CN102923314A - Hybrid power distribution mooring flying platform with double power sources - Google Patents

Hybrid power distribution mooring flying platform with double power sources Download PDF

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Publication number
CN102923314A
CN102923314A CN2012104408504A CN201210440850A CN102923314A CN 102923314 A CN102923314 A CN 102923314A CN 2012104408504 A CN2012104408504 A CN 2012104408504A CN 201210440850 A CN201210440850 A CN 201210440850A CN 102923314 A CN102923314 A CN 102923314A
Authority
CN
China
Prior art keywords
flying platform
mooring
power supply
platform
power source
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.)
Pending
Application number
CN2012104408504A
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Chinese (zh)
Inventor
韩剑华
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHANGHAI JIAO TONG UNIVERSITY WUXI RESEARCH INSTITUTE
Shanghai Jiaotong University
Original Assignee
SHANGHAI JIAO TONG UNIVERSITY WUXI RESEARCH INSTITUTE
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SHANGHAI JIAO TONG UNIVERSITY WUXI RESEARCH INSTITUTE filed Critical SHANGHAI JIAO TONG UNIVERSITY WUXI RESEARCH INSTITUTE
Priority to CN2012104408504A priority Critical patent/CN102923314A/en
Publication of CN102923314A publication Critical patent/CN102923314A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a hybrid power distribution mooring flying platform with double power sources. The hybrid power distribution mooring flying platform comprises a flying platform, a mooring cable and a ground power source, wherein the ground power source supplies power to the flying platform through the mooring cable. The hybrid power distribution mooring flying platform is characterized in that an onboard battery pack power source is arranged on the flying platform and is charged by the ground power source through the mooring cable. After an onboard battery pack is additionally arranged on the flying platform under the supervisory control of a supervisory control module, the posture of the flying platform can be controlled under instantaneous sudden disturbance; capacity of the ground power source can be reduced to effectively achieve mooring power supply for a long time at a long distance, and the bottleneck that cruise duration of an electric flight vehicle is short is relieved; and emergency landing can be achieved when failure of the ground power source happens.

Description

A kind of mixing distribution pending flight platform of dual power supply
Technical field
The present invention relates to a kind of aviation aircraft of hovering, particularly relate to a kind of mixing distribution pending flight platform of dual power supply.
Background technology
Existing pending flight lift-off plateform system has the ground power supply power supply by the mooring cable, because electric energy is sufficient, landing is flexible, controls easyly, can aloft hover for a long time, can satisfy preferably basic demand.But because ground supply voltage output is relatively steady, when transient changing appears in the skyborne flight environment of vehicle of aircraft, can't in time tackle adjustment.When mooring cable or surface power station fault, aircraft will be in runaway condition in addition.
Summary of the invention
The object of the invention is that the defective for prior art provides a kind of mixing distribution pending flight platform of dual power supply
The present invention adopts following technical scheme for achieving the above object:
A kind of mixing distribution pending flight platform of dual power supply, comprise flying platform, mooring cable and ground power supply, described flying platform by ground power supply by the mooring cable power supply, it is characterized in that: organic pond group power supply that powers on is set on the described flying platform, it is charged by the mooring cable by ground power supply.
It is further characterized in that: battery power comprises battery pack and management control module on the platform machine on the described machine; Described management control module is used for charging and the power supply of battery pack on the control platform machine.
Flying platform of the present invention is after battery pack on the adding machine under the management control of management control module, and first can solve the attitude control of flying platform when moment happens suddenly disturbance; Second can reduce the capacity of ground power supply, so that long distance time mooring power supply is able to effective realization, breaks through Electric aircraft short bottleneck in cruise duration; The 3rd emergency landing ability when having possessed the ground power supply fault.
Description of drawings
Fig. 1 is scheme drawing of the present invention
The specific embodiment
A kind of mixing distribution pending flight platform of dual power supply as shown in Figure 1, comprise flying platform 1, mooring cable 2 and ground power supply 3, described flying platform 1 is powered by mooring cable 2 by ground power supply 3, organic pond group power supply 11 that powers on is set on the described flying platform 1, by ground power supply 3 by mooring cable 2 to its charging.
Battery power 11 comprises battery pack and management control module on the platform machine on the described machine; Described management control module is used for charging and the power supply of battery pack on the control platform machine.
The battery pack that disposes on the platform can drive separately aircraft flight 1 ~ 2 minute, provides the electric energy that satisfies 130% energy requirement of normality flight to aircraft by the mooring cable.Intelligent electric power management control module makes that battery pack is charged to saturated on keeping machine in the situation that satisfies normality flight demand, when transient changing appears in flight environment of vehicle, provide the additional electrical energy reply by battery pack on the machine, when mooring cable or surface power station fault, also finish the emergency landing operation by battery pack on the machine equally.

