CN102923314A - Hybrid power distribution mooring flying platform with double power sources - Google Patents
Hybrid power distribution mooring flying platform with double power sources Download PDFInfo
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- 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
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Abstract
本发明公布了一种双电源的混合配电系留飞行平台，包括飞行平台、系留电缆和地面电源，所述飞行平台由地面电源通过系留电缆供电，其特征在于：所述飞行平台上设置有机上电池组电源，由地面电源通过系留电缆对其充电。本发明飞行平台在管理控制模块的管理控制下加入机上电池组后，第一可以解决飞行平台在瞬间突发扰动时的姿态控制；第二可以减小地面电源的容量，使得长距离长时间系留供电得以有效实现，突破电动飞行器续航时间短的瓶颈；第三具备了地面电源故障时的紧急迫降能力。
The invention discloses a moored flying platform with mixed power distribution with dual power supplies, including a flying platform, a mooring cable and a ground power supply. The flying platform is powered by the ground power supply through the mooring cable, and is characterized in that: An on-board battery pack power supply is provided, which is charged by a ground power source via a tethered cable. After the flight platform of the present invention is added to the on-board battery pack under the management control of the management control module, it can firstly solve the attitude control of the flight platform when it is suddenly disturbed in an instant; The reserved power supply can be effectively realized, breaking through the bottleneck of short battery life of electric aircraft; thirdly, it has the emergency landing capability when the ground power supply fails.
Description
技术领域 technical field
本发明涉及一种空中悬停的航空飞行器，特别是涉及一种双电源的混合配电系留飞行平台。 The invention relates to an aerial vehicle hovering in the air, in particular to a dual power source mixed power distribution tethered flight platform.
背景技术 Background technique
现有系留飞行升空平台系统通过系留电缆有地面电源供电，由于电能充足，起降灵活，控制简便，可长时间在空中悬停，能较好地满足基本要求。但是由于地面供电电压输出相对平稳，当飞行器在空中的飞行环境出现瞬态变化时，无法及时进行应对调整。另外当系留电缆或者地面电站故障时，飞行器就会处于失控状态。 The existing tethered flying lift-off platform system is powered by a ground power supply through the tethered cable. Due to sufficient power, flexible take-off and landing, easy control, and long-term hovering in the air, it can better meet the basic requirements. However, due to the relatively stable output of the ground power supply voltage, it is impossible to make timely adjustments when the aircraft's flight environment in the air changes transiently. In addition, when the tethered cable or the ground power station fails, the aircraft will be out of control.
发明内容 Contents of the invention
本发明目的在于针对现有技术的缺陷提供一种双电源的混合配电系留飞行平台 The purpose of the present invention is to provide a hybrid power distribution tethered flight platform with dual power supplies for the defects of the prior art
本发明为实现上述目的，采用如下技术方案： In order to achieve the above object, the present invention adopts the following technical solutions:
一种双电源的混合配电系留飞行平台，包括飞行平台、系留电缆和地面电源，所述飞行平台由地面电源通过系留电缆供电，其特征在于：所述飞行平台上设置有机上电池组电源，由地面电源通过系留电缆对其充电。 A hybrid power distribution tethered flight platform with dual power supplies, including a flight platform, a tethered cable and a ground power supply, the flight platform is powered by the ground power supply through the tethered cable, and it is characterized in that: the flight platform is provided with an on-board battery The group power supply is charged by the ground power supply through the tethered cable.
其进一步特征在于：所述机上电池组电源包括平台机上电池组和管理控制模块；所述管理控制模块用于控制平台机上电池组的充电和供电。 It is further characterized in that: the onboard battery pack power supply includes a platform onboard battery pack and a management control module; the management control module is used to control the charging and power supply of the platform onboard battery pack.
本发明飞行平台在管理控制模块的管理控制下加入机上电池组后，第一可以解决飞行平台在瞬间突发扰动时的姿态控制；第二可以减小地面电源的容量，使得长距离长时间系留供电得以有效实现，突破电动飞行器续航时间短的瓶颈；第三具备了地面电源故障时的紧急迫降能力。 After the flight platform of the present invention is added to the on-board battery pack under the management control of the management control module, first, it can solve the attitude control of the flight platform when it is suddenly disturbed in an instant; The reserved power supply can be effectively realized, breaking through the bottleneck of short battery life of electric aircraft; thirdly, it has the emergency landing capability when the ground power supply fails.
附图说明 Description of drawings
图 1 为本发明示意图 Figure 1 is a schematic diagram of the present invention
具体实施方式 Detailed ways
如图1所示一种双电源的混合配电系留飞行平台，包括飞行平台1、系留电缆2和地面电源3，所述飞行平台1由地面电源3通过系留电缆2供电，所述飞行平台1上设置有机上电池组电源11，由地面电源3通过系留电缆2对其充电。
As shown in Figure 1, a hybrid power distribution mooring flight platform with dual power supplies includes a
所述机上电池组电源11包括平台机上电池组和管理控制模块；所述管理控制模块用于控制平台机上电池组的充电和供电。
The onboard battery
平台上配置的电池组能单独驱动飞行器飞行1~2分钟，通过系留电缆向飞行器提供满足常态飞行130%所需能量的电能。一个智能电源管理控制模块使在满足常态飞行需求的情况下保持对机上电池组充电到饱和，当飞行环境出现瞬态变化时，由机上电池组提供额外电能应对，同样在系留电缆或者地面电站故障时，也由机上电池组完成紧急迫降操作。 The battery pack configured on the platform can independently drive the aircraft to fly for 1 to 2 minutes, and provide the aircraft with electrical energy that meets 130% of the energy required for normal flight through the tethered cable. An intelligent power management control module keeps the on-board battery pack charged to saturation under the condition of meeting the normal flight requirements. When the flight environment undergoes transient changes, the on-board battery pack provides additional power to deal with it, also in the mooring cable or ground power station In the event of failure, the emergency landing operation is also completed by the battery pack on board.
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| Application Number | Priority Date | Filing Date | Title |
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| CN2012104408504A CN102923314A (en) | 2012-11-07 | 2012-11-07 | Hybrid power distribution mooring flying platform with double power sources |
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| CN2012104408504A CN102923314A (en) | 2012-11-07 | 2012-11-07 | Hybrid power distribution mooring flying platform with double power sources |
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Cited By (6)
| 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 | power delivery |
| US11563329B2 (en) | 2016-08-22 | 2023-01-24 | Ee Limited | Delivery of electrical power |
Citations (5)
| 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 |
-
2012
- 2012-11-07 CN CN2012104408504A patent/CN102923314A/en active Pending
Patent Citations (5)
| 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 (8)
| 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 |
| US11563329B2 (en) | 2016-08-22 | 2023-01-24 | Ee Limited | Delivery of electrical power |
| 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 | power delivery |
| 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 |