CN107554809A - Aircraft carrier hoistable platform based on linear electric motors driving - Google Patents
Aircraft carrier hoistable platform based on linear electric motors driving Download PDFInfo
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- CN107554809A CN107554809A CN201710813903.5A CN201710813903A CN107554809A CN 107554809 A CN107554809 A CN 107554809A CN 201710813903 A CN201710813903 A CN 201710813903A CN 107554809 A CN107554809 A CN 107554809A
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- platform
- linear motor
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- carrier
- aircraft
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Abstract
Aircraft carrier hoistable platform of the present invention based on linear electric motors driving is mainly used in aircraft carrier lifting aircraft utilization, and its equipment is light and handy, and maintenance of equipment is simple, and movement aircraft is rapid；It mainly includes platform, multiple linear motor stator electrics, multiple linear motor rotors；Its operation principle is:Carrier-borne aircraft is after hangar is pushed into platform, start the positive power supply of multiple linear motor rotors, linear motor rotor does linear motion vertically upward, and do linear motion vertically upward with moving platform, after platform rises to the height of flight-deck, the linear motor rotor on the left side rises a segment distance again, the linear motor rotor on the right remains stationary as, platform is set to have certain inclination, carrier-borne aircraft enters flight-deck after platform pull-out, then the reverse electrical source of multiple linear motor rotors is started, linear motor rotor does linear motion vertically downward with moving platform, after platform drops to the height of hangar deck, linear motor rotor enters melt pit, wait next carrier-borne aircraft movement.
Description
Technical field
Present invention is mainly used for aircraft carrier to lift aircraft utilization.
Background technology
It is big jacking equipment volume to be all present in the carrier-borne aircraft hoistable platform that aircraft carrier uses at present, and equipment is heavy, and it is empty to take aircraft carrier
Between big, the problems such as movement aircraft is slow.
The content of the invention
The present invention solves above mentioned problem, and its equipment is light and handy, and maintenance of equipment is simple, and movement aircraft is rapid；It mainly includes
Platform（1）, multiple linear motor stator electrics（2）, multiple linear motor rotors（3）, central shaft（4）, flight-deck（5）, hangar first
Plate（6）, melt pit（7）；Central shaft（4）Upper end and platform（1）Lower end fix, central shaft（4）Lower end and melt pit（7）Ground
Face is fixed, linear motor stator electric（2）There is through hole（8）, central shaft（4）Through linear motor stator electric（2）Through hole（8）, central shaft
（4）With linear motor stator electric（2）Through hole（8）Inwall fix；Its operation principle is:Hangar deck of the carrier-borne aircraft from hangar
（6）Upper push-in platform（1）Afterwards, multiple linear motor rotors are started（3）Positive power supply, linear motor rotor（3）Along straight-line electric
Machine stator（2）Linear motion vertically upward is done, and with moving platform（1）Linear motion vertically upward is done, works as platform（1）Rise
To flight-deck（5）Height after, the linear motor rotor on the left side（3）Rise a segment distance, the linear motor rotor on the right again
（3）Remain stationary as, make platform（1）There is certain inclination, carrier-borne aircraft is from platform（1）Enter flight-deck after pull-out（5）, Ran Houqi
Move multiple linear motor rotors（3）Reverse electrical source, linear motor rotor（3）Along linear motor stator electric（2）Do vertically downward
Linear motion, and with moving platform（1）Linear motion vertically downward is done, works as platform（1）Drop to hangar deck（6）Height
Afterwards, linear motor rotor（3）Into melt pit（7）, wait next carrier-borne aircraft movement.
Brief description of the drawings
Description of reference numerals：1- platforms, 2- linear motor stator electrics, 3- linear motor rotors, 4- central shafts, 5- flight first
Plate, 6- hangar decks, 7- melt pits, 8- holes.
Fig. 1 is the vertical cross section schematic diagram of the present invention.
Fig. 2 is the vertical cross section schematic diagram that aircraft is down to hangar deck.
Fig. 3 is that aircraft rises to flight-deck and the vertical cross section schematic diagram in heeling condition.
Fig. 4 is the A-A profiles of the present invention.
The horizontal profile schematic diagram of Fig. 5 linear motor rotors.
The horizontal profile schematic diagram of Fig. 6 linear motor stator electrics.
Fig. 7 is the schematic top plan view of the present invention.
Embodiment
The embodiment of the present invention has been described in detail in the content of the invention, is not repeated herein, needs to illustrate：The present invention's
For linear electric motors using tubular linear motor, the operation principle of this linear electric motors has been known technology, is not repeated herein.
Claims (1)
1. based on the aircraft carrier hoistable platform of linear electric motors driving, it is characterized in that：It mainly includes platform（1）, Duo Gezhi
Line motor stator（2）, multiple linear motor rotors（3）, central shaft（4）, flight-deck（5）, hangar deck（6）, melt pit（7）；
Central shaft（4）Upper end and platform（1）Lower end fix, central shaft（4）Lower end and melt pit（7）Ground fix, straight-line electric
Machine stator（2）There is through hole（8）, central shaft（4）Through linear motor stator electric（2）Through hole（8）, central shaft（4）With linear electric motors
Stator（2）Through hole（8）Inwall fix；Its operation principle is:Hangar deck of the carrier-borne aircraft from hangar（6）Upper push-in platform
（1）Afterwards, multiple linear motor rotors are started（3）Positive power supply, linear motor rotor（3）Along linear motor stator electric（2）Do vertical
Straight upward linear motion, and with moving platform（1）Linear motion vertically upward is done, works as platform（1）Rise to flight-deck（5）
Height after, the linear motor rotor on the left side（3）Rise a segment distance, the linear motor rotor on the right again（3）Remain stationary as, make
Platform（1）There is certain inclination, carrier-borne aircraft is from platform（1）Enter flight-deck after pull-out（5）, then start multiple linear electric motors
Mover（3）Reverse electrical source, linear motor rotor（3）Along linear motor stator electric（2）Linear motion vertically downward is done, and is driven
Platform（1）Linear motion vertically downward is done, works as platform（1）Drop to hangar deck（6）Height after, linear motor rotor
（3）Into melt pit（7）, wait next carrier-borne aircraft movement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710813903.5A CN107554809A (en) | 2017-09-11 | 2017-09-11 | Aircraft carrier hoistable platform based on linear electric motors driving |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710813903.5A CN107554809A (en) | 2017-09-11 | 2017-09-11 | Aircraft carrier hoistable platform based on linear electric motors driving |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107554809A true CN107554809A (en) | 2018-01-09 |
Family
ID=60980490
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710813903.5A Pending CN107554809A (en) | 2017-09-11 | 2017-09-11 | Aircraft carrier hoistable platform based on linear electric motors driving |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107554809A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019201125A1 (en) * | 2018-04-16 | 2019-10-24 | 王武生 | Multi-level aircraft parking device for aircraft carrier |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100294188A1 (en) * | 2009-05-20 | 2010-11-25 | Hsu-Cheng Wang | Double level flight deck type aircraft carrier |
| CN202785189U (en) * | 2012-04-16 | 2013-03-13 | 美奥快速电梯（苏州）有限公司 | Double excitation motor energy-saving elevator |
| CN203047533U (en) * | 2012-08-31 | 2013-07-10 | 赵天烁 | Slope-gliding launching platform for shipboard aircraft, and application aircraft carrier |
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN106428601A (en) * | 2015-09-11 | 2017-02-22 | 陈德荣 | Method for greatly increasing number of aircrafts picked up by aircraft carrier |
-
2017
- 2017-09-11 CN CN201710813903.5A patent/CN107554809A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100294188A1 (en) * | 2009-05-20 | 2010-11-25 | Hsu-Cheng Wang | Double level flight deck type aircraft carrier |
| CN202785189U (en) * | 2012-04-16 | 2013-03-13 | 美奥快速电梯（苏州）有限公司 | Double excitation motor energy-saving elevator |
| CN203047533U (en) * | 2012-08-31 | 2013-07-10 | 赵天烁 | Slope-gliding launching platform for shipboard aircraft, and application aircraft carrier |
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN106428601A (en) * | 2015-09-11 | 2017-02-22 | 陈德荣 | Method for greatly increasing number of aircrafts picked up by aircraft carrier |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019201125A1 (en) * | 2018-04-16 | 2019-10-24 | 王武生 | Multi-level aircraft parking device for aircraft carrier |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180109 |