CN100564160C - Transmitter field on the intermediate ship - Google Patents
Transmitter field on the intermediate ship Download PDFInfo
- Publication number
- CN100564160C CN100564160C CNB2007100709821A CN200710070982A CN100564160C CN 100564160 C CN100564160 C CN 100564160C CN B2007100709821 A CNB2007100709821 A CN B2007100709821A CN 200710070982 A CN200710070982 A CN 200710070982A CN 100564160 C CN100564160 C CN 100564160C
- Authority
- CN
- China
- Prior art keywords
- car launcher
- magnetic
- levitation
- aircraft
- ship
- 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.)
- Expired - Fee Related
Links
Images
Abstract
Transmitter field is with the power of synchronous linear electric motor as car launcher 1 on the intermediate ship, just scolds floating type magnetic suspension car launcher 1 to load the aircraft that will launch with superconduction and carries out launch; Superconducting coil 5 excitation magnetic action are being adorned in the left and right sides of car launcher 1, and the propulsion coil 21 of 20 liang of inboards of track plays the armature effect; Give propulsion coil 21 for variable-frequency power sources, along with car launcher 1 and track 20 relative motions, the phase place of control propulsion coil 21 voltages is identical with the phase place of propulsion coil electric current, controls propulsion coil 21 power frequencies and amplitude, just can handle the speed and the thrust size of car launcher 1.Advantage a, emission V>500km/h, big angle of attack grade climbing performance and bob are penetrated (taking off) stroke, adapt to emission small-sized (no alighting gear) aircraft on the ship; B, saving airport space are strengthened the examination of marine fishing and science, promote ocean civil military cooperation, unity; C, cast out---form pneumatic, flow conditions earlier from driving engine, advance the indirect mode of aircraft taxi with aerodynamic force, and greatly shorten the departure time with the magnetic suspension superconduction, energy-saving and emission-reduction.
Description
Technical field
The present invention is the quick airport of lift-off of blimp in energy-saving and emission-reduction field, is particularly useful for launching on the intermediate ship of 6-7 ton.
Background technology
China is assembled by multi-national assimilation, but a lot of national assimilation is to China, and their ancestors fail to observe original place of origin ancestor motherland territory, by foreign country's predation, causes today China to have a large population and a few land, and one of our outlet is to migrate to the ocean.The Zhoushan in science and technology newspaper report on July 17th, 2007 area, Ningbo, Zhejiang is fishing capital city, nowadays can make all kinds of boats and ships of 8 tons and export to foreign countries.
Summary of the invention
Purpose of the present invention just provides transmitter field on a kind of intermediate ship, to satisfy the quick landing of blimp.
In order to realize foregoing invention purpose of the present invention, the technical scheme that the present invention takes is: the deck layer that comprises ship, it is characterized in that, comprise that car launcher, magnetic-levitation, support roller, little support roller, back hook and superconduction scold floating type magnetic suspension facility, on described deck, magnetic-levitation is housed, in this magnetic-levitation, car launcher is installed; Described car launcher is the groove of U type cross section shape, adorning the superconducting coil of refrigerator pipes circulating liquid nitrogen cooling in two outsides of this U type groove, this U type groove by a front and back number U-shaped rib and vertical several rod members between being connected constitute, be lined with the magnetic radiation barrier layer in the groove, central space is equipped with liquid nitrogen container; The last notch on the U type groove both sides of described car launcher is equipped with two row's support rollers, covers slightly resilient rubber layer outside this support roller, and this two row holds the support roller of aircraft ventral portion, and going ahead extends on two forearms about being contained in; But the back hook of lifting is housed at the rear portion of described car launcher, the axle hinge of this back hook is on described car launcher, when the handle of a cam is vertical, the hook lifting of the described back of this cam jack-up, the back hook of lifting is used for blocking the belly hook of aircraft, and this belly hook can carry when stretching out ventral to head, to the power of tail direction; On described magnetic-levitation, be equipped with little support roller and with the corresponding propulsion coil of described superconducting coil.
Advantage of the present invention: a, emission V>500km/h, big angle of attack grade climbing performance and bob are penetrated (taking off) stroke, adapt to emission small-sized (no alighting gear) aircraft: b on the ship, save airport space: strengthen the examination of marine fishing and science, promote ocean civil military cooperation, unity; C, cast out---form pneumatic, flow conditions earlier from driving engine, advance the secondary fire mode of aircraft taxi again with aerodynamic force, and greatly shorten the departure time with the magnetic suspension superconduction, energy-saving and emission-reduction.
Description of drawings
The lateral plan that Fig. 1 is magnetic suspension car launcher launch plane, take off on intermediate ship.
Fig. 2 is the section drawing of magnetic suspension car launcher launch plane.
Fig. 3 is the position view of magnetic-levitation 20 on intermediate ship.
The specific embodiment
Referring to Fig. 1, be the lateral plan that superconduction scolds floating type magnetic suspension car launcher launch plane to take off on intermediate ship.Car launcher 1 is the framework (the double Fig. 2 of seeing) in U type cross section, and superconducting coil 5 (Fig. 1 has heat screen outward) is being adorned in two outsides of framework, refrigerator pipes 6 circulating liquid nitrogens cooling superconducting coil; Between several the U-shaped ribs 9 in front and back, connected the groove that becomes U type cross section shape admittedly by vertical several rod members, be lined with the magnetic radiation barrier layer in the groove, central space is equipped with liquid nitrogen container 8.The last notch on the U type groove both sides of car launcher 1 is equipped with two row's support rollers 2 (covering rubber layer outward, slightly flexible), and this two row holds the support roller 2 of aircraft ventral portion, and going ahead extends on two forearms 3 about being contained in.
But the back hook 4 of lifting is equipped with at the rear portion of car launcher 1, is used for blocking the belly hook D of aircraft during its lifting, and D is when stretching out ventral, to head, can carry to the power of tail direction.(existing addressing in the application number 2007100704211; Fig. 3 at application number 200710070081.2 has block diagram).When the handle of cam 10 is vertical, hook 4 liftings after the jack-up, back hook 4 with its axle 4a hinge on car launcher 1.
All belong to the car launcher assembly in the outline line that Fig. 1 paints with thick black line, it is to adorn the aircraft that is launched in magnetic-levitation 20, scold floating type magnetic suspension launch plane with superconduction.The 30th, install roller aboard ship, be used for aircraft is drawn on the car launcher 1, the 31st, traction wheel, they are located at the left and right sides (can have several to) of back hook 4, through swing arm 32, axle 33 hinges aboard ship, make traction wheel 31 inflation rubber tires push against ventral, lead capable aircraft and roll on car launcher, the synchronous strap drive of traction wheel 31, but forward and backward revolution and fine motion with balancing device 34 (illustrating with extension spring among Fig. 1).
Fig. 1, the 35th, pneumatic piston (also dress is aboard ship), be used for the lower end final position of spacing car launcher 1: when car launcher 1 carries aircraft at magnetic-levitation, be in when beginning to advance on the magnetic-levitation 20 in level stage, lack magnetic suspension force during initial velocity, only on little support roller 22, advance, along with speed of advance increases, car launcher 1 enters the arc track section of climbing, just realize magnetic suspension ..., when the car launcher magnetcisuspension floats to limes superiors near magnetic-levitation 20 (going up terminal), cam handle is blocked earlier, toward post deflection, cause cam to lose top power, back hook 4 is descended, and the power supply on the track disconnects simultaneously, allows the support roller 2 of aircraft along forearm 3, holder rises once more, fly away from transmitter field, broken electric car launcher 1 with gravity, glided along little support roller 22, up to following terminal point (Fig. 1 of magnetic-levitation 20, Fig. 2).
