Description
Technical field
The utility model provides a kind of lift-off device emission system, belongs to assist device field.
Background technology
At present, the transmitting of rocket is generally ground launch, fixes rocket vertically using the launcher of rocket, then sends out again
When penetrating, launcher unclamps, rocket firing, and the boost motor of rocket sprays substantial amounts of flame, rocket is taken off, and accelerates, directly
To centrifugal force is broken through, into space, but the amount that rocket accommodates fuel is limited, when taking off, due to needing boosting weight pole
Big rocket overcomes centrifugal force to accelerate, so a considerable amount of fuel can be expended, makes rocket after entering in space, supply is carried
It is limited for the fuel of power, meanwhile, the energy in ground launch, substantial amounts of incendiary rocket can pollute atmospheric environment.
Utility model content
The utility model purpose is to provide a kind of lift-off device emission system, rocket launching can be made to be obtained using ground resource
Take initial velocity, it is possible to reduce the consumption of its own energy, it is possible to reduce rocket sprays the pollution to ground environment.
Lift-off device emission system described in the utility model, including be sequentially connected horizontal rail, arc track and vertical
Track；Rocket is arranged on carrier loader, and carrier loader is travelled on horizontal rail, arc track and vertical rail；
Horizontal rail is provided with the steam ejection mechanism accelerated for carrier loader；The linking of steam ejection mechanism end has straight line
Motor acceleration mechanism A；
Arc track is provided with linear motor accelerated mechanism B, linear motor accelerated mechanism B and motor acceleration mechanism A head and the tail
Linking；
Vertical rail is provided with linear motor accelerated mechanism C, linear motor accelerated mechanism C and linear motor accelerated mechanism B
Deceleration device is additionally provided with tandem array, vertical rail, is connected in linear motor accelerated mechanism C-terminal.
Install and be mounted on suspension magnet at acceleration mechanism A and acceleration mechanism B.
Described lift-off device emission system, horizontal rail, arc track and vertical rail are provided with track, linear motor accelerated
Mechanism A, linear motor accelerated mechanism B and linear motor accelerated mechanism C electromagnet and suspension magnet install in orbit, fortune
Carry and longitudinally defined wheel is provided with the mobile devices that dolly bottom is provided with open loop, open loop mobile devices and wheel 26 is laterally defined by open loop
Mobile devices limit in orbit；
Open loop mobile devices provided with steam ejection mechanism dragging link up with, and with linear electric motors coordinate mover and with
The suspension rack that suspension magnet coordinates；
Bracket provided with support rocket bottom at the top of carrier loader, and support the support of rocket body, and fixed rocket
Fixing groove.
Provided with locking electromagnet in described lift-off device emission system, fixing groove, rocket is provided with " L " type eye-splice, " L " type
Eye-splice one end coordinates provided with locking iron plate, " L " type eye-splice insertion fixing groove with the locking electromagnet of fixing groove.
Described lift-off device emission system, bracket is annular, and bracket holds rocket bottom, and passes through the boost motor of rocket
Bracket.
The utility model has the beneficial effect that compared with prior art：
Described lift-off device emission system, will first by that can provide the steam ejection mechanism of the huge power of pullling with moment
The carrier loader that carry rocket starts, and it is obtained certain initial velocity, and the carrier loader for then carrying rocket can be hanged
Floating magnet suspends, and is that linear electric motors drive acceleration by linear accelerating mechanism A, maglev carrier loader can rapidly be added
Speed, then, then reaches after arc track, can make the gradually deflecting of rocket and carrier loader, until vertical, during which linear accelerating
Mechanism B, continues as carrier loader acceleration, and suspension magnet persistently overcomes the centrifugal force that carrier loader is produced on arc track,
After reaching on vertical rail, rocket firing departs from carrier loader, and at this moment rocket has higher initial velocity, can save big
Amount, which is taken off, obtains the energy of initial velocity, can greatly reduce the consumption of self-energy when it takes off.Meanwhile, use steam on ground
Carrier loader and its rocket of delivery can be accelerated with electric energy, it is to avoid the pollution to environment, while electromechanical in straight-line electric
When magnetic accelerates, magnetic suspension is carried out to carrier loader, carrier loader can be made to break away from frictional force and accelerated faster.
Brief description of the drawings
Fig. 1 is the utility model structural representation；
Fig. 2 is carrier loader structural representation；
Fig. 3 is open loop mobile devices structural representation；
Fig. 4 is fixed slot configurations schematic diagram.
In figure：1st, carrier loader；2nd, rocket；3rd, horizontal rail；4th, linear motor accelerated mechanism A；5th, it is linear motor accelerated
Mechanism B；6th, deceleration device；7th, deceleration linear electric motors；8th, vertical rail；9th, linear motor accelerated mechanism C；10th, arc track；
11st, " L " type eye-splice；12nd, fixing groove；13rd, bracket；14th, support；15th, iron plate is locked；16th, electromagnet is locked；17th, open loop is travelled
Device；18th, longitudinally defined wheel；19th, hook is pulled；20th, mover；21st, stator；22nd, rail groove；23rd, " work " type rail；24th, suspend
Magnet；25th, suspension rack；26th, wheel is laterally defined；27th, steam ejection mechanism.
Embodiment
Lift-off device emission system is described further with reference to the utility model：
Embodiment 1：As shown in Figure 1, Figure 2, Figure 3 and Figure 4, lift-off device emission system described in the utility model, including according to
Horizontal rail 3, arc track 10 and the vertical rail 8 of secondary connection；Rocket 2 is arranged on carrier loader 1, and carrier loader 1 is travelled
In on horizontal rail 3, arc track 10 and vertical rail 8；
Horizontal rail 3, arc track 10 and vertical rail 8 are " work " type rail 23, and the top surface of " work " type rail 23 center is provided with rail
Road groove 22, the dragging hook 19 of the bottom of open loop mobile devices 17 is moved in rail groove 22；
Horizontal rail 3 is provided with the steam ejection mechanism 27 accelerated for carrier loader 1, and steam ejection mechanism 27 is installed on water
The lower section of plate rail road 3, reserves the shifting chute of the power output end motion of steam ejection mechanism 27 in horizontal rail 3, shifting chute with
Rail groove 22 is connected, and the clutch end of steam ejection mechanism 27 is connected with pulling the work of hook 19, drives carrier loader 1 along level
Track 3 starts and accelerated；
The end linking of steam ejection mechanism 27 has linear motor accelerated mechanism A4；Linear motor accelerated mechanism A4 is located at level
On track 3, linear motor accelerated mechanism A4 is linear electric motors, and linear motor accelerated mechanism A4 sides are provided with the suspension coordinated with it
Magnet 24, when carrier loader 1 reaches linear motor accelerated mechanism A4 and accelerated, is to be in magnetic suspension state, makes it can
To obtain bigger kinetic energy.
Arc track 10 is provided with linear motor accelerated mechanism B5, linear motor accelerated mechanism B5 and motor acceleration mechanism A
Tandem array；Linear motor accelerated mechanism B5 is similarly linear electric motors, and its side is equally combined with suspension magnet 24, suspension magnet 24
Overcome the huge centrifugal force that carrier loader 1 is produced on arc track 10, make linear motor accelerated mechanism B5 when accelerating for it,
The friction effects that will not be produced by centrifugal force, so that carrier loader 1 obtains bigger kinetic energy.
Vertical rail 8 is provided with linear motor accelerated mechanism C9, linear motor accelerated mechanism C9 and linear motor accelerated machine
Deceleration device 6 is additionally provided with structure B5 tandem arrays, vertical rail 8, is connected in linear motor accelerated mechanism C9 ends.Linear electric motors
Acceleration mechanism C9 is vertically-mounted linear electric motors, because carrier loader 1 is vertical up on vertical rail 8, so not depositing
The frictional force produced in gravity and centrifugal force, therefore and be not provided with suspension magnet 24, enter linear motor accelerated machine in carrier loader 1
After structure C9, locking electromagnet 16 unclamps locking iron plate 15, and the boost motor of rocket 2 starts, and rocket 2 is left carrier loader 1 and is taken off；
Deceleration device 6 includes deceleration track and deceleration linear electric motors 7, but this section of linear electric motors are that carrier loader 1 provides the side of moving
To opposite power, when carrier loader 1 drives to deceleration device 6, deceleration device 6, which provides retarding power, makes carrier loader 1 fast
Speed is slowed down.
