CN204507268U - Helios power system - Google Patents
Helios power system Download PDFInfo
- Publication number
- CN204507268U CN204507268U CN201520127522.8U CN201520127522U CN204507268U CN 204507268 U CN204507268 U CN 204507268U CN 201520127522 U CN201520127522 U CN 201520127522U CN 204507268 U CN204507268 U CN 204507268U
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- China
- Prior art keywords
- photovoltaic
- parafoil
- power
- helios
- aircraft
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
A kind of Helios power system comprises: photovoltaic parafoil, and it is made up of photovoltaic umbrella cloth, and photovoltaic umbrella cloth comprises printing opacity protective layer, photovoltaic interlayer and airtight load bottom; Umbrella rope, it comprises bearing layer, conductor layer and protective cover, and this umbrella rope one end is connected on photovoltaic parafoil, and the other end is connected on aircraft, and wherein this protective cover is set in outside conductor layer, and is arranged on bearing layer side; Control setup, it is connected with described photovoltaic parafoil, following power executing device and storage battery; Storage battery, it is connected with photovoltaic parafoil and following power executing device; And power executing device, it comprises electrical motor, retarder and screw propeller.Photovoltaic parafoil face area is comparatively large, can be electric energy by more light energy conversion, and parafoil can provide flight required lift simultaneously; The all power resources of system are in solar power, and solar power belongs to clean reproducible energy, and system in use can not to environment; Greatly can increase the cruise duration of aircraft.
Description
Technical field
The utility model belongs to Power System of Flight Vehicle field, particularly a kind of Helios power system.
Background technology
Aircraft is the apparatus flyer flown in endoatmosphere or space, exoatmosphere (space) being manufactured by the mankind, can fly away from ground, control in spaceflight and by people.Aircraft can fall into 5 types: aerocraft, spacecraft, rocket, guided missile and guided weapon.Aerocraft is called, as fire balloon, aerodone, dirigible, aircraft, helicopter etc. at the aircraft of endoatmosphere flight.Their quiet buoyancy by air or the aerodynamic force lift-off flight of air relative motion generation.By whether personnel of carrying divide, can be divided into again and have people's aircraft and unmanned vehicle.Mostly existing aircraft is to adopt fossil fuel as the energy.Fossil fuel is used to have following several shortcoming as the energy: first, fossil fuel is non-renewable energy resources; Secondly, environmental pollution can be caused after combustion of fossil fuel; 3rd, aircraft overall weight can lighten along with the burning of fossil fuel, and the barycenter of aircraft also can change, and this can affect the stability of aircraft flight, to the design of aircraft, controls to bring difficulty, adds corresponding R&D costs; 4th, the flying power of aircraft can be subject to the restriction of fossil fuel, and fuel tape has lacked, and flying power is shorter, and fuel tape is many, can increase again the total weight of aircraft.
Therefore, in order to solve many deficiencies and the defect of above-mentioned prior art, be necessary to study a kind of Helios power system.
Utility model content
Consider at least one the problems referred to above and complete the utility model, and an object of the present utility model is to provide a kind of Helios power system, this Helios power system can the original fossil fuel powered systems of Substitute For Partial aircraft.Overcome that fossil fuel is non-renewable, the shortcoming of contaminated environment, meanwhile, in whole flight course, aircraft will cause quality to lighten because of the burning of fuel, and this contributes to the stability strengthening aircraft flight, reduces the difficulty of design.And the flying power of aircraft will increase greatly, be no longer limited to the number of carrying fuel.This contribute to aircraft monitoring, take photo by plane, the application in the field such as communication.Wherein, this Helios power system, is characterized in that comprising:
Photovoltaic parafoil, it is made up of photovoltaic umbrella cloth, and photovoltaic umbrella cloth comprises printing opacity protective layer, photovoltaic interlayer and airtight load bottom;
Umbrella rope, it comprises bearing layer, conductor layer and protective cover, and this umbrella rope one end is connected on photovoltaic parafoil, and the other end is connected on aircraft, and wherein this protective cover is set in outside conductor layer, and is arranged on bearing layer side;
Control setup, it is connected with described photovoltaic parafoil, following power executing device and storage battery;
Storage battery, it is connected with photovoltaic parafoil and following power executing device;
Power executing device, it comprises electrical motor, retarder and screw propeller.
According to the utility model on the other hand, described storage battery is connected with photovoltaic parafoil by described conductor layer.
According to the utility model on the other hand, described photovoltaic interlayer is made up of flexible solar battery.
According to the utility model on the other hand, described control setup is for the mode of operation of the rotating speed and photovoltaic parafoil that control electrical motor.
Compared with prior art, the beneficial effects of the utility model are:
Photovoltaic parafoil face area is comparatively large, can be electric energy by more light energy conversion, and parafoil can provide flight required lift simultaneously; The all power resources of system are in solar power, and solar power belongs to clean reproducible energy, and system in use can not to environment; Greatly can increase the cruise duration of aircraft.
Accompanying drawing explanation
Fig. 1 is the structural representation of the Helios power system according to the utility model preferred embodiment.
Fig. 2 is the structural representation of the Helios power system according to another preferred embodiment of the utility model.
Fig. 3 is the structural representation of the Helios power system according to the another preferred embodiment of the utility model.
Fig. 4 is the structural representation of the Helios power system according to the another preferred embodiment of the utility model.
Fig. 5 is the structural representation of the Helios power system according to the another preferred embodiment of the utility model.
Fig. 6 is the photovoltaic umbrella cloth schematic cross-section of the Helios power system according to the utility model preferred embodiment.
Fig. 7 is the umbrella rope schematic cross-section of the Helios power system according to the utility model preferred embodiment.
Fig. 8 is the power executing device structural representation of the Helios power system according to the utility model preferred embodiment.
Fig. 9 controls schematic diagram according to the control system of the Helios power system of the utility model preferred embodiment.
Detailed description of the invention
Below in conjunction with accompanying drawing; by preferred embodiment, preferred forms of the present utility model is described; here detailed description of the invention is to explain the utility model; and should not be construed as restriction of the present utility model; when not departing from spirit of the present utility model and essential scope; can make various changes and modifications, these all should be included within protection domain of the present utility model.
Embodiment 1
See Fig. 1-9, the utility model provides a kind of Helios power system.Such as, this Helios power system can comprise: photovoltaic parafoil 1, and it is made up of photovoltaic umbrella cloth 6, and photovoltaic umbrella cloth 6 comprises printing opacity protective layer 7, photovoltaic interlayer 8 and airtight load bottom 9;
Umbrella rope 2, it comprises bearing layer 10, conductor layer 11 and protective cover 12, and this umbrella rope 2 one end is connected on photovoltaic parafoil 1, and the other end is connected on aircraft, and wherein this protective cover is set in outside conductor layer, and is arranged on bearing layer side;
Control setup 3, it is connected with described photovoltaic parafoil 1, following power executing device 5 and storage battery 4;
Storage battery 4, it is connected with photovoltaic parafoil 1 and following power executing device 5;
Power executing device 5, it comprises electrical motor 13, retarder and screw propeller 14.
Preferably, state storage battery 4 to be connected with photovoltaic parafoil 1 by described conductor layer.
Preferably, described photovoltaic interlayer is made up of flexible solar battery.
Preferably, described control setup 3 is for the mode of operation of the rotating speed and photovoltaic parafoil 1 that control electrical motor.
Preferably, additionally provide a kind of Helios power system, it comprises photovoltaic parafoil 1, umbrella rope 2, control setup 3, storage battery 4, power executing device 5, and its concrete structure and mode of operation are:
Contrast Fig. 1-6, described photovoltaic parafoil 1 is made by photovoltaic umbrella cloth 6 and is formed, photovoltaic umbrella cloth 6 forms by three layers, and outermost layer is protective layer 7, and protective layer 7 has the characteristic of printing opacity, interlayer is photovoltaic layer 8, photovoltaic layer 8 is made up of flexible solar battery, and can be electric energy by light energy conversion, bottom be bearing layer 9, when photovoltaic parafoil 1 works, bearing layer 9 is mainly used to bear the motive power be subject to when photovoltaic parafoil 1 works.In flight course, photovoltaic parafoil 1 will provide the lift required for aircraft flight, and meanwhile, it is the task of electric energy that photovoltaic parafoil 1 also carries light energy conversion, provides lasting electric power by the rotation for electrical motor 13, makes aircraft have lasting flying power.
Preferably; contrast Fig. 1-5,7; described umbrella rope 2 is made up of bearing layer 10, conductor layer 11, protective cover 12; bearing layer 10 is used for bearing all pulling force; the power delivery that conductor layer 11 is used for photovoltaic parafoil 1 to transform is to consumers such as storage battery 4 and control setup 3, electrical motors, and it is injury-free that protective cover 12 is used for guardwire layer 11.Umbrella rope 2 one end is connected on photovoltaic parafoil 1, and the other end is connected on aircraft.
Preferably, contrast Fig. 1-5,9, described control setup 3 can control rotating speed, the break-make of circuit system, the mode of operation etc. of photovoltaic parafoil 1 of electrical motor, simultaneously can the break-make situation of collection system circuit portions, the information such as service condition, electrical motor 13 rotation situation of photovoltaic parafoil 1.
Preferably, contrast Fig. 1-5, described storage battery 4 is connected with photovoltaic parafoil 1 by the conductor layer 11 in umbrella rope, and the electric energy of photovoltaic parafoil 1 conversion can be saved in storage battery 4, and storage battery 4 is connected by consumers such as wire and control setup 3, electrical motors 13.
Preferably, contrast Fig. 1-5,8, described power executing device 5 is made up of electrical motor 13, screw propeller 14 etc., and electrical motor 13 is connected with storage battery 4, control setup 3 by wire, and electrical motor 13 and screw propeller 14 link together.
Be understandable that, the utility model has the following advantages:
Photovoltaic parafoil face area is comparatively large, can be electric energy by more light energy conversion, and parafoil can provide flight required lift simultaneously; The all power resources of system are in solar power, and solar power belongs to clean reproducible energy, and system in use can not to environment; Greatly can increase the cruise duration of aircraft.
The utility model is not limited to above-mentioned specific embodiment.Be understandable that, when not departing from spirit of the present utility model and essential scope, can make various changes and modifications, these all should be included within protection domain of the present utility model.
Claims (3)
1. a Helios power system, is characterized in that comprising:
Photovoltaic parafoil, it is made up of photovoltaic umbrella cloth, and photovoltaic umbrella cloth comprises printing opacity protective layer, photovoltaic interlayer and airtight load bottom;
Umbrella rope, it comprises bearing layer, conductor layer and protective cover, and this umbrella rope one end is connected on photovoltaic parafoil, and the other end is connected on aircraft, and wherein this protective cover is set in outside conductor layer, and is arranged on bearing layer side;
Control setup, it is connected with described photovoltaic parafoil, following power executing device and storage battery;
Storage battery, it is connected with photovoltaic parafoil and following power executing device; With
Power executing device, it comprises electrical motor, retarder and screw propeller.
2. Helios power system according to claim 1, is characterized in that described storage battery is connected with photovoltaic parafoil by described conductor layer.
3. Helios power system according to claim 2, is characterized in that described photovoltaic interlayer is made up of flexible solar battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520127522.8U CN204507268U (en) | 2015-03-05 | 2015-03-05 | Helios power system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520127522.8U CN204507268U (en) | 2015-03-05 | 2015-03-05 | Helios power system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204507268U true CN204507268U (en) | 2015-07-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520127522.8U Active CN204507268U (en) | 2015-03-05 | 2015-03-05 | Helios power system |
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| CN (1) | CN204507268U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104648669A (en) * | 2015-03-05 | 2015-05-27 | 襄阳宏伟航空器有限责任公司 | Solar air vehicle power system |
| CN105270626A (en) * | 2015-11-09 | 2016-01-27 | 襄阳宏伟航空器有限责任公司 | Intelligent unmanned sowing aerial vehicle |
-
2015
- 2015-03-05 CN CN201520127522.8U patent/CN204507268U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104648669A (en) * | 2015-03-05 | 2015-05-27 | 襄阳宏伟航空器有限责任公司 | Solar air vehicle power system |
| CN105270626A (en) * | 2015-11-09 | 2016-01-27 | 襄阳宏伟航空器有限责任公司 | Intelligent unmanned sowing aerial vehicle |
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| C14 | Grant of patent or utility model | ||
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