CN1084818A - Wire control electric airplane - Google Patents
Wire control electric airplane Download PDFInfo
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- CN1084818A CN1084818A CN 93102904 CN93102904A CN1084818A CN 1084818 A CN1084818 A CN 1084818A CN 93102904 CN93102904 CN 93102904 CN 93102904 A CN93102904 A CN 93102904A CN 1084818 A CN1084818 A CN 1084818A
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- control electric
- wire control
- guide rail
- fuselage
- described wire
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Abstract
The present invention relates to a kind of wire control electric airplane that uses ground electrical power to drive, especially wire control electric autogyro, belong to a kind of later-model transport facility, this aircraft is made of fuselage, propelling unit, alighting gear, main difference is that the actuating device on the machine is an electrical motor, and aircraft is connected by the electrical guide rail of cable and current colector and ground laying.It is comparatively simple that the present invention has self structure, and relevant auxiliary facilities is easy, whole service system small investment, efficiency of loading height, the characteristics that ability is strong.The present invention can be suitable for the long-distance transportation occasion and use.
Description
The present invention relates to a kind of wire control electric airplane that uses ground electrical power to drive, wire control electric autogyro especially, belong to a kind of transport facility.
Existing transport facility, as automobile and train, though himself structure is comparatively simple, cost of manufacture is also lower, but because auxiliary facility highway, the railway one-time investment of relative set are bigger, thereby its development still is subjected to certain restriction, and it is comparatively easy that aircraft, particularly autogyro have auxiliary facility, delivers fireballing characteristics, yet their self structure complexity, the cost of manufacture height need carry fuel during operation, and the energy that is consumed is also very expensive.
The objective of the invention is to avoid above-mentioned weak point and a kind of wire control electric airplane that uses ground electrical power to drive is provided, not only self structure is comparatively simple for it, and relevant auxiliary facilities is also very easy, has the total system small investment, delivers fast characteristic.
Purpose of the present invention is realized by following scheme: have on fuselage 4a, the fuselage and be equipped with propelling unit, alighting gear 6 is equipped with in the fuselage below, its difference is that the actuating device on the machine is an electrical motor 5, and aircraft is connected by the electrical guide rail 1 of cable 2 and current colector 8 and ground laying.
Press such scheme, during operation, aircraft obtains propulsion source by the current colector 8 of cable 2 and slip from ground, start the direct motor drive propelling unit, makes aircraft lift away from ground, and flies forward along the electrical guide rail direction.Owing to adopt electrical motor as actuating device, can make the aircraft power setting obtain bigger simplification, the structure of whole airplane is also simplified simultaneously, weight is corresponding to be alleviated, simultaneously, adopt the power delivery mode of electrical guide rail, both can remove the inconvenience of aircraft from, reduce the cost of energy consumption again, and also make actuating device of the present invention become more easy to be reliable from carrying fuel, relevant auxiliary facilities of the present invention is an electrical guide rail, it is comparatively simple and easy that installation is set on ground, from the whole service system, compares with other traffic and transportation system, has small investment, the efficiency of loading height, the characteristic that ability is strong.
Aircraft of the present invention is usually in low-latitude flying, and electrical guide rail 1 can be laid along ground, also can resemble high up in the air setting up the electric wireline, and current colector 8 keeps sliding synchronously with autogyro at the lower edge electrical guide rail 1 that drags of cable 2.
Fig. 1 is the structural diagrams of one embodiment of the invention.
Fig. 2 is the section drawing of a kind of current colector of the present invention and electrical guide rail embodiment.
Fig. 3 is the block diagram of current colector among Fig. 2.
Fig. 4 is the section drawing of the another kind of electrical guide rail embodiment of the present invention.
Fig. 5 be with Fig. 4 in the current colector section drawing of electrical guide rail phase configuration.
Fig. 6 is the birds-eye view of Fig. 5.
Fig. 7 is the lateral plan of Fig. 5.
Fig. 8 is the section drawing of the third electrical guide rail of the present invention embodiment.
Fig. 9 be with Fig. 8 in the section drawing of current colector of electrical guide rail phase configuration.
Figure 10 is the block diagram of current colector among Fig. 9.
Figure 11 is the section drawing of the 4th kind of current colector of the present invention and electrical guide rail embodiment.
Figure 12 is the block diagram of current colector among Figure 11.
Embodiments of the invention such as Fig. 1,2,3,4,5,6,7,8,9,10,11, shown in 12, be a kind of wire control electric autogyro, has fuselage 4a, the top of fuselage is equipped with horizontal propeller (propeller) 4, also vertical pusher 16 can be set in fuselage front and back or side, the fuselage below is provided with alighting gear 6, in the fuselage both sides wing can also be set as required, be installed on electrical motor 5 in the cabin as actuating device, the cable 2 of aircraft is connected through current colector 8 and electrical guide rail 1 and obtains electric power, be provided with cable wheel 3 in the machine, be used for regulating at any time the length of cable 2, current colector 8 has and the electrical guide rail cross section cavity of fit mutually, can on electrical guide rail 1, slidably reciprocate, and send electric power to cable 2, current colector and cable connection place are provided with universal-joint 7, current colector of the present invention can adopt multiple version, with corresponding electrical guide rail phase configuration, Fig. 2,3 is one of them embodiment, adopt monorail, electrical guide rail 1 is made of I shape rail 9, the centre accompanies insulating barrier 15, the top dual-side has lead 14, current colector is then by the electrode slide 12 that is set on the electrical guide rail, constitute with lead 14 contacted current collection pulleys 11 and guide wheel 10, can set up anti-backlash mechanism on the current collection pulley 11, the centre of electrode slide 12 also is provided with insulating barrier 13.Another embodiment of current colector 8 is shown in Fig. 4,5,6,7, electrical guide rail is made up of the lead 14 and the insulating barrier 15 of fluted body rail 9, both sides, the current colector cross section is the font of falling T, has electrode slide 12, the centre is provided with insulating barrier 13, down either side is equipped with respectively 3 pieces on current collection pulley 11, and current colector is installed in the groove of electric power guide wheel.The 3rd embodiment of current colector is shown in Fig. 8,9,10, electrical guide rail is made of tubular type rail 9, both sides are provided with lead 14, the centre accompanies insulating barrier 15, current colector is a column construction, be provided with the groove that matches with lead 14 in the both sides of electrode slide 12, can set the current collection pulley in the groove, there is insulating barrier 13 centre of electrode slide.The 4th embodiment of current colector of the present invention is shown in Figure 11,12, its structure and first embodiment are roughly the same, difference from above the dead slot of electrode slide 12, also installing guide wheel 10, directly be installed on universal-joint section header 7 on this external electrode slide 12.Electrical guide rail of the present invention also can be arranged to double rail type, along the electrical guide rail sectional distribution substation is set, and situation and existing power locomotive transmission system are similar.
Claims (9)
1, a kind of wire control electric airplane that uses ground electrical power to drive, have fuselage 4a, be equipped with propelling unit on the fuselage, alighting gear 6 is equipped with in the fuselage below, it is characterized in that the actuating device on the machine is an electrical motor 5, aircraft is connected by the electrical guide rail 1 of cable 2 and current colector 8 and ground laying.
2, by the described wire control electric airplane of claim 1, it is characterized in that the fuselage top is equipped with horizontal propeller 4, vertical pusher 16 can be set in fuselage front and back or side.
3, by claim 1 or 2 described wire control electric airplanes, it is characterized in that aircraft is the wire control electric autogyro.
4, by claim 1 or 2 described wire control electric airplanes, it is characterized in that the fuselage both sides are provided with wing.
5,, it is characterized in that being provided with in the machine cable wheel 3 by claim 1 or 2 described wire control electric airplanes.
6,, it is characterized in that electrical guide rail 1 adopts monorail by claim 1 or 2 described wire control electric airplanes.
7, by the described wire control electric airplane of claim 6, it is characterized in that electrical guide rail 1 is made of I shape rail 9, the centre accompanies insulating barrier 15, the top dual-side has lead 14, current colector then is made of the electrode slide 12, current collection pulley 11 and the guide wheel 10 that are set on the electrical guide rail, and the centre of electrode slide 12 also is provided with insulating barrier 13.
8, by the described wire control electric airplane of claim 7, it is characterized in that above the dead slot on the current colector electrode slide 12, also can installing guide wheel 10, on electrode slide 12, directly be installed on universal-joint section header 7.
9, by the described wire control electric airplane of claim 6, it is characterized in that electrical guide rail is made up of the lead 14 and the insulating barrier 15 of fluted body rail 9, both sides, the current colector cross section is the font of falling T, and the centre of electrode slide 12 is provided with insulating barrier 13, and down either side is equipped with current collection pulley 11.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93102904 CN1084818A (en) | 1993-03-12 | 1993-03-12 | Wire control electric airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93102904 CN1084818A (en) | 1993-03-12 | 1993-03-12 | Wire control electric airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1084818A true CN1084818A (en) | 1994-04-06 |
Family
ID=4984377
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 93102904 Pending CN1084818A (en) | 1993-03-12 | 1993-03-12 | Wire control electric airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1084818A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1326748C (en) * | 2002-03-26 | 2007-07-18 | 刘毅 | Low altitude aircraft with power supplied by wired electricity |
| CN102730189A (en) * | 2011-03-29 | 2012-10-17 | 郑鹏 | Marine flying lifesaving method and device |
| CN104691758A (en) * | 2015-03-01 | 2015-06-10 | 朱幕松 | Rotor wing vertical lift electric unmanned machine of linkage fixed wing |
| CN104773303A (en) * | 2015-05-04 | 2015-07-15 | 厦门大学 | Long-endurance multi-rotor-wing unmanned aerial vehicle agricultural plant protection method |
| CN105599896A (en) * | 2014-11-13 | 2016-05-25 | 师伟 | Unlimited low-cost power supply large motor carbon-free anti-air-disaster passenger and goods transportation helicopter arrangement |
| CN110654559A (en) * | 2017-10-13 | 2020-01-07 | 南京涵曦月自动化科技有限公司 | Control method of landing control device of rotor unmanned aerial vehicle |
| CN110834730A (en) * | 2019-12-11 | 2020-02-25 | 深圳市施罗德工业集团有限公司 | Umbilical cord flying device |
| CN111422071A (en) * | 2020-04-21 | 2020-07-17 | 游正广 | Novel transportation device |
-
1993
- 1993-03-12 CN CN 93102904 patent/CN1084818A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1326748C (en) * | 2002-03-26 | 2007-07-18 | 刘毅 | Low altitude aircraft with power supplied by wired electricity |
| CN102730189A (en) * | 2011-03-29 | 2012-10-17 | 郑鹏 | Marine flying lifesaving method and device |
| CN105599896A (en) * | 2014-11-13 | 2016-05-25 | 师伟 | Unlimited low-cost power supply large motor carbon-free anti-air-disaster passenger and goods transportation helicopter arrangement |
| CN104691758A (en) * | 2015-03-01 | 2015-06-10 | 朱幕松 | Rotor wing vertical lift electric unmanned machine of linkage fixed wing |
| CN104691758B (en) * | 2015-03-01 | 2016-09-28 | 朱幕松 | Linkage fixed-wing rotor electric vertical lifting unmanned plane |
| CN104773303A (en) * | 2015-05-04 | 2015-07-15 | 厦门大学 | Long-endurance multi-rotor-wing unmanned aerial vehicle agricultural plant protection method |
| CN110654559A (en) * | 2017-10-13 | 2020-01-07 | 南京涵曦月自动化科技有限公司 | Control method of landing control device of rotor unmanned aerial vehicle |
| CN110654559B (en) * | 2017-10-13 | 2021-05-28 | 南京涵曦月自动化科技有限公司 | Control method of landing control device of rotor unmanned aerial vehicle |
| CN110834730A (en) * | 2019-12-11 | 2020-02-25 | 深圳市施罗德工业集团有限公司 | Umbilical cord flying device |
| CN111422071A (en) * | 2020-04-21 | 2020-07-17 | 游正广 | Novel transportation device |
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