Install and be mounted on suspension magnet 24 at acceleration mechanism A and acceleration mechanism B.
Described lift-off device emission system, horizontal rail 3, arc track 10 and vertical rail 8 are provided with track, linear electric motors
Acceleration mechanism A4, linear motor accelerated mechanism B5 and linear motor accelerated mechanism C9 electromagnet and suspension magnet 24 are arranged on
On track, the bottom of carrier loader 1 is provided with the mobile devices of open loop, open loop mobile devices 17 takes turns 18 and horizontal provided with longitudinally defined
Wheel 26 is limited to limit open loop mobile devices 17 in orbit；Longitudinally defined wheel 18 is provided with two rows, is vertically-mounted, makes delivery
Dolly 1 can be moved in the top surface of " work " type rail 23, laterally defined wheel 26 and be located at the medial surface of open loop mobile devices 17, be horizontal peace
Dress, the both sides of " work " type rail 23 are clamped in both sides, prevent double swerve of the carrier loader 1 when high speed accelerates.
Dragging hook 19 of the open loop mobile devices 17 provided with steam ejection mechanism 27, and the stator 21 with linear electric motors
The mover 20 of cooperation and the suspension rack 25 coordinated with suspension magnet 24；Allow carrier loader 1 and linear electric motors, suspension magnet 24
And the cooperating of steam ejection mechanism 27.
Bracket 13 of the top of carrier loader 1 provided with support rocket 2 bottom, and the support 14 of the body of rocket 2 is supported, and it is solid
Determine the fixing groove 12 of rocket 2.
Provided with locking electromagnet 16 in described lift-off device emission system, fixing groove 12, rocket 2 is provided with " L " type eye-splice
11, bracket 13 is inserted after fixing groove 12 with connection and support that support 14 is only to rocket 2, " L " type eye-splice 11, can be achieved
Rocket 2 is fixed with carrier loader 1, and the one end of " L " type eye-splice 11 is provided with locking iron plate 15, and fixing groove 12 is inserted in " L " type eye-splice 11, and
Coordinate with the locking electromagnet 16 of fixing groove 12, when not reaching vertical rail 8, locking electromagnet 16 holds locking iron plate 15,
Being fixedly connected for rocket 2 and carrier loader 1 is realized, after vertical rail 8 are entered, locking electromagnet 16 unclamps locking iron plate 15,
But " L " type eye-splice 11, still it is inserted in fixing groove 12, after the boost motor of rocket 2 sprays, rocket 2 can be driven with faster
Acceleration accelerates, and makes rocket 2 up more than carrier loader 1, " L " type eye-splice 11 can be made to be extracted out from fixing groove 12, " L " type eye-splice
11 can take connection living with rocket 2, after rocket 2 departs from carrier loader 1, can depart from rocket 2 by release unit.
Described lift-off device emission system, bracket 13 is annular, and bracket 13 holds the bottom of rocket 2, and makes the boosting of rocket 2
Device passes through bracket 13.
Operating procedure and operation principle：
Carrier loader 1 is in simultaneously first for the static starting of carrier loader 1 first by steam ejection mechanism 27 in horizontal rail 3
Accelerate, subsequent carrier loader 1 is suspended magnet 24 and drags suspension, and by linear motor accelerated mechanism A4, linear motor accelerated machine
Structure B5 and linear motor accelerated mechanism C9 accelerate on horizontal rail 3, arc track 10 and vertical rail 8, enter in carrier loader 1
Enter after vertical rail 8, the igniting injection of the boost motor of rocket 2 makes rocket 2 leave carrier loader 1 and taken off.
