CN2128616Y - Electric helicopter - Google Patents
Electric helicopter Download PDFInfo
- Publication number
- CN2128616Y CN2128616Y CN 92216373 CN92216373U CN2128616Y CN 2128616 Y CN2128616 Y CN 2128616Y CN 92216373 CN92216373 CN 92216373 CN 92216373 U CN92216373 U CN 92216373U CN 2128616 Y CN2128616 Y CN 2128616Y
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- Prior art keywords
- electrical motor
- helicopter
- electric power
- cable
- power
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides an electric helicopter, which is applicable to a people-and-article-carrying tool which can vertically ascend into the sky in the flying moving mode or the fixing mode. An electric motor, which is led in through the incidental electric cable ropes and is powered by the electric source supplied from the land, is installed in the body as a prime mover, which drives the rotary wings rotate to ascend into the sky, advance, back and turn. The electric helicopter is suitable for a plurality of purposes, such as tour sightseeing, artificial raining, deinsectization, hail prevention, bridge and cable putting-up, weather air sounding, fire warning reconnaissance, advertisement propaganda, construction illumination, high-altitude aerial photography, mountaineering expedition, etc., and is particular suitable for being used in the areas of complicated terrain, inconvenient traffic and need to transport people and articles frequently and periodically.
Description
The utility model relates to a kind of the rotation as primary mover drive rotor with electrical motor can vertically rise up into the facility that are used in flight movable type and the manned loading of fixed type in the air, be suitable for going sightseeing, explored or the like in the field in rainmaking, deinsectization hail suppression, bridge formation stringing, meteorological sounding, fire alarm scouting, advertising, construction illumination, high-altitude photo and mountain-climbing, be particularly suitable for a varied topography, traffic extremely the area of inconvenience as transportation means.
In the prior art, go straight up to facility and be mainly that it can do short-range manned loading flight as the autogyro of primary mover with turbine engine, it can rise up into aerial stop operation to also have hydrogen balloon, fire balloon, airship etc. in addition, also can utilize wind-force or it on entrained compact spiral starch the flight that driving engine is made certain distance.But they exist some shortcomings that are difficult to overcome simultaneously; Autogyro must also need carry the fuel oil that is used by very big piston reciprocating internal combustion engine or the gas turbine engine of the complicated weight of mounting structure, therefore very big effective weight and the volume that seriously influences and limited manned loading of own wt, expenditure of energy is big, make relatively difficulty, noise is higher and lift-off landing such as hydrogen balloon, fire balloon, airship all trouble bothersome, handle the skyborne position of control difficulty, also the generation balloon burns, is blown away by strong wind accidents such as drift easily.Therefore need to develop and seek the go straight up to facility of the lighter power machine of a kind of use reliable weight simple in structure as can fly on demand mobile or fixed manned loading.
The electrical motor that the purpose of this utility model provides a kind of power supply that is equipped with land supply in body be power drives the facility that the rotor rotation can vertically be gone up to the air and is used in portable or the fixed manned or loading of flight as required respectively as primary mover.
It is to be applicable to vertically to rise up into the portable and fixed facility in order to manned loading of aerial conduct flight that the utility model provides a kind of electric power helicopter, it is to be equipped with driving device by the top to connect the rotor that drives, the bottom is provided with the body that alighting gear, tail end be provided with antitorque propeller and empennage and forms, the driving device that it is characterized in that described drive rotor connects transmission by electrical motor, and the power supply of its electrical motor is to be imported by the cable rope that ground electrical network is connected on the electric power helicopter.Its described electrical motor its electrical motor ［ 6 ］ when on the portable electric power helicopter that is used to fly is to be installed in the body ［ 4 ］ and by the navigating mate of taking in body ［ 4 ］ to handle control, the power take-off of electrical motor ［ 6 ］ is connected on the driving device ［ 5 ］ that can change the elevation angle angle of adjusting the rotor ［ 7 ］ on body ［ 4 ］ top and rotating speed, the power supply of electrical motor ［ 6 ］ is to connect through being contained in the cable rope ［ 10 ］ on the automatic winch ［ 9 ］ in the body ［ 4 ］ to import, and cable rope ［ 10 ］ is to be connected on the motion circuit closer ［ 11 ］ that slides on power transmission network ［ 2 ］ circuit of being derived by ground power station ［ 1 ］.Its described electrical motor is on being used for fixing the formula electric power helicopter time, its electrical motor ［ 14 ］ is to be installed in the body ［ 15 ］, can handle control by the personnel that wherein take, also can handle control by ground staff, the power take-off of electrical motor ［ 14 ］ is connected to and can changes on the driving device ［ 13 ］ of adjusting rotor ［ 12 ］ rotating speed on body ［ 15 ］ top, the power supply of electrical motor ［ 14 ］ be through being contained in the body ［ 15 ］ or ground automatic winch ［ 21 ］ on cable rope ［ 18 ］ and connecting import, cable rope ［ 18 ］ is to connect on hard-wired on the ground power supply and the control setup ［ 19 ］.The cable rope ［ 18 ］ that uses in cable rope ［ 10 ］ in the portable electric power helicopter of its described flight and the described stationary electric power helicopter is respectively by power lead, loop line and reinforcement cable combine, and its length of strengthening cable can be equal to or slightly be shorter than power lead and return cable set.
