CN201494622U - Wired electric flying and floating aircraft - Google Patents
Wired electric flying and floating aircraft Download PDFInfo
- Publication number
- CN201494622U CN201494622U CN2009202221094U CN200920222109U CN201494622U CN 201494622 U CN201494622 U CN 201494622U CN 2009202221094 U CN2009202221094 U CN 2009202221094U CN 200920222109 U CN200920222109 U CN 200920222109U CN 201494622 U CN201494622 U CN 201494622U
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- cable
- track
- motor
- cable track
- transmission cable
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Abstract
The utility model relates to a wired electric flying and floating aircraft, and belongs to the flying and floating field. The aircraft comprises an aerostat and a wired control track device, wherein a capsule cabin, a motor and a propeller are mounted at the bottom part of the aerostat y, and a propeller type thruster is mounted at the tail part of the capsule cabin; the wired control track device comprises a transmission cable, a cable track, a cable track connector, an AC transformer and a DC frequency converter, wherein one end of the transmission cable is connected with a propeller motor for levitation and the motor on the thruster through a power cord connecting device while the other end thereof is connected with the cable track through the cable track connector; the AC transformer for transporting the alternate current is used for connecting the direct current with the transmission cable through cables by dint of the DC frequency converter; and the cable track is mounted and fixed on the ground through a support frame. The utility model has the advantages of extensive levitation range, wide application, multiple functions, energy conservation, environmental protection and no noise, can perform air sport activities of such large-scale activities as low-level aerial photography, tourism, air media advertisements, celebration, and also can work high above the ground according to demands.
Description
Technical field
The utility model relates to the field of wafing that flies, and particularly relates to a kind of flight device by wire cable control.
Background technology
Because the needs that big assembly and shooting, amusement etc. are movable, the unit of various lift-offs are also more and more.But these equipment and device use and operate actual, and its weak point is respectively arranged.Take car as lifting, because lift-off is to realize that by the frame mode adjustable height is limited, vehicle body is huge in addition, when taking in large-scale activity, is unsuitable for walking in the crowd shooting angle and height-limited, this kind vehicle cost also More costliness simultaneously.And use autogyro to carry out the high-altitude when taking, and there is certain danger, be unsuitable on the square of city hive and crowd massing, using.Because Aircraft noise is big, also is very disadvantageous to environment.Remote control is taken photo by plane because wind resistance is relatively poor, restricted by the influence of climatic factor, is difficult to finish predetermined shooting task.The inventor provides a kind of lift-off scope big in " the multi-functional travelling equipment that can go up to the air " (the Granted publication cn201179824y) of application on March 14th, 2008, and range of use is wide, diverse in function, the lift-off device of energy-conserving and environment-protective.But this device needs the electronic car traction control of controlling, and storage battery is heavy, and needs often charging, also has some inconvenient shortcomings.
Summary of the invention
The purpose of this utility model is not highly high at existing lift-off, be used for travelling among a small circle, amusement, the lift-off equipment of shooting and the weak point of device, proposes a kind of electronic flight device of controlling by feed cable.
The technical solution of the utility model is: this flight device comprises the buoyance lift device and the line control rail set is arranged.Passenger cabin, motor and screw propeller are equipped with in the bottom of buoyance lift device, and passenger cabin is arranged in the front position of buoyance lift device bottom, and the passenger cabin afterbody is equipped with the propeller type propelling unit; There is the line control rail set to comprise transmission cable, cable track, cable track adaptor union, AC transformer and DC frequency-changing device.One end of transmission cable is connected with motor on screw propeller motor that is used to go up to the air and the propelling unit by the power cord connecting set of passenger cabin, the other end of transmission cable is connected with the cable track by cable track adaptor union, carry the AC transformer of alternating current by the DC frequency-changing device direct current (DC) to be connected with transmission cable by cable, the cable track installs and fixes on the ground by bracing frame.
Cable track adaptor union comprises grooved card and cable connection contact, and transmission cable is connected with the galvanic cable of transmission by the cable connection contact.
When using the utility model, the buoyance lift device that will be full of unreactable gas earlier is seated on the platform of a track platform.Start the AC transformer switch, alternating current is become direct current (DC) by the DC frequency-changing device.This direct current (DC) is connected with the cable of cable track adaptor union with control buoyance lift device by cable.After the buoyance lift device energized, the chaufeur in the passenger cabin starts the screw propeller motor and begins lift-off, and behind the certain altitude of waiting to go up to the air, the motor that starts on the propelling unit rotates the propelling unit screw propeller, advances the buoyance lift device to move ahead.
The utlity model has following remarkable result:
1, lift-off scope is big.The lift-off of buoyance lift device height can reach between 50 meters to 100 meters, and track length can be according to actual field ground situation, at one kilometer in 100 kilometer range.
2, wide, the diverse in function of range of use.Use the utility model can carry out the low latitude take photo by plane photography, go sightseeing, the activities such as aerial physical culture of large-scale activities such as aerial media advertisement, solid transportation, celebration, also can carry out aloft work as required.
3, when Electric aircraft during in quiescence, the lift-off cable to 1000 that can extend meter makes the buoyance lift device become the highest in the world sightseeing stand.
4, the utility model energy-saving and environmental protection, noise are low, safety, at a high speed, manufacturing expense is low, transportation volume is big.
Brief Description Of Drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a cable track connector construction scheme drawing of the present utility model.
As shown in the figure: 1-buoyance lift device 2-motor 3-lift-off screw propeller 4-propelling unit 5-passenger cabin 6-transmission cable 7-cable track adaptor union 8-feed cable 9-DC frequency-changing device 10 AC transformer 11-cable track 12-bracing frame 13-grooved card 14-cable connection contacts
The specific embodiment
The specific embodiment of the present utility model is illustrated in conjunction with the accompanying drawings: this flight device comprises buoyance lift device (1) and the line control rail set is arranged, passenger cabin (5), motor (2) and screw propeller (3) are equipped with in the bottom of buoyance lift device (1), passenger cabin (5) is arranged in the front position of buoyance lift device bottom, and passenger cabin (5) afterbody is equipped with propeller type propelling unit (4); The power cord connecting set of an end that it is characterized in that transmission cable (6) by passenger cabin (5) and the screw propeller motor (2) that is used to go up to the air are connected with motor on the propelling unit (4), the other end of transmission cable (6) is connected with cable track (11) by cable track adaptor union (7), carry the AC transformer (10) of alternating current by DC frequency-changing device (9) direct current (DC) to be connected with transmission cable (6) by cable (8), cable track (11) installs and fixes on the ground by bracing frame (12).
Can comprise grooved card (13) and cable connection contact (14) along the cable track adaptor union (7) that the cable track slides, transmission cable (6) is connected with cable (8) by cable connection contact (14).Buoyance lift device (1) is for being full of the waving apparatus that flies of unreactable gas.
Claims (2)
1. wire control electric flight device, this aircraft comprises buoyance lift device (1) and the line control rail set is arranged, passenger cabin (5), motor (2) and screw propeller (3) are equipped with in the bottom of buoyance lift device (1), passenger cabin (5) is arranged in the front position of buoyance lift device bottom, and passenger cabin (5) afterbody is equipped with propeller type propelling unit (4); The power cord connecting set of an end that it is characterized in that transmission cable (6) by passenger cabin (5) and the screw propeller motor (2) that is used to go up to the air are connected with motor on the propelling unit (4), the other end of transmission cable (6) is connected with cable track (11) by cable track adaptor union (7), carry the AC transformer (10) of alternating current by DC frequency-changing device (9) direct current (DC) to be connected with transmission cable (6) by cable (8), cable track (11) installs and fixes on the ground by bracing frame (12).
2. wire control electric flight device according to claim 1, it is characterized in that and can comprise grooved card (13) and cable connection contact (14) along the cable track adaptor union (7) that the cable track slides, transmission cable (6) is connected with cable (8) by cable connection contact (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202221094U CN201494622U (en) | 2009-12-18 | 2009-12-18 | Wired electric flying and floating aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202221094U CN201494622U (en) | 2009-12-18 | 2009-12-18 | Wired electric flying and floating aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201494622U true CN201494622U (en) | 2010-06-02 |
Family
ID=42437830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202221094U Expired - Fee Related CN201494622U (en) | 2009-12-18 | 2009-12-18 | Wired electric flying and floating aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201494622U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102030106A (en) * | 2010-11-30 | 2011-04-27 | 杨茂亮 | Omnidirectional traction type rotor reconnaissance aircraft and system thereof |
| CN102040003A (en) * | 2010-12-30 | 2011-05-04 | 吴倌熹 | Orbiter |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN104029811A (en) * | 2013-03-08 | 2014-09-10 | 波音公司 | Autonomous Aircraft |
| GB2526557A (en) * | 2014-05-27 | 2015-12-02 | L C Switchgear Ltd | Power cables |
| CN105228902A (en) * | 2012-12-21 | 2016-01-06 | 欧洲航空防务与空间公司Eads法国 | For fuel resupply device in-flight and the aircraft being equipped with this device of electric memory system |
| CN105292439A (en) * | 2015-11-06 | 2016-02-03 | 东莞华南设计创新院 | Petrol-electric hybrid power airship |
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
| CN107380393A (en) * | 2017-06-06 | 2017-11-24 | 能诚集团有限公司 | A kind of gas-floating facility |
-
2009
- 2009-12-18 CN CN2009202221094U patent/CN201494622U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102030106A (en) * | 2010-11-30 | 2011-04-27 | 杨茂亮 | Omnidirectional traction type rotor reconnaissance aircraft and system thereof |
| CN102040003A (en) * | 2010-12-30 | 2011-05-04 | 吴倌熹 | Orbiter |
| CN105228902A (en) * | 2012-12-21 | 2016-01-06 | 欧洲航空防务与空间公司Eads法国 | For fuel resupply device in-flight and the aircraft being equipped with this device of electric memory system |
| CN104029811A (en) * | 2013-03-08 | 2014-09-10 | 波音公司 | Autonomous Aircraft |
| CN104029811B (en) * | 2013-03-08 | 2017-03-01 | 波音公司 | The operating system of automated spacecraft and operational approach |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| GB2526557A (en) * | 2014-05-27 | 2015-12-02 | L C Switchgear Ltd | Power cables |
| GB2526557B (en) * | 2014-05-27 | 2016-06-29 | L C Switchgear Ltd | Power cables |
| CN105292439A (en) * | 2015-11-06 | 2016-02-03 | 东莞华南设计创新院 | Petrol-electric hybrid power airship |
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
| CN107380393A (en) * | 2017-06-06 | 2017-11-24 | 能诚集团有限公司 | A kind of gas-floating facility |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100602 Termination date: 20121218 |