Specific method is：
(1) carrier loader 1 of the propelling loading rocket 2 of steam ejection mechanism 27, starts and accelerates into linear accelerating mechanism
A；
(2) steam ejection mechanism 27 start after, suspension magnet 24 starts, carrier loader 1 into linear accelerating mechanism A be into
Enter magnetic suspension state, and acceleration is driven by linear accelerating mechanism A；
(3) carrier loader 1 is reached after the linear accelerating mechanism B of arc track 10, is driven by linear accelerating mechanism B and is continued magnetic
Suspend and accelerate；
(4) after carrier loader 1 is reached on vertical rail 8, suspension magnet 24 is departed from, linear accelerating mechanism C continues to drive fortune
Carry dolly 1 to accelerate, locking electromagnet 16 decontrols locking iron plate 15, the boost motor injection of rocket 2 makes rocket 2 depart from carrier loader
1；
(5) linear accelerating mechanism C applies opposition, carrier loader 1 is slowed down.
Claims (4)
1. one kind lift-off device emission system, it is characterised in that including the horizontal rail being sequentially connected, arc track and vertical rail
Road；Rocket is arranged on carrier loader, and carrier loader is travelled on horizontal rail, arc track and vertical rail；
Horizontal rail is provided with the steam ejection mechanism accelerated for carrier loader；The linking of steam ejection mechanism end has linear electric motors
Acceleration mechanism A；
Arc track is provided with linear motor accelerated mechanism B, motor acceleration mechanism B and motor acceleration mechanism A tandem arrays；
Vertical rail is provided with linear motor accelerated mechanism C, linear motor accelerated mechanism C and motor acceleration mechanism B tandem arrays,
Deceleration device is additionally provided with vertical rail, is connected in linear motor accelerated mechanism C-terminal；
Install and be mounted on suspension magnet at acceleration mechanism A and acceleration mechanism B.
2. lift-off device emission system according to claim 1, it is characterised in that horizontal rail, arc track and vertical rail
Road be provided with track, linear motor accelerated mechanism A, linear motor accelerated mechanism B and linear motor accelerated mechanism C electromagnet and
Suspension magnet installs in orbit, and carrier loader bottom is provided with the mobile devices of open loop, open loop mobile devices provided with longitudinal direction limit
Fixed wheel limits open loop mobile devices in orbit with wheel is laterally defined；
Open loop mobile devices provided with steam ejection mechanism dragging link up with, and with linear electric motors coordinate mover and with suspension
The suspension rack that magnet coordinates；
Bracket provided with support rocket bottom at the top of carrier loader, and the support of rocket body is supported, and fix consolidating for rocket
Determine groove.
3. lift-off device emission system according to claim 2, it is characterised in that provided with locking electromagnet, fire in fixing groove
Arrow be provided with " L " type eye-splice, " L " type eye-splice one end provided with locking iron plate, the eye-splice of " L " type insertion fixing groove, and with fixing groove
Electromagnet is locked to coordinate.
4. lift-off device emission system according to claim 3, it is characterised in that bracket is annular, and bracket holds rocket bottom
Portion, and the injector of rocket is passed through bracket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720118105.6U CN206450138U (en) | 2017-02-07 | 2017-02-07 | Lift-off device emission system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720118105.6U CN206450138U (en) | 2017-02-07 | 2017-02-07 | Lift-off device emission system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206450138U true CN206450138U (en) | 2017-08-29 |
Family
ID=59664780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720118105.6U Expired - Fee Related CN206450138U (en) | 2017-02-07 | 2017-02-07 | Lift-off device emission system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206450138U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406697A (en) * | 2018-04-27 | 2019-11-05 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A kind of vehicle launch system based on magnetic suspension electromagnetic booster |
| CN110411276A (en) * | 2018-04-27 | 2019-11-05 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A kind of carrier rocket emission system based on magnetic suspension electromagnetic booster |
-
2017
- 2017-02-07 CN CN201720118105.6U patent/CN206450138U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406697A (en) * | 2018-04-27 | 2019-11-05 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A kind of vehicle launch system based on magnetic suspension electromagnetic booster |
| CN110411276A (en) * | 2018-04-27 | 2019-11-05 | 中国航天科工飞航技术研究院（中国航天海鹰机电技术研究院） | A kind of carrier rocket emission system based on magnetic suspension electromagnetic booster |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170829 Termination date: 20190207 |