CN102935886B - A kind of multistage mooring rotor lift-off plateform system - Google Patents
A kind of multistage mooring rotor lift-off plateform system Download PDFInfo
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- CN102935886B CN102935886B CN201210437352.4A CN201210437352A CN102935886B CN 102935886 B CN102935886 B CN 102935886B CN 201210437352 A CN201210437352 A CN 201210437352A CN 102935886 B CN102935886 B CN 102935886B
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Abstract
The invention discloses a kind of multistage mooring rotor lift-off plateform system, it comprises and is provided with multiple lift-off platform unit, multiple heaving pile unit and a ground safeguard unit.By the different upper and lower cascades of heaving pile unit between lift-off platform unit, upper class lift-off platform unit provides electric energy by the next stage platform unit that goes up to the air, and the most next stage platform unit that goes up to the air provides electric energy by ground safeguard unit.Classification is powered and effectively can be reduced the weight of classification heaving pile unit, makes whole system when equal lift, work of can hovering on higher height.Classification is powered and also effectively can be mated the relation of power-supply system voltage and power, reduces the difficulty realized.
Description
Technical field
The present invention relates to a kind of aviation aircraft of hovering.Be applicable to the radio system such as communication, scouting, monitoring, radar, radio control, electronic countermeasure and space base platform is set, improve " the lift-off benefit " of radio system.
Background technology
Radiowave can be considered rectilinear propagation.Due to the impact of earth surface curvature, the transmission of radiowave is subject to the restriction of sighting distance.The effective ways addressed this problem, are placed on radio equipment exactly on lift-off platform, increase the true altitude on itself and ground, to strengthen horizon range.Namely this is so-called radio equipment " lift-off benefit ".
Existing mooring rotor lift-off plateform system is due to electric energy abundance, and landing is flexible, controls easy, can aloft hover for a long time, can meet basic demand preferably.If but the lift-off platform unit in mooring rotor lift-off plateform system raises hover height further, be used for mentioning longer heavier heaving pile unit by needing the power strengthening driving motor to produce larger lift, add and high-powerly the electric current in heaving pile unit power lead can be made again to strengthen, thus need the sectional area strengthening power lead, increase heaving pile unit weight.Setting like this constrains lift-off platform unit hover height.
Summary of the invention
Problem to be solved by this invention is: provide a kind of multistage mooring rotor lift-off plateform system, every one-level electric power is made to be distribution of grades, upper class heaving pile unit only transmits electric energy needed for self, thus reduce the weight of this grade of heaving pile unit, system can be made under equal electric power in higher height hovering work, meet the needs that radio system improves " lift-off benefit " further.
The present invention for achieving the above object, adopts following technical scheme:
A kind of multistage mooring rotor lift-off plateform system, comprise lift-off platform unit, heaving pile unit, ground safeguard unit, it is characterized in that: this multistage mooring rotor lift-off plateform system is provided with two or more lift-off platform unit, by the different upper and lower cascades of heaving pile unit between lift-off platform unit, upper class lift-off platform unit provides electric energy by the next stage platform unit that goes up to the air, and most next stage lift-off platform unit provides electric energy by ground safeguard unit.
It is further characterized in that: the electric power of described upper class heaving pile unit transmission is less than the electric power of next stage heaving pile unit transmission.
The present invention compared with prior art has the following advantages: 1, classification is powered and effectively can be reduced the weight of classification heaving pile unit, makes whole system when equal lift, work of can hovering on higher height; 2, classification is powered and effectively can be mated the relation of power-supply system voltage and power, reduces the difficulty realized.
Accompanying drawing explanation
Fig. 1 is multistage mooring rotor lift-off plateform system schematic diagram.
In figure: 1, upper class lift-off platform unit, 2, upper class heaving pile unit, 3, next stage lift-off platform unit, 4, next stage heaving pile unit, 5, ground safeguard unit.
Detailed description of the invention
Embodiment provided by the invention is a two-stage mooring rotor lift-off plateform system.
See Fig. 1, upper class lift-off platform unit 1 is connected with upper class heaving pile unit 2, next stage lift-off platform unit 3 is upwards connected with upper class heaving pile unit 2, and downward and next stage heaving pile unit 4 is connected, and last next stage heaving pile unit 4 is bound up on above ground safeguard unit 5.Supply unit in ground safeguard unit 5, by next stage heaving pile unit 4 for next stage lift-off platform unit 3 is powered, next stage lift-off platform unit 3 is powered to upper class lift-off platform unit 1 by upper class heaving pile unit 2.
Next stage lift-off platform unit of the present invention needs the electric power according to upper class lift-off platform unit, for it provides specific electric energy, comprise voltage and the power of power supply, thus the cross-sectional area of power lead in upper class heaving pile unit is rationally set, reduce the unit weight of heaving pile unit, being conducive to lift-off platform unit when mentioning equivalent weight, higher hover height can be had.The heaving pile unit at the corresponding levels that next stage lift-off platform unit is corresponding, except need transmitting the electric power of upper class lift-off platform unit, also needs the electric power transmitting lift-off platform self at the corresponding levels.Therefore upper class go up to the air flat heaving pile platform unit transmission electric power be less than next stage heaving pile unit transmission electric power.
Claims (2)
1. a multistage mooring rotor lift-off plateform system, comprise lift-off platform unit, heaving pile unit, ground safeguard unit, it is characterized in that: this multistage mooring rotor lift-off plateform system is provided with two or more lift-off platform unit, by the different upper and lower cascades of heaving pile unit between lift-off platform unit, upper class lift-off platform unit provides electric energy by the next stage platform unit that goes up to the air, and most next stage lift-off platform unit provides electric energy by ground safeguard unit.
2. multistage mooring rotor lift-off plateform system as claimed in claim 1, is characterized in that: the electric power of described upper class heaving pile unit transmission is less than the electric power of next stage heaving pile unit transmission.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210437352.4A CN102935886B (en) | 2012-11-05 | 2012-11-05 | A kind of multistage mooring rotor lift-off plateform system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210437352.4A CN102935886B (en) | 2012-11-05 | 2012-11-05 | A kind of multistage mooring rotor lift-off plateform system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102935886A CN102935886A (en) | 2013-02-20 |
| CN102935886B true CN102935886B (en) | 2016-01-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210437352.4A Expired - Fee Related CN102935886B (en) | 2012-11-05 | 2012-11-05 | A kind of multistage mooring rotor lift-off plateform system |
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| CN (1) | CN102935886B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105739524B (en) * | 2015-11-11 | 2019-04-26 | 刘晓阳 | One kind being tethered at unmanned rotary wing aircraft cluster platform system and the continuous sprinkling system of liquid |
| CN107667746B (en) * | 2016-08-02 | 2019-07-26 | 国家电网公司 | Smart grid supports the accurate high-efficiency artificial rainfall method and system that have cable to go straight up to platform |
| CN106585972A (en) * | 2017-01-10 | 2017-04-26 | 周欣 | Multistage cascaded self-balancing mooring unmanned aerial vehicle system |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86100378A (en) * | 1986-01-14 | 1987-08-12 | 王泽印 | The unlimited extending structure of tether balloon hawser |
| CN2387031Y (en) * | 1999-06-25 | 2000-07-12 | 蔡渤啸 | Electric power fire ballon |
| CN102092473A (en) * | 2011-01-25 | 2011-06-15 | 凌强 | Multi-rotor craft and method thereof |
| CN202953163U (en) * | 2012-11-05 | 2013-05-29 | 上海交通大学无锡研究院 | Multilevel mooring rotor wing lift-off platform system |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7631834B1 (en) * | 2006-02-24 | 2009-12-15 | Stealth Robotics, Llc | Aerial robot with dispensable conductive filament |
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2012
- 2012-11-05 CN CN201210437352.4A patent/CN102935886B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN86100378A (en) * | 1986-01-14 | 1987-08-12 | 王泽印 | The unlimited extending structure of tether balloon hawser |
| CN2387031Y (en) * | 1999-06-25 | 2000-07-12 | 蔡渤啸 | Electric power fire ballon |
| CN102092473A (en) * | 2011-01-25 | 2011-06-15 | 凌强 | Multi-rotor craft and method thereof |
| CN202953163U (en) * | 2012-11-05 | 2013-05-29 | 上海交通大学无锡研究院 | Multilevel mooring rotor wing lift-off platform system |
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| CN102935886A (en) | 2013-02-20 |
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Granted publication date: 20160106 Termination date: 20161105 |