WO2013134962A1 - 一种具有状态监控功能的遥控飞机 - Google Patents

一种具有状态监控功能的遥控飞机 Download PDF

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Publication number
WO2013134962A1
WO2013134962A1 PCT/CN2012/072489 CN2012072489W WO2013134962A1 WO 2013134962 A1 WO2013134962 A1 WO 2013134962A1 CN 2012072489 W CN2012072489 W CN 2012072489W WO 2013134962 A1 WO2013134962 A1 WO 2013134962A1
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Prior art keywords
aircraft
remote control
signal transceiver
remote
monitoring function
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PCT/CN2012/072489
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English (en)
French (fr)
Inventor
罗之洪
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Luo Zhihong
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Publication date
Application filed by Luo Zhihong filed Critical Luo Zhihong
Priority to PCT/CN2012/072489 priority Critical patent/WO2013134962A1/zh
Publication of WO2013134962A1 publication Critical patent/WO2013134962A1/zh

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    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00—Toy aircraft; Other flying toys
    • A63H27/02—Model aircraft
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H30/00—Remote-control arrangements specially adapted for toys, e.g. for toy vehicles
    • A63H30/02—Electrical arrangements
    • A63H30/04—Electrical arrangements using wireless transmission

Definitions

  • the invention relates to a remote control aircraft, in particular to a remote control aircraft with a state monitoring function.
  • a remotely piloted aircraft is an aircraft that can control flight from a distance.
  • Remotely piloted aircraft typically fly from a battery placed inside the remotely piloted aircraft as an energy driven motor.
  • the temperature of the motor rises as the motor runs. Excessive temperatures can damage the motor.
  • the battery's power will drop as the motor runs. If the battery is too low to provide enough power to the motor, the in-flight remote control aircraft will fall and be damaged.
  • the existing remote-controlled aircraft does not have a state monitoring function, and cannot monitor the state of each component of the remote-controlled aircraft during flight, and therefore cannot make a pre-judgment and rapid response to a situation in which the battery power is too low or the motor temperature is too high, thereby causing The remote control aircraft has a high damage rate.
  • the object of the present invention is to overcome the deficiencies of the prior art and to provide a remote control aircraft having a state monitoring function capable of monitoring the state of a remotely controlled aircraft, thereby reducing the damage rate of the remotely controlled aircraft.
  • the present invention achieves the above object by the following scheme:
  • a remote control aircraft with state monitoring function is composed of a remote control aircraft with a signal transceiver aircraft end and a remote controller with a signal transceiver remote control.
  • the remote control aircraft is provided with a battery-powered motor, and the remote control aircraft is provided with a sensor component.
  • the sensor component transmits the status information of the remote control aircraft to the signal transceiver aircraft end and then to the signal transceiver remote control end.
  • the above-mentioned signal transceiver aircraft terminal and signal transceiver remote control directly utilize the RF of the original remote control aircraft (ie RF, the same below) signal transceiver, no additional modification is required.
  • the RF signal transceiver integrates the RF signal receiver and the transmitter, specifically the RF receiver and the transmitter share an RF The chip has the ability to transmit data in both directions.
  • the sensor component may include a power sensor.
  • the state information is the power of the battery, and may further include information such as voltage, current, and the like of the battery.
  • the sensor component further includes a temperature sensor. The temperature of the motor.
  • the sensor component may also include sensors such as position sensors (longitude, latitude, etc.), height sensors, rotational speed sensors, or GPS modules, etc., can be added as required, and the corresponding status information can include motor speed or GPS data (longitude, latitude, altitude, etc.).
  • the remote controller may further be provided with a display device, and the display device displays status information received by the signal receiver, for example, displaying battery power, motor temperature or other status information.
  • an alarm device may be disposed on the remote controller to issue an alarm when the status information received by the signal receiver exceeds the set range. For example, an alarm can be issued when the battery received by the signal receiver is lower than the set value or the temperature of the motor is higher than the set value.
  • the present invention has the following advantages:
  • the status of the remotely controlled aircraft such as temperature and power
  • the flight status of the remotely controlled aircraft can be prejudged
  • the RF receiver and transmitter share an RF chip.
  • the five-in-one control box can be integrated design; it has the advantages of small size and light weight.
  • FIG. 1 Schematic diagram of the functional modules of the present invention.
  • a remote control aircraft with status monitoring function consisting of a remote control aircraft 1 with a signal transceiver aircraft terminal 10 and a remote terminal with a signal transceiver 20
  • the remote control 2 is composed of a remote control aircraft 1 provided with a motor 12 powered by a battery 11 , a remote control aircraft 1 is provided with a sensor assembly 100 , and the sensor assembly 100 will be a remote control aircraft 1
  • the status information is transmitted to the signal transceiver aircraft terminal 10 and then to the signal transceiver remote terminal 20.
  • the sensor assembly 100 includes a power sensor 110 and a temperature sensor 120 for respectively transferring the amount of power of the battery 11 and the motor Status information such as temperature of 12.
  • the remote control device 2 is provided with a display device 21 for displaying the battery received by the signal transceiver remote terminal 20 11 or the motor 12 Status information such as temperature.
  • the remote control 2 is provided with an alarm device 22, when the signal transceiver remote terminal 20 receives the battery 11 An alarm is issued when the battery level is lower than the set value or the temperature of the motor 12 is higher than the set value.

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Selective Calling Equipment (AREA)

Abstract

一种具有状态监控功能的遥控飞机，由含有信号收发器飞机端（10）的遥控飞机（1）和含有信号收发器遥控端（20）的遥控器（2）组成，遥控飞机（1）上设置有由电池（11）提供能源的电机（12），遥控飞机（1）上设置有传感器组件（100），传感器组件（100）将遥控飞机（1）的状态信息传送至信号收发器飞机端（10），再发送至信号收发器遥控端（20）。通过接收到的状态信息，可以随时了解遥控飞机的状态如温度，电量等，对遥控飞机的飞行状态做出预判；在必要时还可以发出警报，避免遥控飞机的损坏。

Description

一种具有状态监控功能的遥控飞机
技术领域
本发明涉及一种遥控飞机，特别涉及一种具有状态监控功能的遥控飞机。
背景技术
遥控飞机是可以远距离控制飞行的飞行器。遥控飞机通常由置于遥控飞机内部的电池作为能源驱动电机而飞行。电机的温度会随着电机的运转而上升，过高的温度会损坏电机。电池的电量会随着电机的运转而下降，若电池电量过低而无法向电机提供足够的电量，飞行中的遥控飞机会下坠而损坏。但是现有的遥控飞机不具有状态监控功能，在飞行过程中不能监控遥控飞机各个部件的状态，因此不能对电池电量过低或电机温度过高等情况作出预先判断和迅速反应，由此而造成的遥控飞机损坏率较高。
发明内容
本发明的目的是克服现有技术的缺陷，提供一种具有状态监控功能的遥控飞机，能够监控遥控飞机的状态，从而降低遥控飞机的损坏率。
本发明通过下述方案达到上述目的：
一种具有状态监控功能的遥控飞机，由含有信号收发器飞机端的遥控飞机和含有信号收发器遥控端的遥控器组成，遥控飞机上设置有由电池提供能源的电机，遥控飞机上设置有传感器组件，传感器组件将遥控飞机的状态信息传送至信号收发器飞机端，再发送至信号收发器遥控端。
上述信号收发器飞机端和信号收发器遥控端直接利用原本遥控飞机的 RF （即射频，下同）信号收发装置，无需额外添加改造。此 RF 信号收发装置融合 RF 信号接收器和发射器为一体，具体为 RF 接收器和发射器共用一个 RF 芯片，具备双向数据无线传输的能力。
所述传感器组件可以包括电能传感器，此时所述的状态信息为电池的电量，还可以进一步包括电池的电压、电流等信息；所述传感器组件还包括温度传感器，此时所述的状态信息为电机的温度。此外传感器组件还可以包括位置传感器（经度、纬度等）、高度传感器、转速传感器等传感器或 GPS 模块等，可以根据需求进行添加，相应传递的状态信息可以包括电机转速或 GPS 数据（经度、纬度、高度等）。
进一步地，遥控器上还可以设置有显示装置，显示装置显示信号接收器接收到的状态信息，例如显示电池电量、电机温度或其他状态信息。
进一步地，遥控器上还可以设置有报警装置，当信号接收器接收到的状态信息超出设定范围时，发出警报。例如，当信号接收器接收到的电池的电量低于设定值，或者电机的温度高于设定值时，都可以发出警报。
本发明与现有技术相比，有以下优点：
（ 1 ）通过接收到的状态信息，可以随时了解遥控飞机的状态如温度、电量等，对遥控飞机的飞行状态做出预判；
（ 2 ）当遥控飞机的状态异常，比如温度过高或电量过低时，可以发出警报，从而避免遥控飞机的损坏；
（ 3 ） RF 接收器和发射器共用一个 RF 芯片。 接收、遥测、调速、混控、六轴平衡控制 ( 含陀螺 ) 的五合一控制盒可一体化设计； 具有体格小、重量轻的优点。
附图说明
图 1 ：本发明的功能模块示意图。
具体实施方式
实施例 1
以下结合图 1 对本发明作进一步说明。
一种具有状态监控功能的遥控飞机，由含有信号收发器飞机端 10 的遥控飞机 1 和含有信号收发器遥控端 20 的遥控器 2 组成，遥控飞机 1 上设置有由电池 11 提供能源的电机 12 ，遥控飞机 1 上设置有传感器组件 100 ，传感器组件 100 将遥控飞机 1 的状态信息传送至信号收发器飞机端 10 ，再发送至信号收发器遥控端 20 。
所述传感器组件 100 包括电能传感器 110 和温度传感器 120 ，分别传递电池 11 的电量和电机 12 的温度等状态信息。
遥控器 2 上设置有显示装置 21 ，显示信号收发器遥控端 20 接收到的电池 11 电量或电机 12 温度等状态信息。
遥控器 2 上设置有报警装置 22 ，当信号收发器遥控端 20 接收到的电池 11 的电量低于设定值，或者电机 12 的温度高于设定值时，发出警报。

Claims (10)

  1. 一种具有状态监控功能的遥控飞机，由含有信号收发器飞机端（ 10 ）的遥控飞机（ 1 ）和含有信号收发器遥控端（ 20 ）的遥控器（ 2 ）组成，遥控飞机（ 1 ）上设置有由电池（ 11 ）提供能源的电机（ 12 ），其特征在于遥控飞机（ 1 ）上设置有传感器组件（ 100 ），传感器组件（ 100 ）将遥控飞机（ 1 ）的状态信息传送至信号收发器飞机端（ 10 ），再发送至信号收发器遥控端（ 20 ）。
  2. 如权利要求 1 所述的具有状态监控功能的遥控飞机，其特征在于所述传感器组件（ 100 ）包括电能传感器（ 110 ），所述的状态信息为电池（ 11 ）的电量 。
  3. 如权利要求 1 所述的具有状态监控功能的遥控飞机，其特征在于所述传感器组件（ 100 ）包括温度传感器（ 120 ），所述的状态信息为电机（ 12 ）的温度。
  4. 如权利要求 1~3 中任一项所述的具有状态监控功能的遥控飞机，其特征在于遥控器（ 2 ）上还设置有显示装置（ 21 ），显示装置（ 21 ）显示信号收发器遥控端（ 20 ）接收到的状态信息。
  5. 如权利要求 1 所述的具有状态监控功能的遥控飞机，其特征在于遥控器（ 2 ）上还设置有报警装置（ 22 ），当信号收发器遥控端（ 20 ）接收到的状态信息超出设定范围时，发出警报。
  6. 如权利要求 2 所述的具有状态监控功能的遥控飞机，其特征在于遥控器（ 2 ）上还设置有报警装置（ 22 ），当信号收发器遥控端（ 20 ）接收到的电池（ 11 ）的电量低于设定值时，发出警报。
  7. 如权利要求 3 所述的具有状态监控功能的遥控飞机，其特征在于遥控器（ 2 ）上还设置有报警装置（ 22 ），当信号收发器遥控端（ 20 ）接收到的电机（ 12 ）的温度高于设定值时，发出警报。
  8. 如权利要求 1 所述的具有状态监控功能的遥控飞机，其特征在于所述的信号收发器飞机端（ 10 ）和信号收发器遥控端（ 20 ）均为融合 RF 信号接收器和发射器为一体的装置。
  9. 如权利要求 1 所述的具有状态监控功能的遥控飞机，其特征在于所述的传感器组件（ 100 ）还包括位置传感器、高度传感器、转速传感器、 GPS 模块中的一种或多种；所述的状态信息还包括电机转速、经度、纬度、高度中的一种或多种。
  10. 如权利要求 3 所述的具有状态监控功能的遥控飞机，其特征在于所述的状态信息还包括电池（ 11 ）的电压或电流。
PCT/CN2012/072489 2012-03-16 2012-03-16 一种具有状态监控功能的遥控飞机 WO2013134962A1 (zh)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016154977A1 (zh) * 2015-04-01 2016-10-06 尚平 一种飞行器
CN106707192A (zh) * 2017-01-23 2017-05-24 深圳市哈威飞行科技有限公司 飞行器安全检测管理装置及安全控制系统

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19502713A1 (de) * 1994-09-02 1996-03-14 Markus Lisken Vorrichtung zur Meßwertübertragung bei funkferngesteuerten Modellen
US20080014826A1 (en) * 2006-07-12 2008-01-17 Tomy Company, Ltd. Aircraft toy
CN102120088A (zh) * 2011-01-28 2011-07-13 深圳市格兰之特科技有限公司 一种飞行玩具状态检测与安全控制的系统与方法
CN102139164A (zh) * 2011-01-28 2011-08-03 深圳市格兰之特科技有限公司 一种自动规避障碍物的飞行装置与方法
CN102614672A (zh) * 2012-03-16 2012-08-01 罗之洪 一种具有状态监控功能的遥控飞机

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19502713A1 (de) * 1994-09-02 1996-03-14 Markus Lisken Vorrichtung zur Meßwertübertragung bei funkferngesteuerten Modellen
US20080014826A1 (en) * 2006-07-12 2008-01-17 Tomy Company, Ltd. Aircraft toy
CN102120088A (zh) * 2011-01-28 2011-07-13 深圳市格兰之特科技有限公司 一种飞行玩具状态检测与安全控制的系统与方法
CN102139164A (zh) * 2011-01-28 2011-08-03 深圳市格兰之特科技有限公司 一种自动规避障碍物的飞行装置与方法
CN102614672A (zh) * 2012-03-16 2012-08-01 罗之洪 一种具有状态监控功能的遥控飞机

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016154977A1 (zh) * 2015-04-01 2016-10-06 尚平 一种飞行器
CN106707192A (zh) * 2017-01-23 2017-05-24 深圳市哈威飞行科技有限公司 飞行器安全检测管理装置及安全控制系统

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