The three-dimensional dimension of car launcher: 1, at the long ≈ 6m in U type section slot position, high 1m, wealthy ≈ 0.9m; Two outsides fork that turns to suitable for reading of U type is loaded onto (little support roller is used) angle steel baby track 2b, the length ≈ 5m of support roller 2 and carriage 2a:2, forearm 3; 3, the long ≈ 1.6m of back hook (frame), back hook (frame) has only one, is under the longitudinal axis of ventral.The width ≈ 1.8m of magnetic-levitation 20.
Fig. 2, F are the aircraft cross sections, the D belly hook, profile and the hatching place wideer than belly hook D are back hooks 4 (Fig. 1), the 2nd, and support roller, 2a roller frame, the 1st, car launcher, 2b are baby track (can be placed on the little support roller 22 and slide), the 6th, and liquid nitrogen pipe, the 9th, U type rib, 5 superconducting coils, 8 liquid nitrogen containers, 9a roller slide rail (everywhere), be as liquid nitrogen container push or pull out and locate usefulness, little support roller 22 is housed on magnetic- levitation 20,21 propulsion coils, 20a strengthens strut.
Fig. 3, the 20th, magnetic-levitation, the outer deck layer that stretches of the left and right sides of B ship, C be the iron tower that dots, about divide the deck layer outer edge that stands in B, the top of tower C has crossbeam to connect the discrete C in the left and right sides; So can launch plane on the magnetic-levitation 20.
Floating type magnetic suspension feedway principle explanation is scolded in first, superconduction:
A, principle of work: the propelling of superconducting magnetic suspension system, suspension, guidance coil, all be that the magnetic flux that hollow aircored coil does not add any control can produce three dimensional space power, but because superconducting coil is equipped with in the framework of the car launcher outside, just cause propelling, suspension, guiding that effect is all arranged, the coil that forms in the magnetic-levitation has propelling and guiding, suspends and the combined action of leading.
B, principle of propeller: with the propulsive force of synchronous linear electric motor (LSM) as car launcher, the superconducting coil excitation magnetic action in the car launcher frame outside, the magnetic-levitation inboard is established propulsion coil and is played the armature effect.Given at the propulsion coil of magnetic-levitation inboard by the power supply converter plant now and power (figure) along with car launcher and magnetic-levitation relative motion, electric current changes to some extent in the propulsion coil.The phase place of the phase place propulsion coil electric current of control propulsion coil voltage is identical, controls the power frequency and the current amplitude of propulsion coil, just can handle the speed and the thrust size of car launcher.The pacemaker of car launcher is set in the following terminal of magnetic-levitation forever, so during the emission beginning, the coil on the magnetic-levitation and the opposite position of the superconducting coil on the car launcher also are to preestablish unmodified, thus car launcher when at every turn launching, not can with corresponding current phhase dislocation in the coil in the magnetic-levitation.
C, suspension theory: superconducting coil is established in the car launcher frame outside, establish suspended coil in the magnetic-levitation aside, when being advanced generation speed by synchronous linear electric motor with car launcher, change with the magnetic flux of the circle intersecting chain that suspends, form suspended coil interior generation electric current (this is a generator principle) this inducing current and the superconducting coil generation same sex and repel each other---produce lift force.Lift force increases with speed.For keeping the low-temperature superconducting performance of superconducting coil, with vehicle-mounted liquid nitrogen cooling system cooling.But, simplify car launcher equipment, weight, can not establish vehicle-mounted fefrigerator, as changing liquid nitrogen container as the automatic ramming: be exactly after car launcher is launched the aircraft lift-off, to return to close on to withdraw from liquid nitrogen container when terminal point is descended in emission, press the next liquid nitrogen container of using immediately, the liquid nitrogen container of having used is sent into cool room.This only is only applicable to general ocean goer and uses the airport, and military airfield can not be used this mode, and the military aircraft frequency that launches: if the other side launched an aircraft in per 2 minutes, our every emission once circulates must be less than one minute.
D, guiding principle: guiding principle is identical with suspension theory, suspended coil as left and right sides links up mutually, just form the shared compound suspension guidance system of guidance coil and propulsion coil (existing addressing in a, the principle of work in the above), but the direction of the guidance coil of left and right sides generation power is in opposite directions (being that direction differs 180 degree).
If the present invention is equipped with aircraft, the police of landing on the ship, can be used for safeguarding the ocean scientific investigation, fish for, give first aid to, monitor foreign scientific and technological achievement of adopting steathily on Chinese marine resources or the high sea, also, naval supports the army simultaneously for being subjected to more direct fisherman (ocean immigrant) in the ocean, promote the army and the people and cooperate unity, strengthen ocean the army and the people troop, improve the sophisticated technologies equipment, enrich the ocean innovation achievement, can inspire more people in marine cause, to obtain employment, or dedicate oneself to Defence business.
Claims (3)
1, transmitter field on a kind of intermediate ship, comprise the deck layer of ship, it is characterized in that, comprise that car launcher, magnetic-levitation, support roller, back hook and superconduction scold floating type magnetic suspension facility, on described deck, magnetic-levitation is housed, in this magnetic-levitation, car launcher is installed; Described car launcher is the framework in U type cross section, the superconducting coil of refrigerator pipes circulating liquid nitrogen cooling is being adorned in two outsides of this framework, connected the groove that becomes U type cross section shape admittedly by vertical several rod members between several the U-shaped ribs in front and back, be lined with the magnetic radiation barrier layer in the groove, central space is equipped with liquid nitrogen container, and between is equipped with the roller and the slide rail that push or pull out and locate usefulness as liquid nitrogen container; The last notch on the groove both sides of the U type cross section shape of described car launcher is equipped with two row's support rollers, covers slightly resilient rubber layer outside this support roller, and this two row holds the support roller of aircraft ventral portion, and going ahead extends on two forearms about being contained in; But the back hook of lifting is housed at the rear portion of described car launcher, the axle hinge of this back hook is on described car launcher, when the handle of a cam is vertical, the hook lifting of the described back of this cam jack-up, the back hook of lifting is used for blocking the belly hook of aircraft, and this belly hook can carry when stretching out ventral to head, to the power of tail direction; On described magnetic-levitation, be equipped with little support roller and with the corresponding propulsion coil of described superconducting coil.
2, transmitter field on the intermediate ship according to claim 1 is characterized in that, on the ship in the final position, lower end that is positioned at described magnetic-levitation pneumatic piston is housed, and is used for the lower end final position of spacing car launcher at magnetic-levitation.
3, transmitter field on the intermediate ship according to claim 1 is characterized in that, described magnetic-levitation is made up of level stage and arc track section.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB2007100709821A CN100564160C (en) | 2007-08-21 | 2007-08-21 | Transmitter field on the intermediate ship |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNB2007100709821A CN100564160C (en) | 2007-08-21 | 2007-08-21 | Transmitter field on the intermediate ship |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101229850A CN101229850A (en) | 2008-07-30 |
CN100564160C true CN100564160C (en) | 2009-12-02 |
Family
ID=39896751
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB2007100709821A Expired - Fee Related CN100564160C (en) | 2007-08-21 | 2007-08-21 | Transmitter field on the intermediate ship |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN100564160C (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104071346B (en) * | 2013-03-26 | 2017-04-19 | 孟金来 | Linear accelerator |
