CN203652101U - Thermodynamic regulation in-air positioning aircraft - Google Patents
Thermodynamic regulation in-air positioning aircraft Download PDFInfo
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- CN203652101U CN203652101U CN201320723662.2U CN201320723662U CN203652101U CN 203652101 U CN203652101 U CN 203652101U CN 201320723662 U CN201320723662 U CN 201320723662U CN 203652101 U CN203652101 U CN 203652101U
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Abstract
The utility model relates to the field of fluid dynamics, in particular to the field of buoyancy flight equipment. A thermodynamic regulation in-air positioning aircraft comprises an airbag main body and also comprises a suspension positioning system, wherein the suspension positioning system is connected to the airbag main body; a height measurement device is connected with a control circuit, and the control circuit is connected with a lifting power device. Flying height is detected by the height measurement device, and height information is transmitted to the control circuit by the height measurement device. The lifting power device is controlled by the control circuit according to the height information, and accordingly, the flight height of the airbag main body is controlled. When a height detecting device detects that the flight height is lower than a set height, rising is executed by the lifting power device under the control of the control circuit, and the airbag main body is lifted; when the height detecting device detects that the flight height is higher than the set height, dropping is executed by the lifting power device under the control of the control circuit, and the airbag main body is lowered.
Description
Technical field
The utility model relates to fluid mechanics field, is specifically related to buoyancy flight equipment field.
Background technology
Balloon is being a kind of conventional toy, decorative fitting, meeting-place articles for use.In live and work, often can use balloon.The application of balloon in live and work, has had century-old above history.
Along with scientific and technological development, shape, the color of balloon are more and more abundanter, and material is also more and more firm.But overall variation is little.In whole design, relatively dull, lack intention.
Utility model content
The purpose of this utility model is, provides a kind of heating power to regulate aerial positioning flight device, to address the above problem.
The technical matters that the utility model solves can realize by the following technical solutions:
Heating power regulates aerial positioning flight device, comprises an air bag main body, it is characterized in that, also comprises a suspension position fixing system; Described suspension position fixing system is connected on described air bag main body;
Described suspension position fixing system, comprise that one provides the lifting power plant of power for rising or declining, and one detects height measuring device and a control circuit highly;
Described height measuring device connects described control circuit, lifting power plant described in described control circuit control linkage one;
Described lifting power plant adopts a heat energy regulator control system.
Described height measuring device detects flying height.And elevation information is passed to described control circuit, control circuit, according to elevation information, is controlled lifting power plant.And then the flying height of control air bag main body.
In the time that height detecting device detects flying height lower than setting height, lifting power plant is carried out vertical motion described in described control circuit control, makes air bag main body increase.In the time flying height being detected higher than setting height, lifting power plant is carried out down maneuver described in described control circuit control, and air bag main body is declined.
Described heating power regulates the aerial buoyancy of aerial positioning flight device to be less than self gravitation, and described lifting power plant is for only providing the lifting power plant of rising power.With simplification system.
Described heating power regulates the aerial buoyancy of aerial positioning flight device to be greater than self gravitation, and described lifting power plant is for only providing the lifting power plant of decline power.With simplification system.
Or described lifting power plant, for rising power both can be provided, can provide again the lifting power plant of decline power.To realize flexible response.
Described heat energy regulator control system comprises an electric heater unit, and described electric heater unit is connected on balloon.For described balloon provides heat, after the material in balloon is heated, expand, and then impel balloon volume to increase, and then buoyancy is increased, thereby produce buoyancy upwards.
Described electric heater unit can be positioned at described balloon or be attached to outside the balloon wall of described balloon.
Described balloon can be described air bag main body, and described electric heater unit is positioned at described air bag main body.
Described balloon also can be independent of described air bag main body, is connected with described air bag main body.Can be positioned at outside described air bag main body or described air bag main body.
Described balloon below is also provided with a container, and the heater element of described electric heater unit is positioned at described container.
In described container, liquid substance is housed.Described liquid substance, under the heating of described heater element, produces steam, and then increases the volume of described balloon.Thereby increase buoyancy.Described liquid can adopt the boiling points such as water, propylene dichloride, parabolic hydrocarbon, alkene, alcohol, aldehyde, amine, ester, ether, ketone, aromatic hydrocarbon, hydrogenate hydrocarbon, terpene hydrocarbon, halogenated hydrocarbons lower, the liquid that is easy to evaporation, concrete composition can also be water, alcohol, formaldehyde, gasoline.
Described container is positioned at described balloon below, the balloon wall laminating of the edge of opening of described container and described balloon.So that become liquid or solid-state material after cooling, again fall back in described container, use in order to heating next time.
Described height measuring device can adopt reflective height measuring device, comprises a sender unit and a signal receiving device;
The signal downrange of described sender unit towards, with the receiving side signal of described signal receiving device to towards consistent, so that receive the signal firing back.
The signal downrange of described sender unit towards, with the receiving side signal of described signal receiving device to towards, all downward or top.
Downward time, can, by measuring terrain clearance, know elevation information.Upward time, when indoor, can pass through the distance of measuring distance top ceiling, side reflects the elevation information of flight.
Described signal receiving device is being received after the signal that described sender unit sends, and produces a high level, and described high level output is given described control circuit, and described control circuit is described lifting power plant power supply, makes described lifting power plant work.
Described control circuit can be a signal amplification circuit.Amplify the electric current of described signal receiving device output, and then drive described lifting power plant work.
Described control circuit can comprise a time delay circuit.Time delay is carried out in current impulse to described signal receiving device output, and then drives described lifting power plant to work gently, avoids pulse current to cause rush of current to described lifting power plant.
Described suspension position fixing system also comprises a battery system, and described battery system is provided with charging inlet.And be described suspension position fixing system power supply.
Receiving side signal to towards down, below described signal receiving device receives, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height lower than setting height, and controlling described lifting power plant provides the lift of rising.
Receiving side signal to towards down, below described signal receiving device does not receive, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height higher than setting height, and controlling described lifting power plant provides the power of decline.
Receiving side signal to towards upward, above described signal receiving device receives, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height higher than setting height, and controlling described lifting power plant provides the power of decline.
Reflective height measuring device, can adopt an active infra-red distance measuring equipment (DME), and described sender unit adopts an infrared launcher, and described signal receiving device adopts an infrared receiving device.
Reflective height measuring device, can adopt a supersonic range finder, and described sender unit adopts a ultrasonic transmission device, and described signal receiving device adopts a ultrasonic probe, ultrasonic receiver.
Reflective height measuring device, can adopt a laser ranging system, and described sender unit adopts a laser feedway, and described signal receiving device adopts a laser signal receiving device.
In described air bag main body, being filled with the gas that density is less than air, can be hydrogen, helium or other gas.
Described air bag main body sealing.Avoid gas leakage.
Described heating power regulates the difference of the aerial buoyancy of aerial positioning flight device and self gravitation, is less than 1/10th of self gravitation value.Further preferably, heating power regulates the difference of the aerial buoyancy of aerial positioning flight device and self gravitation, is greater than one of two percentages of self gravitation value.
Described air bag main body can be for being at least one in superman, angel, angle, fairy maiden, dragon, bird, winged insect, aircraft, the sun or moon moulding.
Described suspension position fixing system detouchable is fixed on described air bag main body.Can be by being adhesively fixed on described air bag main body.So that described suspension position fixing system and common air bag main body are arranged in pairs or groups flexibly.
Can be that described suspension position fixing system is bonded in described air bag main body top or below.
Described suspension position fixing system is provided with a bonding coat.On described bonding coat, can be provided with a parting paper.In use parting paper is peeled off, be then bonded on described air bag main body.
Can be that described heating power regulates aerial positioning flight device that flying power system is not installed so that simplification system, reduce gravity, reduce costs, save energy extend the flight time.
Also can be, also comprise a flying power system, and a signal handling equipment, described signal handling equipment also connects the control interface of described flying power system.For heating power regulates, aerial positioning flight device provides action power to described flying power system.
Described flying power system comprises electrical motor and blower impeller, and blower impeller rotates described in described direct motor drive provides power.
Can also be, described flying power system comprises electrical motor and fin, and fin swings described in described direct motor drive provides power.
Described signal handling equipment is also connected with a wireless interaction system, and described wireless interaction system support has a wireless interaction terminal.Heating power regulates aerial positioning flight device to realize information interaction by described wireless interaction system and wireless interaction terminal.
Described information interaction comprises that heating power regulates aerial positioning flight device status data to be handed down to described unlimited interactive terminal.Also comprise, control command is uploaded to described wireless interaction system by described wireless interaction terminal, and then be uploaded to described signal handling equipment.
Also comprise, described wireless interaction terminal sends remote signal to described wireless interaction system in real time, and then is uploaded to described signal handling equipment, carries out real time remote control control.
Brief description of the drawings
Fig. 1 is a kind of integral structure schematic diagram that heating power regulates aerial positioning flight device;
Fig. 2 is lifting power plant structural principle schematic diagram.
Detailed description of the invention
For technological means, creation characteristic that the utility model is realized, reach object and effect is easy to understand, below in conjunction with further elaboration the utility model of concrete diagram.
With reference to Fig. 1, Fig. 2, heating power regulates aerial positioning flight device, comprises an air bag main body 1, also comprises a suspension position fixing system 2; Suspension position fixing system 2 is fixed on air bag main body 1.Suspension position fixing system 2, comprise that one provides the lifting power plant 21 of power for rising or declining, and one detects height measuring device 23 and a control circuit 22 highly.Height measuring device 23 connects control circuit 22, control circuit 22 control linkage one lifting power plants 21.In control circuit 22, can be provided with a microprocessor system.In order to processing data.
Height measuring device 23 detects flying height.And elevation information is passed to control circuit 22, control circuit 22, according to elevation information, is controlled lifting power plant 21.And then the flying height of control air bag main body 1.
In the time that height detecting device detects flying height lower than setting height, control circuit 22 is controlled lifting power plant 21 and is carried out vertical motion, makes air bag main body 1 increase.In the time flying height being detected higher than setting height, control circuit 22 is controlled lifting power plant 21 and is carried out down maneuver, and air bag main body 1 is declined.
In air bag main body 1, being filled with the gas that density is less than air, can be hydrogen, helium or other gas.Air bag main body 1 seals.Avoid gas leakage.Heating power regulates the difference of the aerial buoyancy of aerial positioning flight device and self gravitation, is less than 1/10th of self gravitation value.Further preferably, heating power regulates the difference of the aerial buoyancy of aerial positioning flight device and self gravitation, is greater than one of two percentages of self gravitation value.
Air bag main body 1 can be for being at least one in superman, angel, angle, fairy maiden, dragon, bird, winged insect, aircraft, the sun or moon moulding.
Suspension position fixing system 2 detouchables are fixed on air bag main body 1.Can be by being adhesively fixed on air bag main body 1.So that suspension position fixing system 2 is arranged in pairs or groups flexibly with common air bag main body 1.Can be that suspension position fixing system 2 is bonded in air bag main body 1 top or below.Suspension position fixing system 2 is provided with a bonding coat.Bonding coat is provided with a parting paper.In use parting paper is peeled off, be then bonded on air bag main body 1.Can be that heating power regulates aerial positioning flight device that flying power system is not installed so that simplification system, reduce gravity, reduce costs, save energy extend the flight time.
In concrete enforcement, a kind of form can be set to: heating power regulates the aerial buoyancy of aerial positioning flight device to be less than self gravitation, and lifting power plant 21 is for the lifting power plant 21 of rising power is only provided, with simplification system.Another kind of form can be set to: heating power regulates the aerial buoyancy of aerial positioning flight device to be greater than self gravitation, and lifting power plant 21 is for only providing the lifting power plant 21 of decline power.With simplification system; Or can be set to: lifting power plant 21, for rising power both can be provided, can provide again the lifting power plant 21 of decline power, to realize flexible response.
In concrete enforcement, lifting power plant 21 can adopt following form:
Lifting power plant 21 adopts a heat energy regulator control system, and heat energy regulator control system comprises an electric heater unit, and electric heater unit is on a balloon, for balloon provides heat, after the material in balloon is heated, expand, and then impel balloon volume to increase, and then buoyancy is increased, thereby produce buoyancy upwards.Electric heater unit can be positioned at balloon or be attached to outside the balloon wall of balloon.Balloon can be air bag main body 1, and electric heater unit is positioned at air bag main body 1.Balloon also can be independent of air bag main body 1, is connected with air bag main body 1.Can be positioned at outside air bag main body 1 or air bag main body 1.
In the time adopting heat energy regulator control system, balloon below is also provided with a container, and electric heater unit heater element is positioned at container.Liquid substance is housed in container, and liquid substance, under the heating of heater element, produces steam, and then increases the volume of balloon.Thereby increase buoyancy.Liquid can adopt the boiling points such as water, propylene dichloride, parabolic hydrocarbon, alkene, alcohol, aldehyde, amine, ester, ether, ketone, aromatic hydrocarbon, hydrogenate hydrocarbon, terpene hydrocarbon, halogenated hydrocarbons lower, the liquid that is easy to evaporation, concrete composition can also be water, alcohol, formaldehyde, gasoline.Container is positioned at balloon below, the balloon wall laminating of the edge of opening of container and balloon.So that become liquid or solid-state material after cooling, again fall back in container, use in order to heating next time.
In specific embodiment, height measuring device 23 can adopt following form:
Downward time, can, by measuring terrain clearance, know elevation information.Upward time, when indoor, can pass through the distance of measuring distance top ceiling, side reflects the elevation information of flight.
Signal receiving device is being received after the signal that sender unit sends, and produces a high level, and high level output is to control circuit 22, and control circuit 22 is powered for lifting power plant 21, and lifting power plant 21 is worked, and rises or declines.
Receiving side signal to towards down, when the useful signal of being launched by sender unit that reflects below signal receiving device receives, control circuit 22 is considered as flying height lower than setting height, controlling lifting power plant 21 provides the lift of rising.
Receiving side signal to towards down, when the useful signal of being launched by sender unit that reflects below signal receiving device does not receive, control circuit 22 is considered as flying height higher than setting height, controlling lifting power plant 21 provides the power of decline.
Receiving side signal to towards upward, when the useful signal of being launched by sender unit that reflects above signal receiving device receives, control circuit 22 is considered as flying height higher than setting height, controlling lifting power plant 21 provides the power of decline.
Reflective height measuring device 23, can adopt an active infra-red distance measuring equipment (DME), and sender unit adopts an infrared launcher, and signal receiving device adopts an infrared receiving device.
Reflective height measuring device 23, can adopt a supersonic range finder, and sender unit adopts a ultrasonic transmission device, and signal receiving device adopts a ultrasonic probe, ultrasonic receiver.
Reflective height measuring device 23, can adopt a laser ranging system, and sender unit adopts a laser feedway, and signal receiving device adopts a laser signal receiving device.
Heating power regulates aerial positioning flight device also passable, also comprises a flying power system, and a signal handling equipment, and signal handling equipment also connects the control interface of flying power system.For heating power regulates, aerial positioning flight device provides action power to flying power system.
Flying power system comprises electrical motor and blower impeller, and direct motor drive blower impeller rotates provides power.Can also be, flying power system comprises electrical motor and fin, and direct motor drive fin swings provides power.
Signal handling equipment is also connected with a wireless interaction system, and wireless interaction system support has a wireless interaction terminal.Heating power regulates aerial positioning flight device to realize information interaction by wireless interaction system and wireless interaction terminal.
Information interaction comprises that heating power regulates aerial positioning flight device status data to be handed down to unlimited interactive terminal.Also comprise, control command is uploaded to wireless interaction system by wireless interaction terminal, and then be uploaded to signal handling equipment.Also comprise, wireless interaction terminal sends remote signal to wireless interaction system in real time, and then is uploaded to signal handling equipment, carries out real time remote control control.
More than show and described groundwork of the present utility model and principal character and advantage of the present utility model.The technical personnel of the industry should be understood; the utility model is not restricted to the described embodiments; that in above-described embodiment and specification sheets, describes just illustrates principle of the present utility model; do not departing under the prerequisite of the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (49)
1. heating power regulates aerial positioning flight device, comprises an air bag main body, it is characterized in that, also comprises a suspension position fixing system; Described suspension position fixing system is connected on described air bag main body;
Described suspension position fixing system, comprise that one provides the lifting power plant of power for rising or declining, and one detects height measuring device and a control circuit highly;
Described height measuring device connects described control circuit, lifting power plant described in described control circuit control linkage one;
Adopt a heat energy regulator control system at described lifting power plant, described heat energy regulator control system comprises an electric heater unit, and described electric heater unit is connected on balloon.
2. heating power according to claim 1 regulates aerial positioning flight device, it is characterized in that: described heating power regulates the aerial buoyancy of aerial positioning flight device to be less than self gravitation, and described lifting power plant is for only providing the lifting power plant of rising power.
3. heating power according to claim 1 regulates aerial positioning flight device, it is characterized in that: described heating power regulates the aerial buoyancy of aerial positioning flight device to be greater than self gravitation, and described lifting power plant is for only providing the lifting power plant of decline power.
4. heating power according to claim 1 regulates aerial positioning flight device, it is characterized in that: described balloon below is also provided with a container, and described heater element is positioned at described container;
In described container, liquid substance is housed.
5. heating power according to claim 1 regulates aerial positioning flight device, it is characterized in that: described height measuring device adopts reflective height measuring device, comprises a sender unit and a signal receiving device;
The signal downrange of described sender unit towards, with the receiving side signal of described signal receiving device to towards consistent, so that receive the signal firing back.
6. heating power according to claim 5 regulates aerial positioning flight device, it is characterized in that: described signal receiving device is being received after the signal that described sender unit sends, produce a high level, described high level output is given described control circuit, described control circuit is described lifting power plant power supply, makes described lifting power plant work.
7. heating power according to claim 5 regulates aerial positioning flight device, it is characterized in that: described reflective height measuring device, adopt an active infra-red distance measuring equipment (DME), described sender unit adopts an infrared launcher, and described signal receiving device adopts an infrared receiving device.
8. regulate aerial positioning flight device according to the heating power described in any one in claim 1 to 7, it is characterized in that: described heating power regulates the difference of the aerial buoyancy of aerial positioning flight device and self gravitation, be less than 1/10th of self gravitation value, be greater than one of two percentages of self gravitation value.
9. regulate aerial positioning flight device according to the heating power described in any one in claim 1 to 7, it is characterized in that: described suspension position fixing system detouchable is fixed on described air bag main body; By being adhesively fixed on described air bag main body.
10. regulate aerial positioning flight device according to the heating power described in any one in claim 1 to 7, it is characterized in that: described heating power regulates aerial positioning flight device that flying power system is not installed.
11. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described control circuit is provided with a microprocessor system processing data.
12. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described height measuring device detects flying height.
13. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: elevation information is passed to described control circuit, and control circuit, according to elevation information, is controlled lifting power plant.
14. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: when described height detecting device detects flying height lower than setting height, described in described control circuit control, lifting power plant is carried out vertical motion, makes air bag main body increase.
15. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: when described height detecting device detects flying height higher than setting height, described in described control circuit control, lifting power plant is carried out down maneuver, and air bag main body is declined.
16. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described lifting power plant, for rising power is both provided, provides again the lifting power plant of decline power.
17. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described electric heater unit is positioned at described balloon or is attached to outside the balloon wall of described balloon.
18. heating power according to claim 17 regulate aerial positioning flight device, it is characterized in that: described balloon is described air bag main body, and described electric heater unit is positioned at described air bag main body.
19. heating power according to claim 17 regulate aerial positioning flight device, it is characterized in that: described balloon is independent of described air bag main body, are connected with described air bag main body.
20. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described balloon is positioned at outside described air bag main body or described air bag main body.
21. heating power according to claim 4 regulate aerial positioning flight device, it is characterized in that: described liquid substance, under the heating of described heater element, produces steam.
22. heating power according to claim 4 regulate aerial positioning flight device, it is characterized in that: described liquid is that any one boiling point in water, propylene dichloride, parabolic hydrocarbon, alkene, alcohol, aldehyde, amine, ester, ether, ketone, aromatic hydrocarbon, hydrogenate hydrocarbon, terpene hydrocarbon, halogenated hydrocarbons is lower, be easy to the liquid of evaporation.
23. heating power according to claim 4 regulate aerial positioning flight device, it is characterized in that: described container is positioned at described balloon below, the balloon wall laminating of the edge of opening of described container and described balloon.
24. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: the signal downrange of described sender unit towards, with the receiving side signal of described signal receiving device to towards, all downward or top.
25. heating power according to claim 6 regulate aerial positioning flight device, it is characterized in that: described control circuit can be a signal amplification circuit.
26. heating power according to claim 25 regulate aerial positioning flight device, it is characterized in that: amplify the electric current of described signal receiving device output, and then drive described lifting power plant work.
27. heating power according to claim 6 regulate aerial positioning flight device, it is characterized in that: described control circuit comprises a time delay circuit.
28. heating power according to claim 27 regulate aerial positioning flight device, it is characterized in that: time delay is carried out in the current impulse to described signal receiving device output, and then drives described lifting power plant to work gently.
29. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described suspension position fixing system comprises a battery system, and described battery system is provided with charging inlet, are described suspension position fixing system power supply.
30. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: receiving side signal to towards down, below described signal receiving device receives, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height lower than setting height, and controlling described lifting power plant provides the lift of rising.
31. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: receiving side signal to towards down, below described signal receiving device does not receive, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height higher than setting height, and controlling described lifting power plant provides the power of decline.
32. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: receiving side signal to towards upward, above described signal receiving device receives, reflect the useful signal of being launched by described sender unit time, described control circuit is considered as flying height higher than setting height, and controlling described lifting power plant provides the power of decline.
33. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: described reflective height measuring device, adopt a supersonic range finder, described sender unit adopts a ultrasonic transmission device, and described signal receiving device adopts a ultrasonic probe, ultrasonic receiver.
34. heating power according to claim 5 regulate aerial positioning flight device, it is characterized in that: described reflective height measuring device, adopt a laser ranging system, described sender unit adopts a laser feedway, and described signal receiving device adopts a laser signal receiving device.
35. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: in described air bag main body, being filled with the gas that density is less than air, can be hydrogen, helium or other gas.
36. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described air bag main body sealing.
37. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described air bag main body is at least one in superman, angel, angle, fairy maiden, dragon, bird, winged insect, aircraft, the sun or moon moulding.
38. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described suspension position fixing system is bonded in described air bag main body top or below.
39. regulate aerial positioning flight device according to the heating power described in claim 38, it is characterized in that: described suspension position fixing system is provided with a bonding coat.
40. regulate aerial positioning flight device according to the heating power described in claim 39, it is characterized in that: described bonding coat is provided with a parting paper.
41. heating power according to claim 1 regulate aerial positioning flight device, it is characterized in that: described heating power regulates aerial positioning flight device, comprise a flying power system, and a signal handling equipment, described signal handling equipment also connects the control interface of described flying power system.
42. regulate aerial positioning flight device according to the heating power described in claim 41, it is characterized in that: for heating power regulates, aerial positioning flight device provides action power to described flying power system.
43. regulate aerial positioning flight device according to the heating power described in claim 41, it is characterized in that: described flying power system comprises electrical motor and blower impeller, and blower impeller rotates described in described direct motor drive provides power.
44. regulate aerial positioning flight device according to the heating power described in claim 41, it is characterized in that: described flying power system comprises electrical motor and fin, and fin swings described in described direct motor drive provides power.
45. regulate aerial positioning flight device according to the heating power described in claim 41, it is characterized in that: described signal handling equipment is also connected with a wireless interaction system, and described wireless interaction system support has a wireless interaction terminal.
46. regulate aerial positioning flight device according to the heating power described in claim 45, it is characterized in that: heating power regulates aerial positioning flight device to realize information interaction by described wireless interaction system and wireless interaction terminal.
47. regulate aerial positioning flight device according to the heating power described in claim 46, it is characterized in that: described information interaction comprises that heating power regulates aerial positioning flight device status data to be handed down to described unlimited interactive terminal.
48. regulate aerial positioning flight device according to the heating power described in claim 45, it is characterized in that: control command is uploaded to described wireless interaction system by described wireless interaction terminal, and then are uploaded to described signal handling equipment.
49. regulate aerial positioning flight device according to the heating power described in claim 45, it is characterized in that: described wireless interaction terminal sends remote signal to described wireless interaction system in real time, and then is uploaded to described signal handling equipment, carries out real time remote control control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320723662.2U CN203652101U (en) | 2013-02-08 | 2013-11-15 | Thermodynamic regulation in-air positioning aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310050866.9 | 2013-02-08 | ||
| CN201310050866 | 2013-02-08 | ||
| CN201320723662.2U CN203652101U (en) | 2013-02-08 | 2013-11-15 | Thermodynamic regulation in-air positioning aircraft |
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| CN203652101U true CN203652101U (en) | 2014-06-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201320723662.2U Expired - Fee Related CN203652101U (en) | 2013-02-08 | 2013-11-15 | Thermodynamic regulation in-air positioning aircraft |
| CN201320723619.6U Expired - Fee Related CN203727639U (en) | 2013-02-08 | 2013-11-15 | Aerial positioning air vehicle |
| CN201310572047.0A Pending CN103977568A (en) | 2013-02-08 | 2013-11-15 | Height self-feedback positioning suspension device |
| CN201320728904.7U Expired - Fee Related CN203803115U (en) | 2013-02-08 | 2013-11-18 | Height control device of buoyancy aircraft |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201320723619.6U Expired - Fee Related CN203727639U (en) | 2013-02-08 | 2013-11-15 | Aerial positioning air vehicle |
| CN201310572047.0A Pending CN103977568A (en) | 2013-02-08 | 2013-11-15 | Height self-feedback positioning suspension device |
| CN201320728904.7U Expired - Fee Related CN203803115U (en) | 2013-02-08 | 2013-11-18 | Height control device of buoyancy aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105311839A (en) * | 2014-06-25 | 2016-02-10 | 上海本星电子科技有限公司 | Balloon aerial height positioner |
| CN107656529A (en) * | 2016-07-23 | 2018-02-02 | 深圳曼塔智能科技有限公司 | Unmanned plane and the fixed high control method of unmanned plane |
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| CN106595572B (en) * | 2016-10-20 | 2020-07-03 | 北京理工大学 | Method and device for measuring low-altitude flight height of aircraft |
| CN106774365A (en) * | 2016-12-20 | 2017-05-31 | 华中科技大学 | A kind of unmanned plane debugging system based on external view positioning |
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|---|---|---|---|---|
| CN201280224Y (en) * | 2008-09-16 | 2009-07-29 | *** | Hot gas airship of helium gas |
| CN201445800U (en) * | 2009-06-25 | 2010-05-05 | 汕头市澄海区锦江玩具实业有限公司 | Coaxial double rotor wing remote control helicopter and obstacle avoidance system thereof |
| CN102139164B (en) * | 2011-01-28 | 2012-05-23 | 深圳市格兰之特科技有限公司 | Flying device and method capable of automatically avoiding barrier |
| CN102339063B (en) * | 2011-07-14 | 2013-08-21 | 沈阳航空航天大学 | Autonomous taking off and landing control method for indoor airship |
| CN203806130U (en) * | 2013-01-28 | 2014-09-03 | 上海科斗电子科技有限公司 | Phase change regulation and control aircraft |
-
2013
- 2013-11-15 CN CN201320723662.2U patent/CN203652101U/en not_active Expired - Fee Related
- 2013-11-15 CN CN201320723619.6U patent/CN203727639U/en not_active Expired - Fee Related
- 2013-11-15 CN CN201310572047.0A patent/CN103977568A/en active Pending
- 2013-11-18 CN CN201320728904.7U patent/CN203803115U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105311839A (en) * | 2014-06-25 | 2016-02-10 | 上海本星电子科技有限公司 | Balloon aerial height positioner |
| CN107656529A (en) * | 2016-07-23 | 2018-02-02 | 深圳曼塔智能科技有限公司 | Unmanned plane and the fixed high control method of unmanned plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103977568A (en) | 2014-08-13 |
| CN203727639U (en) | 2014-07-23 |
| CN203803115U (en) | 2014-09-03 |
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