Claims (2)

1. the mixing distribution pending flight platform of a dual power supply, comprise flying platform, mooring cable and ground power supply, described flying platform by ground power supply by the mooring cable power supply, it is characterized in that: organic pond group power supply that powers on is set on the described flying platform, it is charged by the mooring cable by ground power supply.
2. the mixing distribution pending flight platform of dual power supply according to claim 1, it is characterized in that: battery power comprises battery pack and management control module on the platform machine on the described machine; Described management control module is used for charging and the power supply of battery pack on the control platform machine.
CN2012104408504A 2012-11-07 2012-11-07 Hybrid power distribution mooring flying platform with double power sources Pending CN102923314A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2012104408504A CN102923314A (en) 2012-11-07 2012-11-07 Hybrid power distribution mooring flying platform with double power sources

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2012104408504A CN102923314A (en) 2012-11-07 2012-11-07 Hybrid power distribution mooring flying platform with double power sources

Publications (1)

Publication Number Publication Date
CN102923314A true CN102923314A (en) 2013-02-13

Family

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Family Applications (1)

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CN2012104408504A Pending CN102923314A (en) 2012-11-07 2012-11-07 Hybrid power distribution mooring flying platform with double power sources

Country Status (1)

Country Link
CN (1) CN102923314A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104192316A (en) * 2014-09-10 2014-12-10 徐伟佳 Unmanned aerial vehicle mooring system
JP2015189321A (en) * 2014-03-28 2015-11-02 株式会社熊谷組 Unmanned flight imaging device
CN107340779A (en) * 2017-07-26 2017-11-10 上海俏动智能化科技有限公司 Voltage compensating method and device in a kind of flight control process
CN108279731A (en) * 2018-01-25 2018-07-13 南京佰联信息技术有限公司 Method, system and the computer readable storage medium of supply voltage adjustment
CN111344224A (en) * 2017-11-29 2020-06-26 英国电讯有限公司 Electric power transmission

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1080609A (en) * 1992-06-29 1994-01-12 蔡渤啸 Electric power helicopter
US5709580A (en) * 1996-05-28 1998-01-20 Stanzel; Victor Control and power mechanism for model aircraft
WO2009005875A2 (en) * 2007-04-19 2009-01-08 Samuel Alan Johnson Aerial robot with dispensable conductive filament
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
CN202953185U (en) * 2012-11-07 2013-05-29 上海交通大学无锡研究院 Dual-power-source mixed power distribution tethered flight platform

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1080609A (en) * 1992-06-29 1994-01-12 蔡渤啸 Electric power helicopter
US5709580A (en) * 1996-05-28 1998-01-20 Stanzel; Victor Control and power mechanism for model aircraft
WO2009005875A2 (en) * 2007-04-19 2009-01-08 Samuel Alan Johnson Aerial robot with dispensable conductive filament
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
CN202953185U (en) * 2012-11-07 2013-05-29 上海交通大学无锡研究院 Dual-power-source mixed power distribution tethered flight platform

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015189321A (en) * 2014-03-28 2015-11-02 株式会社熊谷組 Unmanned flight imaging device
CN104192316A (en) * 2014-09-10 2014-12-10 徐伟佳 Unmanned aerial vehicle mooring system
CN107340779A (en) * 2017-07-26 2017-11-10 上海俏动智能化科技有限公司 Voltage compensating method and device in a kind of flight control process
CN111344224A (en) * 2017-11-29 2020-06-26 英国电讯有限公司 Electric power transmission
US10926890B2 (en) 2017-11-29 2021-02-23 British Telecommunications Public Limited Company Delivery of electrical power to an unmanned aircraft
CN108279731A (en) * 2018-01-25 2018-07-13 南京佰联信息技术有限公司 Method, system and the computer readable storage medium of supply voltage adjustment
CN108279731B (en) * 2018-01-25 2020-07-31 南京佰联信息技术有限公司 Method, system and computer readable storage medium for adjusting power supply voltage

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Application publication date: 20130213

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