CN203681179U - Air and earth dual-purpose consubstantial gasoline helicopter - Google Patents
Air and earth dual-purpose consubstantial gasoline helicopter Download PDFInfo
- Publication number
- CN203681179U CN203681179U CN201320782568.4U CN201320782568U CN203681179U CN 203681179 U CN203681179 U CN 203681179U CN 201320782568 U CN201320782568 U CN 201320782568U CN 203681179 U CN203681179 U CN 203681179U
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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
Abstract
The utility model discloses an air and earth dual-purpose consubstantial gasoline helicopter. The air and earth dual-purpose consubstantial gasoline helicopter comprises a helicopter body, propellers, solar panels, an empennage, a lighting lamp, an instrument panel, a steering wheel, as well as a storage battery, a gearbox, a gasoline engine and wheels which are mounted at the bottom of the helicopter body; the propellers and the solar panels are mounted at the top of the helicopter body; the empennage is mounted at the tail of the helicopter body; the storage battery is connected with the solar panels; the propellers and the empennage are driven by the gasoline engine. The air and earth dual-purpose consubstantial gasoline helicopter has the superior effects that the area of the solar panels is large enough, so that clean renewable electrical energy can be provided for the helicopter; sufficient lift force can be provided for the helicopter and blades are avoided to be oversized at the same time through the design of the double propellers; the helicopter saves energy; meanwhile, the problem of traffic jam is solved effectively, so as to facilitate trip of people.
Description
Technical field
The utility model belongs to a kind of vehicle, is 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 when 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 local section, cause local traffic paralysis.
Because solar panel generally uses on locomotive, its foot can be for locomotive provides power endlessly, and as clean energy resource, have social economic value widely.But up to the present also do not have locomotive to rely on the ground solar power to provide power to travel 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 cannot solve at present the problem of charging difficulty, road congestion and the environmental pollution of existing locomotive.
Utility model content
The utility model provides a kind of world double-purpose consubstantiality gasoline helicopter, to solve existing locomotive when the road traveling, and 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 utility model is taked 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 storage battery, change speed gear box, spark ignition engine and the wheel of described organism bottom, 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 the first cell panel, the second cell panel and the 3rd cell panel are rectangle, and splice with described the first cell panel and the 3rd cell panel respectively at the two ends of described the second cell panel.
Be preferably, described solar panel comprises the first cell panel and the second cell panel, and described the first cell panel and the second cell panel are rectangle, described the first cell panel and the splicing of the second cell panel.
Be preferably, described solar panel comprises the first cell panel, and described the 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 sub warhead circle.
Adopting after technique scheme, the area of solar panel is enough large, thereby 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, in the time that road motor vehicle is less, solar panel drives world double-purpose consubstantiality gasoline helicopter at road traveling for storage battery provides electric energy, more when road motor vehicle, blocks up when serious, start spark ignition engine, spark ignition engine drives screw propeller to rotate, world double-purpose consubstantiality gasoline helicopter lift-off flight, thus can avoid congestion in road.Twin screw design, can avoid again paddle size excessive when can providing enough lift for world double-purpose consubstantiality gasoline helicopter.When world double-purpose consubstantiality gasoline helicopter is saved the energy, efficiently solve traffic jam issue, facilitated people's trip.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, to the accompanying drawing of required use in embodiment or description of the Prior Art be briefly described below, apparently, accompanying drawing in the following describes is embodiment more of the present utility model, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the first topology view of the utility model world double-purpose consubstantiality gasoline helicopter;
Fig. 2 is the second topology view of the utility model world double-purpose consubstantiality gasoline helicopter;
Fig. 3 is the topology view of the utility model solar panel embodiment 1;
Fig. 4 is the topology view of the utility model solar panel embodiment 2;
Fig. 5 is the topology view of the utility model solar panel embodiment 3.
The specific embodiment
For making object, technical scheme and the advantage of the utility model embodiment clearer, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is the utility model part embodiment, rather than whole embodiment.Based on the embodiment in the utility model, those of ordinary skills are not making all other embodiment that obtain under creative work prerequisite, all belong to the scope of the utility model protection.
As shown in Figure 1 to Figure 2, world double-purpose consubstantiality gasoline helicopter comprises body 1, be arranged on storage battery 2, change speed gear box 3, spark ignition engine 4 and the wheel 5 of body 1 bottom, 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 respectively the front and back position at body 1 top.In the process that two screw propellers 6 rotate, when providing enough lift for world double-purpose consubstantiality gasoline helicopter, can reduce the paddle size of single screw propeller 6, thereby world double-purpose consubstantiality gasoline helicopter is in the time of road traveling, avoids the blade of screw propeller 6 and other object bump and damage.Screw propeller comprises 6 blades, and the length of every 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, and storage battery 2 comprises photovoltaic electric pressure regulation charger, battery pack, for Electronmotive Force socket and change-over swith.Spark ignition engine 4 is passed to screw propeller 6 and empennage 7 by propulsive effort by change speed gear box 3.Wheel 5 is that heavier-duty inflation regulates tire, and empennage 7 is controlled 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.Be provided with air conditioning window 17 at the side of body 1, 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 turning to of controlling in the time of locomotive driving.Rear wheel 52 is drive wheel, adopts the disconnected formula tyre rim of full envelope, can play the effect of balance rudder blade in the time of flight.
As shown in Figure 3, solar panel 11 comprises the first cell panel 111, the second cell panel 112 and the 3rd cell panel 113.The first cell panel 111, the second cell panel 112 and the 3rd cell panel 113 are rectangle, splice with the first cell panel 111 and the 3rd cell panel 113 respectively at the two ends of the second cell panel 112, and the first cell panel 111, the second cell panel 112 and the 3rd cell panel 113 splicings cover the top of body 1.
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.
As shown in Figure 5, solar panel 11 comprises the top of the first cell panel 111, the first cell panels 111 whole body 1 for arc covers.
Because the front portion of body 1 is sub warhead circle, therefore world double-purpose consubstantiality gasoline helicopter is in the process of running at high speed and flying, and air resistance coefficient is little, has reduced air resistance.
The area of solar panel 11 is enough large, thereby 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 in the time that road motor vehicle is less, solar panel 11 drives world double-purpose consubstantiality gasoline helicopter at road traveling for storage battery 2 provides electric energy.More when road motor vehicle, block up when 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, and when can providing enough lift for world double-purpose consubstantiality gasoline helicopter, can avoid again paddle size excessive.When the utility model world double-purpose consubstantiality gasoline helicopter is saved the energy, efficiently solve traffic jam issue, facilitated people's trip.
Finally it should be noted that: above embodiment only illustrates the technical solution of the utility model, is not intended to limit; Although the utility model is had been described in detail with reference to previous embodiment, those of ordinary skill in the art is to be understood that: its technical scheme that still can record aforementioned each embodiment is modified, or part technical characterictic is wherein equal to replacement; And these modifications or replacement do not make the essence of appropriate technical solution depart from the spirit and scope of the each embodiment technical scheme of the utility model.
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 storage battery, change speed gear box, spark ignition engine and the wheel of described organism bottom, 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, is characterized in that, described screw propeller has two.
3. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, 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, is characterized in that, described the first cell panel, the second cell panel and the 3rd cell panel are rectangle, and splice with described the first cell panel and the 3rd cell panel respectively at the two ends of described the second cell panel.
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 the first cell panel and the second cell panel are rectangle, described the first cell panel and the splicing of the second cell panel.
6. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, is characterized in that, described solar panel comprises the first cell panel, and described the first cell panel is arc.
7. the world according to claim 1 double-purpose consubstantiality gasoline helicopter, 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, 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 sub warhead circle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320782568.4U CN203681179U (en) | 2013-11-29 | 2013-11-29 | Air and earth dual-purpose consubstantial gasoline helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320782568.4U CN203681179U (en) | 2013-11-29 | 2013-11-29 | Air and earth dual-purpose consubstantial gasoline helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203681179U true CN203681179U (en) | 2014-07-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320782568.4U Expired - Fee Related CN203681179U (en) | 2013-11-29 | 2013-11-29 | Air and earth dual-purpose consubstantial gasoline helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203681179U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104589937A (en) * | 2013-11-29 | 2015-05-06 | 仇文江 | Gasoline helicopter used both in air and on ground and provided with same helicopter body |
-
2013
- 2013-11-29 CN CN201320782568.4U patent/CN203681179U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104589937A (en) * | 2013-11-29 | 2015-05-06 | 仇文江 | Gasoline helicopter used both in air and on ground and provided with same helicopter body |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140702 Termination date: 20141129 |
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| EXPY | Termination of patent right or utility model |