CN201678037U - Natural power levitation platform - Google Patents
Natural power levitation platform Download PDFInfo
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- CN201678037U CN201678037U CN2010202378002U CN201020237800U CN201678037U CN 201678037 U CN201678037 U CN 201678037U CN 2010202378002 U CN2010202378002 U CN 2010202378002U CN 201020237800 U CN201020237800 U CN 201020237800U CN 201678037 U CN201678037 U CN 201678037U
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Abstract
The utility model belongs to the field of levitation, and relates to a natural power levitation platform, which comprises an aerostat (1), a control vehicle (9) and a wind-driven generator (11). The aerostat is connected with a platform (7) through a pull rope. A natural wind power propeller (2), the wind-driven generator (11) and an ascending screw propeller (10) are installed and fixed on the platform (7). The control vehicle (9) is connected to the lower part of the platform (7); a bevel gear positioned at the upper part in a bevel gear gearbox (3) in the natural wind power propeller is connected with a rotary rod of a flower bud-shaped helical blade, and a bevel gear positioned on the sides are connected with a rotary rod of a thrust propeller (4) to dive the thrust propeller (4) to rotate through the flower bud-shaped helical blade. A rudder (5) is installed at the rear end of a fixing frame. A multi-channel remote controller is installed on the control vehicle (9), and an electric propulsion propeller (8) is installed at the rear end of the vehicle. The utility model has the advantages of energy conservation, environmental protection, conformity with low carbon and economical requirements, wide levitation range, wide application range, multiple functions, strong wing resistance, safety and reliability.
Description
Technical field
The utility model relates to the field of wafing that flies, and particularly relates to the flight device of the natural power control that utilizes the wind energy generation.
Background technology
Existing aircraft, all adopt fuel oil equal energy source power to start aircraft as various aviation aircrafts such as aircraft, dirigibles, under the more and more exhausted situation of fuel oil equal energy source, the aviation aircraft that adopts the energy to do power does not meet low-carbon economy and environmental protection requirement, and flight cost is also very high.Existing low flyer, poor as fire balloon, helium balloon etc. because of wind resistance, under the big situation of wind-force, can't go up to the air or fly, even lift-off reluctantly, air security is difficult to ensure.
Summary of the invention
Thereby the purpose of this utility model is to use fuel oil power to quicken the weak point that the future source of energy exhaustion brings at existing aircraft, propose a kind of by utilizing this natural energy resources of wind energy, while is at the problem of low flyer wind resistance difference, natural wind by aerial up current and different directions is handled, can be in the low latitude flight device of safe flight.
The technical solution of the utility model is: this natural power platform that flies to waft comprises buoyance lift device (helium balloon), handles car and aerogenerator.The buoyance lift device is connected with platform by stay cord, install, be fixed with natural wind propelling unit, aerogenerator and lift-off screw propeller on the platform, the natural wind propelling unit comprise spiral bud shape blade, bevel gear change speed gear box, thrust screw propeller and be used for controlling party to yaw rudder, platform below is connected with the manipulation car.
Being positioned at upper bevel gear in the bevel gear change speed gear box in the natural wind propelling unit is connected with the revolving bar of spiral bud shape blade, the bevel gear that is positioned at the side position is connected with the revolving bar of thrust screw propeller, yaw rudder is installed in the rear end of fixed frame, fixed frame be connected and fixed bar and be connected.
Handle on the car multi-channel remote device is installed, the rear end of car is equipped with electronic propelling screws.
When using the utility model, understand wind conditions on the same day,, promptly possessed the condition of the platform lift-off that flies to waft when wind-force during at three to six grades by weather forecast.By handling the multi-channel remote device of installing on the car, open the circuit of aerogenerator and lift-off screw propeller, electric energy by blade of wind-driven generator rotation generation, start 4 the lift-off screw propellers rotation that is positioned at four jiaos on platform, by the effect of lift-off screw propeller and buoyance lift device, drive the platform in balance lift-off.In rear end of the present utility model, the natural wind propelling unit drives the propelling screws rotation by the rotation of spiral bud shape blade, promotes the utility model and moves ahead.The direction that the utility model moves ahead is under the manipulation of multi-channel remote device, and the direction of passage rudder is realized.Simultaneously, the electric energy transmitting of aerogenerator makes its rotation to the electronic propelling screws of handling the car rear end, has increased propelling thrust of the present utility model.When the utility model descends, by handling the control of multi-channel remote device on the car, stop the rotation of aerogenerator and spiral bud shape blade, under the effect of buoyance lift device, slowly descend, until landing.
The utlity model has following remarkable result:
1, because the utility model uses nature clean energy resource one wind energy as power, meets the requirement of energy-saving and environmental protection and low-carbon economy, brought revolutionary innovation to low flyer;
2, the utility model lift-off scope is big.The lift-off height of buoyance lift device can be between 10 meters to 1000 meters.
3, 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, air rescue, the activities such as aerial sports and amusement of large-scale activities such as media advertisement, celebration in the air, also can carry out aloft work as required.
4, the utility model can carry out long-distance air transport, and load carrying ability is big, the airborne period overlength.
5, the utility model can be used for aerial scientific research or military surveillance.
6, the utility model has overcome the deficiency that common low flyer can't go up to the air, fly under the big situation of wind-force, can balance, stable lift-off under the big situation of wind-force, and aloft wind resistance is strong, and is safe and reliable.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
As shown in the figure: the electronic propelling screws 9-of 1-buoyance lift device 2-natural wind propelling unit 3-bevel gear change speed gear box 4-thrust screw propeller 5-yaw rudder 6-fixed connecting rod 7-platform 8-handles car 10-lift-off screw propeller 11-aerogenerator
The specific embodiment
The specific embodiment of the present utility model is illustrated in conjunction with the accompanying drawings: this platform that flies to waft comprises buoyance lift device (1), controls car (9) and aerogenerator (11).Buoyance lift device (1) is connected with platform (7) by stay cord, and natural wind propelling unit (2), aerogenerator (11) and lift-off screw propeller (10) are installed, are fixed with on the platform (7).Four lift-off screw propellers (10) are installed in the symmetric position that is positioned at (7) four jiaos on platform, and aerogenerator (11) is installed in the center-of-gravity position on the platform.The rotation under wind-force promotes of the blade of aerogenerator, the electric energy of generation drives lift-off screw propeller (10) rotation.Natural wind propelling unit (2) comprise spiral bud shape blade, bevel gear change speed gear box (3), thrust screw propeller (4) and be used for controlling party to yaw rudder (5), platform (7) below is connected with handles car (9).Being positioned at upper bevel gear in the bevel gear change speed gear box (3) in the natural wind pusher is connected with the revolving bar of spiral bud shape blade, the bevel gear that is positioned at the side position is connected with the revolving bar of thrust screw propeller (4), drives the rotation of thrust screw propeller (4) by spiral bud shape blade.Yaw rudder (5) is installed in the rear end of fixed frame, fixed frame be connected and fixed bar (6) and be connected.
Handle on the operation bench on the car (9) the multi-channel remote device is installed, the rear end of car is equipped with electronic propelling screws (8), and the electric energy that transmits by aerogenerator drives electronic propelling screws (8) rotation.
Claims (4)
1. natural power flies the platform that wafts, this platform that flies to waft comprises buoyance lift device (1), controls car (9) and aerogenerator (11), it is characterized in that: buoyance lift device (1) is connected with platform (7) by stay cord, natural wind propelling unit (2), aerogenerator (11) and lift-off screw propeller (10) are installed, are fixed with on the platform (7), natural wind propelling unit (2) comprise spiral bud shape blade, bevel gear change speed gear box (3), thrust screw propeller (4) and be used for controlling party to yaw rudder (5), platform (7) below is connected with handles car (9).
2. natural power according to claim 1 flies the platform that wafts, it is characterized in that being positioned in the bevel gear change speed gear box (3) in the natural wind propelling unit upper bevel gear is connected with the revolving bar of spiral bud shape blade, the bevel gear that is positioned at the side position is connected with the revolving bar of thrust screw propeller (4), yaw rudder (5) is installed in the rear end of fixed frame, fixed frame be connected and fixed bar (6) and be connected.
3. natural power according to claim 1 flies the platform that wafts, and it is characterized in that the lift-off screw propeller that can play equilibrium activity has 4, is installed in the symmetric position of (7) four jiaos on platform respectively, and aerogenerator (11) is installed in the center-of-gravity position of platform (7).
4. natural power according to claim 1 flies the platform that wafts, and it is characterized in that handling on the car (9) the multi-channel remote device is installed, and the rear end of car is equipped with electronic propelling screws (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202378002U CN201678037U (en) | 2010-06-25 | 2010-06-25 | Natural power levitation platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202378002U CN201678037U (en) | 2010-06-25 | 2010-06-25 | Natural power levitation platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201678037U true CN201678037U (en) | 2010-12-22 |
Family
ID=43343092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010202378002U Expired - Fee Related CN201678037U (en) | 2010-06-25 | 2010-06-25 | Natural power levitation platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201678037U (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102407933A (en) * | 2011-10-08 | 2012-04-11 | 西安森兰科贸有限责任公司 | Intrinsic safety type mine rescue aircraft |
| CN102582385A (en) * | 2012-04-09 | 2012-07-18 | 杨礼诚 | Breeze power generation dual-purpose dart flyer for air and ground |
| CN105227723A (en) * | 2015-11-06 | 2016-01-06 | 林丽娟 | Balloon tumbler device can be turned to |
| CN105245667A (en) * | 2015-11-06 | 2016-01-13 | 林丽娟 | Balloon tumbler device with universal ball |
| CN105292435A (en) * | 2015-11-10 | 2016-02-03 | 黄立丽 | Inclined wind-energy airship carrier device |
| CN105292430A (en) * | 2015-11-06 | 2016-02-03 | 施东德 | Steering hot-air balloon carrying body with tumbler |
| CN105292433A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Horizontal airship carrying body |
| CN105292431A (en) * | 2015-11-06 | 2016-02-03 | 唐建军 | Hot-air balloon carrying body with tumbler and universal joint |
| CN105292428A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Inclined airship carrying body |
| CN105292436A (en) * | 2015-11-10 | 2016-02-03 | 黄立丽 | Steerable wind-powered airship carrier device |
| CN105292432A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Steerable airship carrier |
| CN105292434A (en) * | 2015-11-10 | 2016-02-03 | 廖晓兰 | Solar airship device with rotating shaft |
| CN105292438A (en) * | 2015-11-10 | 2016-02-03 | 陈建红 | Horizontal wind-solar-complementary electric generation airship carrier device |
| CN105430136A (en) * | 2015-11-06 | 2016-03-23 | 林丽娟 | Balloon tumbler device with universal joint |
| CN107433046A (en) * | 2017-09-28 | 2017-12-05 | 中国特种飞行器研究所 | Travel aircraft and floating type is ridden aircraft |
| CN108640030A (en) * | 2018-07-14 | 2018-10-12 | 浙江中升建设有限公司 | A kind of high-altitude lifter and elevating method |
| CN110386257A (en) * | 2018-07-30 | 2019-10-29 | 魏荣亮 | For vertical translation aircraft warship device and naval vessel |
-
2010
- 2010-06-25 CN CN2010202378002U patent/CN201678037U/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102407933A (en) * | 2011-10-08 | 2012-04-11 | 西安森兰科贸有限责任公司 | Intrinsic safety type mine rescue aircraft |
| CN102582385A (en) * | 2012-04-09 | 2012-07-18 | 杨礼诚 | Breeze power generation dual-purpose dart flyer for air and ground |
| CN105292432A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Steerable airship carrier |
| CN105227723A (en) * | 2015-11-06 | 2016-01-06 | 林丽娟 | Balloon tumbler device can be turned to |
| CN105245667A (en) * | 2015-11-06 | 2016-01-13 | 林丽娟 | Balloon tumbler device with universal ball |
| CN105292430A (en) * | 2015-11-06 | 2016-02-03 | 施东德 | Steering hot-air balloon carrying body with tumbler |
| CN105292433A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Horizontal airship carrying body |
| CN105292431A (en) * | 2015-11-06 | 2016-02-03 | 唐建军 | Hot-air balloon carrying body with tumbler and universal joint |
| CN105292428A (en) * | 2015-11-06 | 2016-02-03 | 黄可椅 | Inclined airship carrying body |
| CN105430136A (en) * | 2015-11-06 | 2016-03-23 | 林丽娟 | Balloon tumbler device with universal joint |
| CN105292435A (en) * | 2015-11-10 | 2016-02-03 | 黄立丽 | Inclined wind-energy airship carrier device |
| CN105292434A (en) * | 2015-11-10 | 2016-02-03 | 廖晓兰 | Solar airship device with rotating shaft |
| CN105292438A (en) * | 2015-11-10 | 2016-02-03 | 陈建红 | Horizontal wind-solar-complementary electric generation airship carrier device |
| CN105292436A (en) * | 2015-11-10 | 2016-02-03 | 黄立丽 | Steerable wind-powered airship carrier device |
| CN107433046A (en) * | 2017-09-28 | 2017-12-05 | 中国特种飞行器研究所 | Travel aircraft and floating type is ridden aircraft |
| CN108640030A (en) * | 2018-07-14 | 2018-10-12 | 浙江中升建设有限公司 | A kind of high-altitude lifter and elevating method |
| CN110386257A (en) * | 2018-07-30 | 2019-10-29 | 魏荣亮 | For vertical translation aircraft warship device and naval vessel |
| CN110386257B (en) * | 2018-07-30 | 2024-06-04 | 魏荣亮 | Ship landing device for vertical lifting aircraft and ship |
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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: 20101222 Termination date: 20170625 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |