CN202557242U - Breeze generation airphibious flying aircraft - Google Patents
Breeze generation airphibious flying aircraft Download PDFInfo
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- CN202557242U CN202557242U CN2012201432634U CN201220143263U CN202557242U CN 202557242 U CN202557242 U CN 202557242U CN 2012201432634 U CN2012201432634 U CN 2012201432634U CN 201220143263 U CN201220143263 U CN 201220143263U CN 202557242 U CN202557242 U CN 202557242U
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- wind energy
- bearing
- storage tank
- sail
- bent axle
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Abstract
The utility model discloses a breeze generation airphibious flying aircraft and relates to the field of low-altitude aircrafts. The breeze generation airphibious flying aircraft comprises an aerostat, an automobile, a wind energy absorber and a wind energy converter; the wind energy absorber comprises windmills, sails, a bearing and a bearing fixing frame; the wind energy converter comprises a wind energy converting box, a crankshaft, a connection rod and a piston; a gas storage tank is installed on the wind energy converting box in a supporting mode, the wind energy absorber is fixedly installed on one side of the gas storage tank through the bearing fixing frame, and a rotor generator is installed below the bearing through the bearing fixing frame; a bearing rotation shaft is connected with the crankshaft, and the crankshaft is connected with the piston through the connection rod; and the wind energy converting box is communicated with the gas storage tank through a gas inlet, the gas storage tank is connected with the aerostat through a connection rope, and a power-driven lift-off propeller is installed at the bottom of the aerostat. According to the breeze generation airphibious flying aircraft, wind energy is used as power of the flying aircraft, the idea is revolutionary innovation, and the flying aircraft is low-carbon and environment-friendly.
Description
Technical field
The utility model relates to the aircraft field, particularly relates to the low flyer field of the natural power control that utilizes the wind energy generation.
Background technology
Existing aircraft adopts fuel oil equal energy source power to come start the engine usually, and under the more and more exhausted situation of fuel oil equal energy source, the aircraft that adopts the energy to do power does not meet low-carbon economy and environmental protection requirement, and operating cost is also very high.Though be the requirement that the non-fuel oil aircraft of power meets the energy-conserving and environment-protective low-carbon economy with the fire balloon, the fire balloon flying speed is slow, carrying capacity is little, can not satisfy the fast and big requirement of carrying capacity of people's running velocity.Utilizing natural wind energy to generate electricity does not also have the report of this respect at present as the aircraft that continues the energy.
Summary of the invention
The purpose of the utility model is the weak point to existing flight device; Propose a kind ofly, flight device just can be gone up to the air and can be in the environment of gentle breeze with natural wind generating flight device as the continuous running energy through utilizing this natural energy resources of wind energy.
The technical scheme of the utility model is: this flight device comprises buoyance lift device, automobile and sail, it is characterized in that: load on the automobile and settle wind energy absorber and wind energy converter.Wind energy absorber comprises windmill, sail and bearing and fixed mount.Wind energy converter comprises wind energy transfer trunk, bent axle, connecting rod and piston.Support on the wind energy transfer trunk storage tank is installed; One side of storage tank is installed with bearing through the bearing fixing frame; The bearing top is equipped with bearing carrier ring, on the position of symmetry the sail frame is installed around the bearing carrier ring, and the below of bearing is equipped with rotor generator through the bearing fixing frame.On the sail frame sail is installed, the front end of sail frame is equipped with windmill, and bearing cone is equipped with turning cylinder in the hole; Turning cylinder is connected with bent axle; The lower end of bent axle is sleeved in the axle sleeve, and bent axle is connected with the wind energy transfer trunk with strut bar through axle sleeve, and the recessed axle of bent axle is connected with the connecting rod in the wind energy transfer trunk; Connecting rod is connected with piston; The wind energy transfer trunk is connected with storage tank through admission port, and the car body rear side of automobile is installed the storage battery that reserve power is used, and storage tank is connected with the buoyance lift device through connection cord.Storage tank and wind energy transfer trunk, between wind energy transfer trunk and the automobile, there all have the strut bar of connection to be fixing.The bottom of buoyance lift device is equipped with the electric lift-up screw propeller.
When using the utility model, in place breezy, under wind effect, windmill rotates and drives the sail rotation, drives the wind energy absorber unitary rotation with automobile parking in elder generation.The bearing of wind energy absorber drives turning cylinder and rotates together, and turning cylinder is in rotation process, and the rotor generator generating is stored in electric energy in the storage battery through power transmission line.Raise after the buoyance lift device is full of gas, the electric lift-up screw propeller rotates, and drives the utility model miscellaneous part in company with the buoyance lift device and goes up to the air thereupon.After the lift-off, the rotation of the bearing inner ring of wind energy absorber drives bent axle and rotates thereupon when turning cylinder rotates; Make the piston in the wind energy transfer trunk move back and forth; Air through the reciprocating motion of the pistons inspiration is transported to storage tank through admission port, and when the air pressure in the storage tank reached certain pressure, the air nozzle air valve of storage tank afterbody was opened automatically; Outwards go out than air flow, promote the utility model as jet plane and fly fast.When arriving predetermined place, through remote controller the electric lift-up screw propeller is stopped operating, the utility model descends slowly this moment; Close wind energy absorber simultaneously, sail stops operating, and the air nozzle air valve SELF CL of storage tank afterbody makes the utility model drop to assigned address.When the utility model need not go up to the air, also can go as the common electrical motor-car in the land.
The utlity model has following remarkable result:
1, the utility model uses nature clean energy resource-wind energy as the lasting generating that flies to waft, lift-off operation power, meets the requirement of energy-saving and environmental protection and low-carbon economy, has brought revolutionary innovation for the low latitude flight device;
2, the utility model makes wind energy convert high pressure gas into through wind energy absorber and wind energy converter, sprays continuously through the storage tank air nozzle, promotes the utility model and moves ahead, and compares with existing low flyer, has improved flying speed greatly;
3, the utility model is less demanding to wind environment, because the utility model has windmill, sail structure, wind-force promptly just can satisfy generating, inflation requirement at gentle breeze between the 2-3 level wind;
4, but the utility model vacant lot is dual-purpose, is not using under the buoyance lift device situation, can be used as electronlmobil and uses.
Brief Description Of Drawings
Fig. 1 is the structural representation of the utility model.
Fig. 2 the utility model Fig. 1 sail, windmill A are to structural representation.
As shown in the figure: 1- buoyance lift device 2- is connected and fixed rope 3- air accumulator 4- puff prot 5- air valve 6- inflation inlet 7- valve 8 piston 9- sealing gasket 10- and connects bracing frame 11- storage battery 12- wind energy cross box 13- connecting rod 14 connection bracing frame 15- automobile 16- Connection Bracket 17- axle sleeve 18- valve 19- rotating shaft 20- bearing fixing frame 21- bearing 22- windmill 23- wind axle 24- bearing inner race cover 25- sail frame 26- sail 27- bent axle 28- rotor generator 29- electric lift-up screws
The specific embodiment
The specific embodiment of the utility model combines accompanying drawing explanation.This aircraft comprises
The specific embodiment of the utility model combines accompanying drawing explanation.This aircraft comprises buoyance lift device (1), automobile (15) and sail (26).Automobile (15) is gone up to load and is mounted with wind energy absorber and wind energy converter, and wind energy absorber comprises windmill (22), sail (26), bearing (21) and bearing fixing frame (20); Wind energy converter comprises wind energy transfer trunk (12), bent axle (27) connecting rod (13) and piston (8).Wind energy transfer trunk (12) is gone up to support storage tank (3) is installed; One side of storage tank (3) is installed with bearing (21) through bearing fixing frame (20); Bearing (21) top is equipped with bearing carrier ring (24), and the below of bearing is mounted with rotor generator (28) through bearing fixing frame (20); Bearing carrier ring (24) all around the symmetry the position on sail frame (25) is installed; Sail (26) is installed on the sail frame (25), and the front end of sail frame (25) is equipped with windmill (22), and turning cylinder (19) is installed in the inner ring hole of bearing (21); Turning cylinder (19) is connected with bent axle (27); The lower end of bent axle (27) is sleeved in the axle sleeve (17), and bent axle (27) is connected with wind energy transfer trunk (12) with strut bar (16) through axle sleeve (17), and the front and back end of wind energy transfer trunk (12) all is equipped with valve (7) and valve (18).The recessed axle of bent axle (27) is connected with the connecting rod (13) in the wind energy transfer trunk (12), and connecting rod (13) is connected with piston (8), and wind energy transfer trunk (12) is connected with storage tank (3) through admission port (6), and the afterbody of storage tank (3) is provided with inflation inlet (4).The car body rear side of automobile (15) is installed the storage battery (11) that reserve power is used, and storage tank (3) is connected with buoyance lift device (1) through connection cord (2).The bottom of buoyance lift device (1) is equipped with electric lift-up screw propeller (29).
The utility model buoyance lift device (1) can be the helium dirigible, also can be the hydrogen dirigible.
Claims (2)
1. the dual-purpose flight device in breeze wind vacant lot; This aircraft comprises buoyance lift device (1), automobile (15) and sail (26); It is characterized in that: automobile (15) is gone up to load and is mounted with wind energy absorber and wind energy converter, and wind energy absorber comprises windmill (22), sail (26), bearing (21) and bearing fixing frame (20); Wind energy converter comprises wind energy transfer trunk (12), bent axle (27), connecting rod (13) and piston (8); Wind energy transfer trunk (12) is gone up to support storage tank (3) is installed; One side of storage tank (3) is installed with bearing (21) through bearing fixing frame (20); Bearing (21) top is equipped with bearing carrier ring (24), and the below of bearing is mounted with rotor generator (28) through bearing fixing frame (20); Bearing carrier ring (24) all around the symmetry the position on sail frame (25) is installed, sail (26) is installed on the sail frame (25), the front end of sail frame (25) is equipped with windmill (22); Turning cylinder (19) is installed in the inner ring hole of bearing (21); Turning cylinder (19) is connected with bent axle (27), and the lower end of bent axle (27) is sleeved in the axle sleeve (17), and bent axle (27) is connected with wind energy transfer trunk (12) with strut bar (16) through axle sleeve (17); The recessed axle of bent axle (27) is connected with the connecting rod (13) in the wind energy transfer trunk (12); Connecting rod (13) is connected with piston (8), and wind energy transfer trunk (12) is connected with storage tank (3) through admission port (6), and the car body rear side of automobile (15) is installed the storage battery (11) that reserve power is used; Storage tank (3) is connected with buoyance lift device (1) through connection cord (2), and the bottom of buoyance lift device (1) is equipped with electric lift-up screw propeller (29).
2. the dual-purpose flight device in breeze wind according to claim 1 vacant lot is characterized in that buoyance lift device (1) can be the helium dirigible, also can be the hydrogen dirigible.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012201432634U CN202557242U (en) | 2012-04-09 | 2012-04-09 | Breeze generation airphibious flying aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012201432634U CN202557242U (en) | 2012-04-09 | 2012-04-09 | Breeze generation airphibious flying aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202557242U true CN202557242U (en) | 2012-11-28 |
Family
ID=47206935
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012201432634U Expired - Fee Related CN202557242U (en) | 2012-04-09 | 2012-04-09 | Breeze generation airphibious flying aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202557242U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582385A (en) * | 2012-04-09 | 2012-07-18 | 杨礼诚 | Breeze power generation dual-purpose dart flyer for air and ground |
| CN103661915A (en) * | 2013-11-18 | 2014-03-26 | 中国空间技术研究院 | Natural heat and sail driven aerostat system with controllable track |
| RU2658938C1 (en) * | 2017-07-19 | 2018-06-26 | Александр Александрович Перфилов | Aerostat |
| RU2752039C2 (en) * | 2018-03-30 | 2021-07-22 | Александр Александрович Перфилов | Hybrid aeronautical vehicle |
-
2012
- 2012-04-09 CN CN2012201432634U patent/CN202557242U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102582385A (en) * | 2012-04-09 | 2012-07-18 | 杨礼诚 | Breeze power generation dual-purpose dart flyer for air and ground |
| CN103661915A (en) * | 2013-11-18 | 2014-03-26 | 中国空间技术研究院 | Natural heat and sail driven aerostat system with controllable track |
| CN103661915B (en) * | 2013-11-18 | 2015-12-30 | 中国空间技术研究院 | The controlled aerostat system of track that a kind of atural beat and sail drive |
| RU2658938C1 (en) * | 2017-07-19 | 2018-06-26 | Александр Александрович Перфилов | Aerostat |
| RU2752039C2 (en) * | 2018-03-30 | 2021-07-22 | Александр Александрович Перфилов | Hybrid aeronautical vehicle |
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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: 20121128 Termination date: 20180409 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |