CN105129076A - Remotely-piloted vehicle with isolating layers arranged on planes of rotor wings - Google Patents
Remotely-piloted vehicle with isolating layers arranged on planes of rotor wings Download PDFInfo
- Publication number
- CN105129076A CN105129076A CN201510595152.5A CN201510595152A CN105129076A CN 105129076 A CN105129076 A CN 105129076A CN 201510595152 A CN201510595152 A CN 201510595152A CN 105129076 A CN105129076 A CN 105129076A
- Authority
- CN
- China
- Prior art keywords
- remotely
- rotor
- isolation layer
- piloted vehicle
- rotor wings
- Prior art date
- 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.)
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Classifications
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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
Abstract
A remotely-piloted vehicle with isolating layers arranged on planes of rotor wings comprises a vehicle body, a plurality of rotor wings, a flight state computer control system, a battery, an air vehicle load and a remote control, wherein the flight state computer control system comprises a satellite positioning terminal, an accelerometer, a magnetometer, an air pressure transducer, a gyroscope and a communication module. The remotely-piloted vehicle is characterized by comprising a thin film object which is approximately located in the same horizontal plane position with the rotor wings, and holes are formed in positions, corresponding to the electric rotor wings, of the thin film object. The isolating layers are located on the same plane as rotor wing panels, so that a low pressure area is efficiently kept above the isolating layers, upward tensile force on the remotely-piloted vehicle is formed, and wind pressure loss of the remotely-piloted vehicle provided with the rotor wings is remarkably reduced. A power transmission line is connected with an external power supply, and accordingly, the hovering capability can be improved.
Description
Technical field
The present invention relates to the remotely-piloted vehicle that rotor plane arranges isolation layer.
Background technology
Existing a kind of rotor craft, the blast utilizing rotor to produce promotes aircraft.But these blast are due to the centrifugal action of air-flow and had more loss by the reverse flow of periphery.
Summary of the invention
The object of the invention is to provide the rotor craft reducing blast loss.
The present invention realizes the technical scheme of its object: manufacture the remotely-piloted vehicle that a rotor plane arranges isolation layer, comprise fuselage, several rotors, state of flight computer control system, battery, aircraft load and remote controller, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module; Adopt a film-form object being roughly in same level position with rotor; This film-form object is in electronic rotor place perforate.
The power transmission line that can also adopt external power supply and be connected with external power supply.
Can also in the periphery of isolation layer seamless link flange up and/or down; Or described tapping seamless link axial flow air channel, a rotor is just arranged in inside, axial flow air channel.
The upper edge hole of described flange can also be made to be connected with a lightweight retaining frame.
The surface of described isolation layer can also be made to contain photovoltaic cell.
Rotor craft comprises a post and multiaxis rotor craft, and a post comprises single-blade and double-vane.
Beneficial effect of the present invention: be positioned at conplane isolation layer with rotor fin, makes an efficient maintenance meiobar on isolation layer form a pulling force upwards to aircraft, thus obviously reduces the blast loss of rotor craft.Adopt power transmission line to be connected with external power supply, stagnant empty ability can be improved.
Accompanying drawing explanation
Fig. 1 is the top view that a rotor plane arranges four rotor remotely-piloted vehicles of isolation layer.
Fig. 2 is the front elevation that a rotor plane arranges four rotor remotely-piloted vehicles of isolation layer.
Fig. 3 is the structural representation in an axial flow air channel.
1. aircraft in figure; 2. fuselage; 3. electronic rotor; 4. early warning radar; 5. power transmission line; 6. external power supply; 7. isolation layer; 8. flange; 9. retaining frame; 10. air channel; 11. high-pressure areas; 12. areas of low pressure; 13. connecting rods.
Detailed description of the invention
Fig. 1 to 3 provides embodiment 1.
In embodiment 1, the remotely-piloted vehicle 1 that rotor plane arranges isolation layer comprises fuselage 2, electronic rotor 3, state of flight computer control system, radio signal reception process launch facility, early warning radar 4, remote controller, external power supply 6, the power transmission line 5 connecting external power supply 6 and isolation layer 7 as aircraft load.
Isolation layer 7 comprises aluminium sheet with lightweight sheet material and plastic sheeting makes, and is arranged at plane place, electronic rotor 3 place; The seamless link flange 8 up and down in the periphery of isolation layer 7; The upper edge hole of flange 8 is connected with a lightweight retaining frame 9; Lightweight retaining frame 9 is connected with fuselage 2 by connecting rod 13.
Isolation layer 7 is in electronic rotor 3 place's perforate and seamless adapter shaft stream air channel 10.The prior art of all right axis of reference flow fan of related content in axial flow air channel.
Lightweight retaining frame can adopt carbon fiber material, light, shock-resistant.Port below axial flow air channel can be larger than port above.
Adopt the benefit of isolation layer 7 comprise by isolation layer 7 can the plane of each electronic rotor 3 place below and above a maintenance high-pressure area 11 and an area of low pressure 12 respectively.When the pressure of high-pressure area 11 exceeds about 0.003 standard atmosphere in area of low pressure 12, every sq m just can produce about 30kg(10000*0.003*1) lift.And the electric power consumed is only about 1.5kw, significantly reduce than not adopting during isolation layer.Flange 8 and axial flow air channel 10 contribute to strengthening the difference of pressure between high-pressure area 11 and area of low pressure 12.The efficiency of electronic rotor can be improved in axial flow air channel 10.The altitude range of flange 8 can get 50 to 600 millimeters; The altitude range in axial flow air channel 10 can get 10 to 65 millimeters.
The photovoltaic cell of insulation surface can adopt film photovoltaic cell, specifically can with reference to prior art.
The remotely-piloted vehicle that rotor plane arranges isolation layer also can utilize self-contained storage battery to be used as power power supply flight.
Claims (5)
1. rotor plane arranges the remotely-piloted vehicle of isolation layer, comprise fuselage, several rotors, state of flight computer control system, battery, aircraft load and remote controller, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module, it is characterized in that the film-form object being roughly in same level position containing with rotor; This film-form object is in electronic rotor place perforate.
2. the remotely-piloted vehicle of isolation layer is set according to rotor plane according to claim 1, it is characterized in that containing external power supply and the power transmission line that is connected with external power supply.
3. the remotely-piloted vehicle of isolation layer is set according to the rotor plane described in claims 1 or 2, it is characterized in that in the periphery of isolation layer seamless link flange up and/or down; Or described tapping seamless link axial flow air channel, a rotor is just arranged in inside, axial flow air channel.
4. the remotely-piloted vehicle of isolation layer is set according to the rotor plane described in claims 1 or 2, it is characterized in that the upper edge hole of described flange is connected with a lightweight retaining frame.
5. the remotely-piloted vehicle of isolation layer is set according to the rotor plane described in claims 1 or 2, it is characterized in that photovoltaic cell is contained on the surface of described isolation layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595152.5A CN105129076A (en) | 2015-09-18 | 2015-09-18 | Remotely-piloted vehicle with isolating layers arranged on planes of rotor wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510595152.5A CN105129076A (en) | 2015-09-18 | 2015-09-18 | Remotely-piloted vehicle with isolating layers arranged on planes of rotor wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105129076A true CN105129076A (en) | 2015-12-09 |
Family
ID=54714766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510595152.5A Withdrawn CN105129076A (en) | 2015-09-18 | 2015-09-18 | Remotely-piloted vehicle with isolating layers arranged on planes of rotor wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105129076A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110220853A (en) * | 2019-04-29 | 2019-09-10 | 西安科技大学 | Laser spectrum telemetering early warning UAV system and localization method for pipe gallery |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101385903A (en) * | 2007-09-14 | 2009-03-18 | 北京德庐影像技术有限责任公司 | Hitching type electric self-service helicopter and system thereof |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| CN103803075A (en) * | 2012-11-15 | 2014-05-21 | 西安韦德沃德航空科技有限公司 | Solar gear-transmission disc type multi-rotor-wing aircraft |
| CN104002974A (en) * | 2014-06-16 | 2014-08-27 | 中国科学院自动化研究所 | Dragging type unmanned liquid application system based on multi-rotor craft |
-
2015
- 2015-09-18 CN CN201510595152.5A patent/CN105129076A/en not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101385903A (en) * | 2007-09-14 | 2009-03-18 | 北京德庐影像技术有限责任公司 | Hitching type electric self-service helicopter and system thereof |
| US20130233964A1 (en) * | 2012-03-07 | 2013-09-12 | Aurora Flight Sciences Corporation | Tethered aerial system for data gathering |
| CN103803075A (en) * | 2012-11-15 | 2014-05-21 | 西安韦德沃德航空科技有限公司 | Solar gear-transmission disc type multi-rotor-wing aircraft |
| CN104002974A (en) * | 2014-06-16 | 2014-08-27 | 中国科学院自动化研究所 | Dragging type unmanned liquid application system based on multi-rotor craft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110220853A (en) * | 2019-04-29 | 2019-09-10 | 西安科技大学 | Laser spectrum telemetering early warning UAV system and localization method for pipe gallery |
| CN110220853B (en) * | 2019-04-29 | 2022-04-12 | 西安科技大学 | Laser spectrum telemetering and early warning unmanned aerial vehicle system for comprehensive pipe gallery and positioning method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| CB02 | Change of applicant information |
Address after: Taizhou City, Zhejiang province 317500 Wenling City Taiping Street South Road 109 Lane 9 Applicant after: Shi Zhongtian Address before: 200335 Changning District, Gan Xi Road, Lane 100, room 30, No. 502, room Applicant before: Shi Zhongtian |
|
| COR | Change of bibliographic data | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20151209 |