The utility model compared with prior art, because the power supply of the land supply of employing is the primary mover of helicopter as the electrical motor of power, total weight than existing gas turbine engine fuel case sum is light, has increased the useful weight and the space of manned loading.But the electric motor structure simple-to-maintain easily, use reliable, be convenient to that speed governing, control comfort, noise are slight, it also a plurality of electrical motors of varying in size of installation power to do lift-off, advance and to turn to very convenient practicality.Though it need be built ground-surface supply station and set up electrical network, for have certain manned loading transportation volume and must be continuously frequently and the section that transports of cycle to drop into certain fund in the early stage still be economical.And it need not take the influence that valuable land area is not subjected to any high-lager building and chain of mountains river valley on the ground yet, and its investment construction expense is not too large, can also solve periodic continuous transport over a long time.For at the both urban and rural area of original existing land power supply supply as advertising, the construction illumination, to watch the stationary electric power helicopter that fire alarm, meteorological sounding be provided with then particularly easy, also is convenient to using with dress, need not tearing the easy province's expense that saves time open with regard to demolition, installation.
Accompanying drawing:
Fig. 1, the total assembly drawing of electric power helicopter (flight is portable).
Fig. 2, the total assembly drawing of electric power helicopter (fixed type):
Parts title in the figure:
1, power station 2, power transmission network 3, alighting gear 4, body 5, driving device 6, electrical motor 7, rotor 8, antitorque propeller 9, automatic winch 10, cable rope 11, motion circuit closer 12, rotor 13, driving device 14, electrical motor 15, body 16, alighting gear 17, suspension 18, cable rope 19, power supply and control setup 20, empennage 21, automatic winch
Embodiment: accompanying drawing 1,2 is respectively total assembly drawing of flight movable type and stationary electric power helicopter, and it belongs to two kinds of schemes of same design.Its structure is basic identical, is contained in the electrical network supply of the power supply of the electrical motor (the electric power helicopter body is not cut open, fails in the figure to represent) in the body by the power station derivation of land.The portable electric power helicopter that flies is provided with except that its primary mover changes the cable bands place of entering that electrical motor and power supply introduce into by gas turbine engine that all the other all can be same as existing autogyro the automatic winch, is prior art.Also can utilize existing autogyro to be reequiped when its driving engine exceeds the time limit to continue to use must to change in the time of can't flying.Rotor ［ 7 ］ on body ［ 4 ］ top is changed by bonded assembly driving device ［ 5 ］ on electrical motor ［ 6 ］ power take-off adjusts the angle of attack, so that go up to the air, advance, retreat or stop.Alighting gear wherein ［ 3 ］ for two slide plates, rise and fall wheel to or be applicable to hull waterborne.Antitorque propeller ［ 8 ］ is the device of balance rotor ［ 7 ］ torsion.Automatic winch ［ 9 ］ is can self-jacked winch according to the length of lift-off or when landing helicopter actual needs cable rope ［ 10 ］.Cable rope ［ 10 ］ then is power supply lead-in wire and loop line group and the combination cable of strengthening cable, and reinforcement cable wherein also can be arranged on separately beyond the cable group, but the length of cable set need slightly be lacked or should be equal to its length when the longest, in order to avoid cable set is broken.Motion circuit closer ［ 11 ］ is connected on the electrical network ［ 2 ］ for installation, and it not only can smoothly successfully slide mobile or adopt the small-sized electric car rolling to advance but also can not pulled off by the mobile helicopter that advances of flight and deviate to cause the degeneration accident of cutting off the power supply.Stationary electric power helicopter structure is then simpler, and whether the electrical motor ［ 14 ］ that is loaded on body ［ 15 ］ is then decided according to the needs and the purposes of this electric power helicopter by the navigating mate or the manipulation of staff on the ground that ride in the body ［ 15 ］; Take pictures, photograph, scout, watch from a height or a distance etc. as needs and then can grasp voluntarily by passenger, as only observing and watch from a height or a distance, hang exploitation poster (shown in accompanying drawing 2 piece numbers 17) for construction site built in light, the rotation of installation pick up camera, meteorological soundings etc. then can be handled by the surface work personnel and get final product, its mounting or dismounting displacement is more convenient laborsaving, and the stationary electric power helicopter also can be removed the structure that empennage ［ 20 ］ is installed from.
