CN104589937A - Gasoline helicopter used both in air and on ground and provided with same helicopter body - Google Patents
Gasoline helicopter used both in air and on ground and provided with same helicopter body Download PDFInfo
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- CN104589937A CN104589937A CN201310631892.0A CN201310631892A CN104589937A CN 104589937 A CN104589937 A CN 104589937A CN 201310631892 A CN201310631892 A CN 201310631892A CN 104589937 A CN104589937 A CN 104589937A
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- helicopter
- gasoline
- cell panel
- consubstantiality
- double
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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Abstract
The invention discloses a gasoline helicopter used both in air and on the ground and provided with the same helicopter body. The gasoline helicopter used both in air and on the ground and provided with the same helicopter body comprises the helicopter body, propellers, solar cell panels, an empennage, an illumination lamp, an instrument panel, a steering wheel, a storage battery, a gearbox, a gasoline engine and wheels, wherein the storage battery, the gearbox, the gasoline engine and the wheels are installed at the bottom of the helicopter body, the propellers and the solar cell panels are installed on the top of the helicopter body, the empennage is installed at the tail of the helicopter body, the storage battery is connected with the solar cell panels, and the gasoline engine drives the propellers and the empennage. The gasoline helicopter used both in air and on the ground and provided with the same helicopter body has the advantages that the area of the solar cell panels is large enough, so clean and renewable electric energy can be provided for the gasoline helicopter used both in air and on the ground and provided with the same helicopter body. The two propellers are designed, so enough lift force can be provided for the gasoline helicopter used both in air and on the ground and provided with the same helicopter body, and meanwhile the situation that the size of paddles is overlarge can be avoided. The gasoline helicopter used both in air and on the ground and provided with the same helicopter body saves energy resources, effectively solves the problem of traffic congestion and facilitates travelling by people.
Description
Technical field
The invention belongs to a kind of vehicle, be specifically related to a kind of world double-purpose consubstantiality gasoline helicopter.
Background technology
Along with developing rapidly of national economy, the automobile pollution of China is constantly broken a record, and almost each large and medium-sized city exists traffic jam now.At present, sooner or later during peak on and off duty, from the unidirectional traffic congestion of traffic, progressively become the phenomenon of the two-way traffic congestion of traffic, all block to section, local, cause local traffic to paralyse.
Because solar panel generally uses on locomotive, its foot can provide power endlessly for locomotive, and as clean energy resource, has social economic value widely.But up to the present also do not have locomotive to rely on solar power to provide power to travel on the ground completely, and rely on spark ignition engine to drive the world double-purpose consubstantiality gasoline motor car that flies on high of screw propeller, and the charging that cannot solve existing locomotive is at present difficult, the problem of road congestion and environmental pollution.
Summary of the invention
The invention provides a kind of world double-purpose consubstantiality gasoline helicopter, to solve existing locomotive when road traveling, road congestion, the technical matters that environmental pollution is serious and charging is inconvenient.
In order to solve above technical matters, the technical scheme that the present invention takes is:
A kind of world double-purpose consubstantiality gasoline helicopter, described world double-purpose consubstantiality gasoline helicopter comprises body, screw propeller, solar panel, empennage, illuminating lamp, gauge panel and bearing circle, and be arranged on the storage battery of described organism bottom, change speed gear box, spark ignition engine and wheel, described screw propeller and solar panel are arranged on the top of described body, described empennage is arranged on the afterbody of described body, described storage battery is connected with described solar panel, and described spark ignition engine drives described screw propeller and empennage.
Be preferably, described screw propeller has two.
Be preferably, described solar panel comprises the first cell panel, the second cell panel and the 3rd cell panel.
Be preferably, described first cell panel, the second cell panel and the 3rd cell panel are rectangle, and the two ends of described second cell panel are spliced with described first cell panel and the 3rd cell panel respectively.
Be preferably, described solar panel comprises the first cell panel and the second cell panel, and described first cell panel and the second cell panel are rectangle, described first cell panel and the splicing of the second cell panel.
Be preferably, described solar panel comprises the first cell panel, and described first cell panel is arc.
Be preferably, described helicopter is built-in with five arrange seatses, and described five arrange seatses comprise row's single seat and four row's two-seaters.
Be preferably, described screw propeller comprises 6 blades, and the length of described blade is 1.6 meters to 2.5 meters.
Be preferably, described storage battery comprises photovoltaic electric pressure regulation charger, battery pack, supplies Electronmotive Force socket and change-over swith.
Be preferably, the front portion of described body is that sub warhead is circular.
After employing technique scheme, the area of solar panel is enough large, thus can provide clean reproducible electric energy for world double-purpose consubstantiality gasoline helicopter.World double-purpose consubstantiality gasoline helicopter can either travel on the ground, can fly in the sky again, when road motor vehicle is less, solar panel provides electrical energy drive world double-purpose consubstantiality gasoline helicopter at road traveling, when road motor vehicle is more, when blocking up serious for storage battery, start spark ignition engine, spark ignition engine drives propeller rotational, world double-purpose consubstantiality gasoline helicopter lift-off flight, thus can avoid congestion in road.Twin screw design, can for world double-purpose consubstantiality gasoline helicopter enough lift is provided while paddle size can be avoided again excessive.While the double-purpose consubstantiality gasoline helicopter economize energy of the world, efficiently solve traffic jam issue, facilitate people's trip.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the first topology view of the world of the present invention double-purpose consubstantiality gasoline helicopter;
Fig. 2 is the second topology view of the world of the present invention double-purpose consubstantiality gasoline helicopter;
Fig. 3 is the topology view of solar panel embodiment 1 of the present invention;
Fig. 4 is the topology view of solar panel embodiment 2 of the present invention;
Fig. 5 is the topology view of solar panel embodiment 3 of the present invention.
Detailed description of the invention
For making the object of the embodiment of the present invention, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
As shown in Figure 1 to Figure 2, world double-purpose consubstantiality gasoline helicopter comprises body 1, be arranged on the storage battery 2 bottom body 1, change speed gear box 3, spark ignition engine 4 and wheel 5, wherein the front portion of body 1 is provided with illuminating lamp 8, gauge panel 9 and bearing circle 10, the top of body 1 is provided with screw propeller 6 and solar panel 11, and the rear portion of body 1 is provided with empennage 7.Screw propeller 6 has two, and two screw propellers 6 are arranged on the front and back position at body 1 top respectively.In the process of two screw propeller 6 rotations, while world double-purpose consubstantiality gasoline helicopter provides enough lift, can reduce the paddle size of single screw propeller 6, thus world double-purpose consubstantiality gasoline helicopter is when road traveling, avoids the blade of screw propeller 6 and other object collide and damage.Screw propeller comprises 6 blades, and the length of often propping up blade is 1.6 meters to 2.5 meters.Storage battery 2 is connected by electric wire with solar panel 11, and solar panel 11 provides electric energy endlessly for storage battery 2, storage battery 2 comprise photovoltaic electric pressure regulation charger, battery pack, for Electronmotive Force socket and change-over swith.Propulsive effort is passed to screw propeller 6 and empennage 7 by change speed gear box 3 by spark ignition engine 4.Wheel 5 is that heavier-duty inflation regulates tire, and empennage 7 controls the heading of world double-purpose consubstantiality gasoline helicopter, and screw propeller 6 provides lift for world double-purpose consubstantiality gasoline helicopter.Built-in 5 arrange seatses of world double-purpose consubstantiality gasoline helicopter: row's single seat and four row's two-seaters, wherein first row seat 12 is single seat operator's saddle, and second row seat 13, the 3rd arrange seats 14, the 4th arrange seats 15 and the 5th arrange seats 16 are Double-seat.The side of body 1 is provided with air conditioning window 17, and air conditioning window 17 is positioned at the lateral location of the 5th arrange seats 16.Wheel 5 comprises front vehicle wheel 51 and rear wheel 52, and wherein front vehicle wheel 51 and rear wheel 52 respectively have two, and two front vehicle wheels 51 and two rear wheels 52 are distributed in the left and right sides of body 1.Front vehicle wheel 51 and rear wheel 52 provide driven by power world double-purpose consubstantiality gasoline helicopter at ground run by storage battery 2, and front vehicle wheel 51 adopts the steel ring of the disconnected formula tire of full envelope, play the effect controlling to turn to when locomotive driving.Rear wheel 52 is drive wheel, adopting the disconnected formula tyre rim of full envelope, can play the effect of balance rudder blade when flying.
Embodiment 1
As shown in Figure 3, solar panel 11 comprises the first cell panel 111, second cell panel 112 and the 3rd cell panel 113.First cell panel 111, second cell panel 112 and the 3rd cell panel 113 are rectangle, the two ends of the second cell panel 112 are spliced with the first cell panel 111 and the 3rd cell panel 113 respectively, and the first cell panel 111, second cell panel 112 and the splicing of the 3rd cell panel 113 cover the top of body 1.
Embodiment 2
As shown in Figure 4, solar panel 11 comprises the first cell panel 111 and the second cell panel 112, and wherein the first cell panel 111 and the second cell panel 112 are rectangle, and the first cell panel 111 and the second cell panel 112 splice and cover the top of body 1.
Embodiment 3
As shown in Figure 5, solar panel 11 comprises the top of the first cell panel 111, first cell panel 111 whole body 1 for arc covers.
Front portion due to body 1 is that sub warhead is circular, and therefore world double-purpose consubstantiality gasoline helicopter is in the process of running at high speed and flying, and air resistance coefficient is little, reduces air resistance.
The area of solar panel 11 is enough large, thus can provide clean reproducible electric energy for world double-purpose consubstantiality gasoline helicopter.World double-purpose consubstantiality gasoline helicopter can either travel on the ground, can fly in the sky again, and when road motor vehicle is less, solar panel 11 provides electrical energy drive world double-purpose consubstantiality gasoline helicopter at road traveling for storage battery 2.When road motor vehicle is more, when blocking up serious, start spark ignition engine 4, spark ignition engine 4 drives screw propeller 6 to rotate, world double-purpose consubstantiality gasoline helicopter lift-off flight, thus can avoid congestion in road.Twin screw 6 designs, can for world double-purpose consubstantiality gasoline helicopter enough lift is provided while paddle size can be avoided again excessive.While the double-purpose consubstantiality gasoline helicopter economize energy of the world of the present invention, efficiently solve traffic jam issue, facilitate people's trip.
Last it is noted that above embodiment only illustrates technical scheme of the present invention, be not intended to limit; Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (10)
1. a world double-purpose consubstantiality gasoline helicopter, it is characterized in that, described world double-purpose consubstantiality gasoline helicopter comprises body, screw propeller, solar panel, empennage, illuminating lamp, gauge panel and bearing circle, and be arranged on the storage battery of described organism bottom, change speed gear box, spark ignition engine and wheel, described screw propeller and solar panel are arranged on the top of described body, described empennage is arranged on the afterbody of described body, described storage battery is connected with described solar panel, and described spark ignition engine drives described screw propeller and empennage.
2. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described screw propeller has two.
3. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described solar panel comprises the first cell panel, the second cell panel and the 3rd cell panel.
4. the world according to claim 3 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described first cell panel, the second cell panel and the 3rd cell panel are rectangle, and the two ends of described second cell panel are spliced with described first cell panel and the 3rd cell panel respectively.
5. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described solar panel comprises the first cell panel and the second cell panel, and described first cell panel and the second cell panel are rectangle, described first cell panel and the splicing of the second cell panel.
6. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described solar panel comprises the first cell panel, and described first cell panel is arc.
7. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described helicopter is built-in with five arrange seatses, and described five arrange seatses comprise row's single seat and four row's two-seaters.
8. the world according to claim 2 double-purpose consubstantiality gasoline helicopter, it is characterized in that, described screw propeller comprises 6 blades, and the length of described blade is 1.6 meters to 2.5 meters.
9. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, is characterized in that, described storage battery comprises photovoltaic electric pressure regulation charger, battery pack, supplies Electronmotive Force socket and change-over swith.
10. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, is characterized in that, the front portion of described body is that sub warhead is circular.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310631892.0A CN104589937A (en) | 2013-11-29 | 2013-11-29 | Gasoline helicopter used both in air and on ground and provided with same helicopter body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310631892.0A CN104589937A (en) | 2013-11-29 | 2013-11-29 | Gasoline helicopter used both in air and on ground and provided with same helicopter body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104589937A true CN104589937A (en) | 2015-05-06 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310631892.0A Pending CN104589937A (en) | 2013-11-29 | 2013-11-29 | Gasoline helicopter used both in air and on ground and provided with same helicopter body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104589937A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539038A (en) * | 2016-01-06 | 2016-05-04 | 潘祖国 | Air-land dual-purpose solar emergency ambulance |
| CN109878281A (en) * | 2019-03-07 | 2019-06-14 | 浙江叶尼塞电气有限公司 | A kind of sea, land and air one hydrogen fuel new-energy automobile |
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| CN201559493U (en) * | 2009-11-23 | 2010-08-25 | 武岚 | Solar air-land sightseeing bus |
| CN201639320U (en) * | 2010-01-18 | 2010-11-17 | 上海东裕电动车有限公司 | Electric vehicle and solar charging device thereof |
| GB2479206A (en) * | 2010-04-01 | 2011-10-05 | Philip Michael Pauley | A land vehicle for use with a water or air transportation vehicle |
| CN102616095A (en) * | 2012-03-26 | 2012-08-01 | 史智勇 | Vertical lifting aerocar with ring-shaped rotor wings |
| CN202593200U (en) * | 2012-01-13 | 2012-12-12 | 唐山 | Vehicle, boat and airplane three-in-one device |
| CN203134929U (en) * | 2013-03-28 | 2013-08-14 | 长安大学 | Protector for batteries of electric vehicle under low temperature environment |
| JP2013154879A (en) * | 2013-03-06 | 2013-08-15 | Jin Nakajo | Coalesced aero-land carrier of automobile, stern of airplane and helicopter |
| CN203681179U (en) * | 2013-11-29 | 2014-07-02 | 仇文江 | Air and earth dual-purpose consubstantial gasoline helicopter |
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2013
- 2013-11-29 CN CN201310631892.0A patent/CN104589937A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201390114Y (en) * | 2009-03-06 | 2010-01-27 | 刘国斌 | Triphibian hybrid vehicle |
| CN201357728Y (en) * | 2009-03-12 | 2009-12-09 | 杨克成 | Flying automobile |
| CN201559493U (en) * | 2009-11-23 | 2010-08-25 | 武岚 | Solar air-land sightseeing bus |
| CN201639320U (en) * | 2010-01-18 | 2010-11-17 | 上海东裕电动车有限公司 | Electric vehicle and solar charging device thereof |
| GB2479206A (en) * | 2010-04-01 | 2011-10-05 | Philip Michael Pauley | A land vehicle for use with a water or air transportation vehicle |
| CN202593200U (en) * | 2012-01-13 | 2012-12-12 | 唐山 | Vehicle, boat and airplane three-in-one device |
| CN102616095A (en) * | 2012-03-26 | 2012-08-01 | 史智勇 | Vertical lifting aerocar with ring-shaped rotor wings |
| JP2013154879A (en) * | 2013-03-06 | 2013-08-15 | Jin Nakajo | Coalesced aero-land carrier of automobile, stern of airplane and helicopter |
| CN203134929U (en) * | 2013-03-28 | 2013-08-14 | 长安大学 | Protector for batteries of electric vehicle under low temperature environment |
| CN203681179U (en) * | 2013-11-29 | 2014-07-02 | 仇文江 | Air and earth dual-purpose consubstantial gasoline helicopter |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539038A (en) * | 2016-01-06 | 2016-05-04 | 潘祖国 | Air-land dual-purpose solar emergency ambulance |
| CN109878281A (en) * | 2019-03-07 | 2019-06-14 | 浙江叶尼塞电气有限公司 | A kind of sea, land and air one hydrogen fuel new-energy automobile |
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| C06 | Publication | ||
| PB01 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150506 |