CN102614672B - Remote control aircraft with state monitoring function - Google Patents
Remote control aircraft with state monitoring function Download PDFInfo
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- CN102614672B CN102614672B CN201210070248.6A CN201210070248A CN102614672B CN 102614672 B CN102614672 B CN 102614672B CN 201210070248 A CN201210070248 A CN 201210070248A CN 102614672 B CN102614672 B CN 102614672B
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- remote control
- aircraft
- signal transceiver
- telecontrolled aircraft
- monitoring function
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Abstract
The invention discloses a remote control aircraft with a state monitoring function. The remote control aircraft comprises a remote control aircraft and a remote controller, wherein the remote control aircraft includes a signal transceiver aircraft end; the remote controller includes a signal transceiver remote control end; a motor supplied with energy by a battery is arranged on the remote control aircraft; a sensor module is arranged on the remote control aircraft; and the state information of the remote control aircraft is transmitted to the signal transceiver aircraft end by the sensor module and then transmitted to the signal transceiver remote control end. By using the received state information, the state of the remote control aircraft, such as temperature, electric quantity and the like, can be understood at any time so that anticipation judgment is made on the flying state of the remote control aircraft; and an alarm can be also made if necessary so as to avoid the damage of the remote control aircraft.
Description
Technical field
The present invention relates to a kind of telecontrolled aircraft, particularly a kind of telecontrolled aircraft with condition monitoring function.
Background technology
Telecontrolled aircraft be can far distance controlled flight aircraft.Telecontrolled aircraft is flown as driven by energy motor by the battery being placed in telecontrolled aircraft inside usually.The temperature of motor can rise along with the running of motor, and too high temperature can damage motor.The electricity of battery can decline along with the running of motor, if battery electric quantity is too low and cannot provide enough electricity to motor, aloft telecontrolled aircraft can drop and damage.But existing telecontrolled aircraft does not have condition monitoring function, the state of telecontrolled aircraft all parts can not be monitored in flight course, therefore too low or motor temperature can not cross high situation and make and prejudge and react rapidly battery electric quantity, the telecontrolled aircraft spoilage caused therefrom is higher.
Summary of the invention
The object of the invention is the defect overcoming prior art, a kind of telecontrolled aircraft with condition monitoring function is provided, the state of telecontrolled aircraft can be monitored, thus reduce the spoilage of telecontrolled aircraft.
The present invention is achieved the above object by following proposal:
A kind of telecontrolled aircraft with condition monitoring function, be made up of the telecontrolled aircraft containing signal transceiver aircraft end and the remote controller containing signal transceiver remote control end, telecontrolled aircraft is provided with the motor that the energy is provided by battery, telecontrolled aircraft is provided with sensor cluster, the status information of telecontrolled aircraft is sent to signal transceiver aircraft end by sensor cluster, then is sent to signal transceiver remote control end.
Above-mentioned signal transceiver aircraft end and signal transceiver remote control end directly utilize RF(and the radio frequency of telecontrolled aircraft originally, lower same) signal receiving/transmission device, without the need to additionally adding transformation.This RF signal receiving/transmission device merges RF signal receiver and transmitter is integrated, and is specially RF receiver and the shared RF chip of transmitter, possesses the ability of bi-directional data wireless transmission.
Described sensor cluster can comprise electrical power sensor, and now described status information is the electricity of battery, can further include the information such as the voltage of battery, electric current; Described sensor cluster also comprises temperature sensor, and now described status information is the temperature of motor.In addition sensor cluster can also comprise sensor or the GPS module etc. such as position sensor (longitude, latitude etc.), height sensor, speed probe, can add according to demand, the status information of corresponding transmission can comprise motor speed or gps data (longitude, latitude, height etc.).
Further, remote controller can also be provided with display unit, the status information that display unit display receiver receives, such as, show battery electric quantity, motor temperature or other status informations.
Further, remote controller can also be provided with warning device, when the status information that signal receiver receives exceeds setting range, give the alarm.Such as, the electricity of the battery received when signal receiver lower than setting value, or the temperature of motor higher than setting value time, can give the alarm.
The present invention compared with prior art, has following advantage:
(1) status information by receiving, can understand the state of telecontrolled aircraft at any time as temperature, electricity etc., make anticipation to the state of flight of telecontrolled aircraft;
(2) when the abnormal state of telecontrolled aircraft, when such as temperature is too high or electricity is too low, can give the alarm, thus avoid the damage of telecontrolled aircraft;
(3) RF receiver and transmitter share a RF chip.Reception, remote measurement, speed governing, mixing, six spindle balances control the five in one control box of (containing gyro) can integrated design; There is little, the lightweight advantage of physique.
Accompanying drawing explanation
Fig. 1: high-level schematic functional block diagram of the present invention.
Detailed description of the invention
embodiment 1
Below in conjunction with Fig. 1, the invention will be further described.
A kind of telecontrolled aircraft with condition monitoring function, be made up of the telecontrolled aircraft 1 containing signal transceiver aircraft end 10 and the remote controller 2 containing signal transceiver remote control end 20, telecontrolled aircraft 1 is provided with the motor 12 that the energy is provided by battery 11, telecontrolled aircraft 1 is provided with sensor cluster 100, the status information of telecontrolled aircraft 1 is sent to signal transceiver aircraft end 10 by sensor cluster 100, then is sent to signal transceiver remote control end 20.
Described sensor cluster 100 comprises electrical power sensor 110 and temperature sensor 120, transmits the status information such as the electricity of battery 11 and the temperature of motor 12 respectively.
Remote controller 2 is provided with display unit 21, the status informations such as battery 11 electricity that display transceiver remote control end 20 receives or motor 12 temperature.
Remote controller 2 is provided with warning device 22, the electricity of the battery 11 received when signal transceiver remote control end 20 lower than setting value, or the temperature of motor 12 higher than setting value time, give the alarm.
Claims (4)
1. one kind has the telecontrolled aircraft of condition monitoring function, be made up of the telecontrolled aircraft (1) containing signal transceiver aircraft end (10) and the remote controller (2) containing signal transceiver remote control end (20), telecontrolled aircraft (1) is provided with the motor (12) that the energy is provided by battery (11), it is characterized in that telecontrolled aircraft (1) is provided with sensor cluster (100), the status information of telecontrolled aircraft (1) is sent to signal transceiver aircraft end (10) by sensor cluster (100), then is sent to signal transceiver remote control end (20); Described sensor cluster (100) comprises electrical power sensor (110) and temperature sensor (120), and described status information is the electricity of battery (11) and the temperature of motor (12); Remote controller (2) is also provided with display unit (21) and warning device (22), the status information that display unit (21) display transceiver remote control end (20) receives;
Remote controller (2) is also provided with warning device (22), when the electricity of the battery (11) that signal transceiver remote control end (20) receives is lower than setting value, gives the alarm; Or when the temperature of the motor (12) that signal transceiver remote control end (20) receives is higher than setting value, give the alarm.
2. there is the telecontrolled aircraft of condition monitoring function as claimed in claim 1, it is characterized in that described signal transceiver aircraft end (10) and signal transceiver remote control end (20) are the device merging RF signal receiver and transmitter and be integrated.
3. there is the telecontrolled aircraft of condition monitoring function as claimed in claim 1, it is characterized in that described sensor cluster (100) also comprises in position sensor, height sensor, speed probe, GPS module one or more; Described status information also comprise in motor speed, longitude, latitude, height one or more.
4. there is the telecontrolled aircraft of condition monitoring function as claimed in claim 1, it is characterized in that described status information also comprises voltage or the electric current of battery (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210070248.6A CN102614672B (en) | 2012-03-16 | 2012-03-16 | Remote control aircraft with state monitoring function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210070248.6A CN102614672B (en) | 2012-03-16 | 2012-03-16 | Remote control aircraft with state monitoring function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102614672A CN102614672A (en) | 2012-08-01 |
| CN102614672B true CN102614672B (en) | 2015-07-08 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201210070248.6A Active CN102614672B (en) | 2012-03-16 | 2012-03-16 | Remote control aircraft with state monitoring function |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013134962A1 (en) * | 2012-03-16 | 2013-09-19 | Luo Zhihong | Remote controlled aircraft with state monitoring function |
| CN103657110A (en) * | 2013-12-15 | 2014-03-26 | 苏州市峰之火数码科技有限公司 | Remote control aircraft toy |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201551845U (en) * | 2009-09-05 | 2010-08-18 | 魏承赟 | Flight assisting system for model airplane with fixed wings |
| CN202044782U (en) * | 2010-12-22 | 2011-11-23 | 曹权亮 | Machine flying man |
| CN202460124U (en) * | 2012-03-16 | 2012-10-03 | 罗之洪 | Remote control aircraft with state monitoring function |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE29701669U1 (en) * | 1997-01-31 | 1997-04-17 | Gärtner, Richard, Dipl.-Ing. (FH), 86647 Buttenwiesen | Electronic speed controller for electric drive motors in radio-controlled flight, ship and vehicle models |
| JP2001209427A (en) * | 2000-01-28 | 2001-08-03 | Fuji Heavy Ind Ltd | Remote controller for unmanned airplane |
| CN201871239U (en) * | 2010-10-15 | 2011-06-22 | 北京工业大学 | Steering engine driver of intelligent robot |
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2012
- 2012-03-16 CN CN201210070248.6A patent/CN102614672B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201551845U (en) * | 2009-09-05 | 2010-08-18 | 魏承赟 | Flight assisting system for model airplane with fixed wings |
| CN202044782U (en) * | 2010-12-22 | 2011-11-23 | 曹权亮 | Machine flying man |
| CN202460124U (en) * | 2012-03-16 | 2012-10-03 | 罗之洪 | Remote control aircraft with state monitoring function |
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| CN102614672A (en) | 2012-08-01 |
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Effective date of registration: 20170327 Address after: 511475 Nansha District, Guangdong, Tung Chung Town, Tai Po Industrial Zone Patentee after: Guangzhou city huakeer Polytron Technologies Inc Address before: Guangdong city of Guangzhou province Panyu District 511430 Guangzhou Walkera Technology Co Ltd yuwotou Taishi Industrial Zone Patentee before: Luo Zhihong |