CN106314814B (en) * | 2016-09-28 | 2018-12-18 | 天津大学 | A kind of field the scientific research portable launching apparatus of fixed-wing unmanned plane and application method |
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 |
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 |
CN110371312B (en) * | 2019-08-20 | 2023-01-03 | 哈尔滨工程大学 | Discontinuous electromagnetic catapult |
CN111993980A (en) * | 2020-07-21 | 2020-11-27 | 南昌航空大学 | Unmanned aerial vehicle magnetic suspension take-off and landing device |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1394777A (en) * | 2002-08-02 | 2003-02-05 | 黄先革 | Gas suspension vehicle for track transportation and space launching and its special-purpose equipment |
-
2007
- 2007-08-21 CN CNB2007100709821A patent/CN100564160C/en not_active Expired - Fee Related
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1394777A (en) * | 2002-08-02 | 2003-02-05 | 黄先革 | Gas suspension vehicle for track transportation and space launching and its special-purpose equipment |
Non-Patent Citations (8)
Title |
---|
与磁悬浮车辆现有超导磁体合为一体的线性发动机. H.Hasegawa等.变流技术与电力牵引. 2005 |
与磁悬浮车辆现有超导磁体合为一体的线性发动机. H.Hasegawa等.变流技术与电力牵引. 2005 * |
几种典型的高速磁悬浮列车方案比较. 张瑞华,严陆光,徐善纲,武瑛.电工电能新技术,第23卷第2期. 2004 |
几种典型的高速磁悬浮列车方案比较. 张瑞华,严陆光,徐善纲,武瑛.电工电能新技术,第23卷第2期. 2004 * |
可重复使用运载器磁悬浮助推发射参数研究. 杨文将,刘宇.飞行力学,第24卷第2期. 2006 |
可重复使用运载器磁悬浮助推发射参数研究. 杨文将,刘宇.飞行力学,第24卷第2期. 2006 * |
航天发射用磁悬浮助推发射系统概念研究. 杨文将,刘宇,杨博.北京航空航天大学学报,第31卷第1期. 2005 |
航天发射用磁悬浮助推发射系统概念研究. 杨文将,刘宇,杨博.北京航空航天大学学报,第31卷第1期. 2005 * |
Also Published As
Publication number | Publication date |
---|---|
CN101229850A (en) | 2008-07-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN100564160C (en) | Transmitter field on the intermediate ship | |
JP4880795B1 (en) | Departing and landing aircraft, takeoff equipment and hull reduction equipment | |
CN106585899A (en) | Fishing vessel with seawater desalting device | |
US20150203184A1 (en) | Sail-equipped amphibious aerostat or dirigible | |
CN2761521Y (en) | Tourist aircraft carrier | |
CN110386257A (en) | For vertical translation aircraft warship device and naval vessel | |
CN100551779C (en) | Destination on the intermediate ship | |
CN201148207Y (en) | Motor driven hydrofoil bionic thruster | |
CN106945807A (en) | A kind of unmanned air cushion platform without flight-deck aircraft carrier | |
CN201712793U (en) | Novel aircraft catapult | |
CN106080955A (en) | Eliminate passenger-cargo ultrahigh speed ship and the ultrahigh speed combat vessel of wave making resistance | |
CN115675805B (en) | Cross-medium carrying unmanned aerial vehicle submarine | |
CN115891529A (en) | Separable unmanned aerial vehicle body and control method thereof | |
CN116353861A (en) | Integrated inspection, beating and supplementing type split, recycling and supplementing cross-medium unmanned platform and system | |
CN204021244U (en) | Waters runway military aircraft lifting gear | |
GB517331A (en) | Improvements connected with the catapulting of aircraft | |
Sutherland et al. | The RAF Air Sea Rescue Service, 1918–1986 | |
CN85105602A (en) | Jet Propellent aircraft | |
CN105197238A (en) | Transformable pump jetting craft ship provided with flapping wings and equipped with pneumatic energy cannon structure | |
CN105501458A (en) | Track block chain shipboard aircraft catapult | |
CN107685844B (en) | Multi-functional aircraft carrier | |
CN201385784Y (en) | Aircraft carrier launching device | |
CN210478996U (en) | High-efficiency propelling speedboat | |
Still | Electromagnetic launchers for use in aircraft launch at sea | |
Gonçalves-Coelho et al. | Tests of a light UAV for naval surveillance |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C56 | Change in the name or address of the patentee | ||
CP02 | Change in the address of a patent holder |
Address after: 315327, Zhejiang, Cixi Province East Town Industrial Zone Wei two road Ningbo man and Mechanical Bearing Co., Ltd. Patentee after: Huang Jinlun Address before: 315327, No. 457-459, Zhen Zhen Dong Road, Cixi, Zhejiang Patentee before: Huang Jinlun |
|
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091202 Termination date: 20110821 |