Claims (4)
1, a kind of electric power helicopter is to be applicable to vertically to rise up into the portable and fixed facility in order to manned loading of aerial conduct flight, it is to be equipped with driving device by the top to connect the rotor that drives, the bottom is provided with the body that alighting gear, tail end be provided with antitorque propeller and empennage and forms, the device that it is characterized in that the transmission of described drive rotor connects transmission by electrical motor, and the power supply of its electrical motor is to be imported by the cable rope that ground electrical network is connected on the electric power helicopter.
2, electric power helicopter according to claim 1, it is characterized in that described electrical motor its electrical motor ［ 6 ］ when on the portable electric power helicopter that is used to fly is to be installed in the body ［ 4 ］ and by the navigating mate of taking to handle control in body ［ 4 ］, the power take-off of electrical motor ［ 6 ］ is connected on the driving device ［ 5 ］ that can change the elevation angle angle of adjusting the rotor ［ 7 ］ on body ［ 4 ］ top and rotating speed, the power supply of electrical motor ［ 6 ］ is to connect through being contained in the cable rope ［ 10 ］ on the automatic winch ［ 9 ］ in the body ［ 4 ］ to import, and cable rope ［ 10 ］ is to be connected on the motion circuit closer ［ 11 ］ that slides on power transmission network ［ 2 ］ circuit of being derived by ground power station ［ 1 ］.
3, electric power helicopter according to claim 1, when it is characterized in that described electrical motor is on being used for fixing the formula electric power helicopter, its electrical motor ［ 14 ］ is to be installed in the body ［ 15 ］, can handle control by the personnel that wherein take, also can handle control by ground staff, the power take-off of electrical motor ［ 14 ］ is connected to and can changes on the driving device ［ 13 ］ of adjusting rotor ［ 12 ］ rotating speed on body ［ 15 ］ top, the power supply of electrical motor ［ 14 ］ be through being contained in the body ［ 15 ］ or ground automatic winch ［ 21 ］ on cable rope ［ 18 ］ and connecting import, cable rope ［ 18 ］ is to connect on hard-wired on the ground power supply and the control setup ［ 19 ］.
4, according to claim 2,3 described electric power helicopters, the cable rope ［ 18 ］ that it is characterized in that using in cable rope ［ 10 ］ and the described stationary electric power helicopter in the portable electric power helicopter of described flight is respectively by power lead, loop line and reinforcement cable combine, and its length of strengthening cable can be equal to or slightly be shorter than power lead and return cable set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 92216373 CN2128616Y (en) | 1992-06-29 | 1992-06-29 | Electric helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 92216373 CN2128616Y (en) | 1992-06-29 | 1992-06-29 | Electric helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2128616Y true CN2128616Y (en) | 1993-03-24 |
Family
ID=33764511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 92216373 Expired - Fee Related CN2128616Y (en) | 1992-06-29 | 1992-06-29 | Electric helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2128616Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008113220A1 (en) * | 2007-03-22 | 2008-09-25 | Yuejun Yan | Cable-feeding suspended information transceive system |
| 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 |
-
1992
- 1992-06-29 CN CN 92216373 patent/CN2128616Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008113220A1 (en) * | 2007-03-22 | 2008-09-25 | Yuejun Yan | Cable-feeding suspended information transceive system |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |