CN107992075A - A kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane - Google Patents
A kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane Download PDFInfo
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- CN107992075A CN107992075A CN201711286770.7A CN201711286770A CN107992075A CN 107992075 A CN107992075 A CN 107992075A CN 201711286770 A CN201711286770 A CN 201711286770A CN 107992075 A CN107992075 A CN 107992075A
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- Prior art keywords
- lift
- monitoring
- control system
- data
- machine performance
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
- G07C5/0808—Diagnosing performance data
-
- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C5/00—Registering or indicating the working of vehicles
- G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
- G07C5/0841—Registering performance data
- G07C5/085—Registering performance data using electronic data carriers
Abstract
The invention belongs to unmanned air vehicle technique field, discloses a kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane, including：DC AC inverters, temperature monitoring module, rotation speed monitoring module, lift monitoring modular, dynamoelectric accelerograph system, wireless remote-control system.Lighted a fire and started using wireless remote-control system oil feeder, wireless system remote control adjustment dynamoelectric accelerograph to relevant position；By temperature monitoring system, rotational speed monitor system, lift monitoring system, which is monitored various parameters and is transmitted to computer end using wireless system, carries out data analysis.The present invention can monitor the operating status of petrol engine in real time, fill up the market vacancy so that gyroplane is preferably ensured with the operation of petrol engine.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, more particularly to a kind of oil machine performance monitoring instrument control system and method, rotation
Wing machine, unmanned plane.
Background technology
Gyroplane be it is a kind of using autorotation to produce the rotary wing aircraft of lift, be between helicopter and aircraft
Aircraft；According to the motionless propeller equipped with varying number of species, there is VTOL, can low speed low-latitude flying, simple
Lightly, easy to it is hidden the features such as.In recent years, with the maturation of gyroplane items technology, gyroplane starts to be subject to more and more
Pay attention to.For at present, gyroplane is mainly made of dynamical system, control system, execution system and fuselage etc..Gyroplane moves
Power is generally provided by lithium battery or petrol engine.With petrol engine at work, gyroplane needs dress to gyroplane
The operating status for monitor petrol engine in real time is put, flight control system judges to be according to the operating status of petrol engine
No continuation task.With the general development of unmanned plane cause.The oil machine that power is big, cruising ability is strong more and more enters people
Sight.Gradually company and individual begin attempt to voluntarily research and develop and assemble the unmanned plane using this power.And in the market is simultaneously
Without the test device of these equipment.The loss of the person and property will be brought without the blind flight of test.But at present
In the market does not have this device.
In conclusion problem existing in the prior art is：Flight control system can not be according to the fortune of petrol engine at present
Row state is to determine whether disclosure satisfy that aerial mission, it is impossible to judges the maximum lift and lift curve of the machine；It cannot monitor
Lift and rotation speed relation；The limit for reaching parameter in the air is dangerous, easily will appear from runaway condition in the air.
The content of the invention
In view of the problems of the existing technology, the present invention provides a kind of oil machine performance monitoring instrument control system and method,
Gyroplane, unmanned plane.
The present invention is achieved in that a kind of oil machine performance monitoring instrument control system, the oil machine performance monitoring instrument control system
System includes：
DC-AC inverter, the direct current for generator to be sent are converted to the alternating current that native internal module uses；It is logical
Cross conducting wire be transported to temperature monitoring module, rotation speed monitoring module, lift monitoring modular, dynamoelectric accelerograph system, wireless remote-control system,
Data computer；
Temperature monitoring module, for monitoring the running temperature of engine；Monitoring is connected with engine by temperature sensor；
Data computer is connected by 485 buses；
Rotation speed monitoring module, for monitoring the rotating speed of engine；Monitoring is connected with engine by speed probe；Pass through
485 buses connect data computer；
Lift monitoring modular, for monitoring the lift of complete machine；Monitoring is connected with complete machine by lift transducer；Pass through 485
Bus connects data computer；
Dynamoelectric accelerograph system, the control signal sent according to wireless remote-control system, passes through the oil of throttle line traffic control engine
Door size；
Wireless remote-control system, including launch and receive two parts, emitting portion is handheld device, and receiving portion is according to reception
The instruction arrived, passes through the startup and stopping of polygon control survey engine；Action message is sent to dynamoelectric accelerograph system by conducting wire；
Data computer, the various data sent by 485 bus receiving hosts；And number is analyzed by special-purpose software
According to；Provide detailed curve and analysis result.
Another object of the present invention is to provide a kind of oil machine performance monitoring of the oil machine performance monitoring instrument control system
Instrument control method, the oil machine performance monitoring instrument control method comprise the following steps：
Step 1, is lighted a fire using wireless remote-control system oil feeder and started, and wireless system remote control adjustment dynamoelectric accelerograph is to accordingly
Position；
Step 2, by temperature monitoring system, rotational speed monitor system, lift monitoring system is monitored simultaneously various parameters
Computer end, which is transmitted to, using wireless system carries out data analysis.
Further, the oil machine performance monitoring instrument control method comprises the following steps：
The various data that data computer is sent by 485 bus receiving hosts；According to the parameter being originally inputted, logarithm
According to being handled；After normal startup, rotating speed and lift data are received, lift song is provided according to different rotating speeds and lift data
Line, draws comprehensive lift curve and maximum, minimum lift；
According to curved configuration load, host monitors throttle size at the same time, provides oil mass signal by fuel tank, and detection temperature is believed
Number；Draw fuel consumption and temperature rise situation of the engine under different rotating speeds difference lift and the maximum oil consumption under limit speed
And temperature rise situation；
Optimal fuel tank, and the oil plant amount of laying down optimal during flight are configured according to experimental data recommended user.
Another object of the present invention is to provide a kind of gyroplane for being provided with the oil machine performance monitoring instrument control system.
Another object of the present invention is to provide a kind of unmanned plane for being provided with the oil machine performance monitoring instrument control system.
The present invention can monitor the operating status of petrol engine in real time, fill up the market vacancy so that gyroplane vapour
The operation of oil turbine is preferably ensured.After data computer receives data, according to data such as rotating speed, lift, temperature
Curve is drawn, provides correspondence and analysis result；Client replaces different rotors by replacing different engines；Can be with
Find most suitable system schema；Ensure flight.After test, relevant parameter is inputted in flight control system；It can be very good to control
Flight parameter processed, and the absolute rating to in-flight occurring sends early warning.
Brief description of the drawings
Fig. 1 is oil machine performance monitoring instrument control system architecture schematic diagram provided in an embodiment of the present invention；
In figure：1st, DC-AC inverter；2nd, temperature monitoring module；3rd, rotation speed monitoring module；4th, lift monitoring modular；5th, it is electric
Dynamic throttle system；6th, wireless remote-control system；7th, data computer.
Fig. 2 is oil machine performance monitoring instrument control method flow chart provided in an embodiment of the present invention.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, with reference to embodiments, to the present invention
It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to
Limit the present invention.
The present invention can monitor the operating status of petrol engine in real time, and metrical information is sent to control system, be
Gyroplane performs task and provides sound assurance.
The application principle of the present invention is explained in detail below in conjunction with the accompanying drawings.
As shown in Figure 1, oil machine performance monitoring instrument control system provided in an embodiment of the present invention includes：DC-AC inverter 1,
Temperature monitoring module 2, rotation speed monitoring module 3, lift monitoring modular 4, dynamoelectric accelerograph system 5, wireless remote-control system 6, data meter
Calculation machine 7.
DC-AC inverter 1, the direct current for generator to be sent are converted to the alternating current that native internal module uses；
Temperature monitoring module 2, rotation speed monitoring module 3, lift monitoring modular 4, dynamoelectric accelerograph system 5, wireless remote are transported to by conducting wire
Control system 6, data computer 7.
Temperature monitoring module 2, for monitoring the running temperature of engine；Prison is connected with engine by temperature sensor
Survey；Data computer is connected by 485 buses.
Rotation speed monitoring module 3, for monitoring the rotating speed of engine；Monitoring is connected with engine by speed probe；It is logical
Cross 485 buses connection data computer.
Lift monitoring modular 4, for monitoring the lift of complete machine；Monitoring is connected with complete machine by lift transducer；Pass through 485
Bus connects data computer.
Dynamoelectric accelerograph system 5, the control signal sent according to wireless remote-control system 6, passes through throttle line traffic control engine
Throttle size.
Wireless remote-control system 6, including launch and receive two parts, emitting portion are handheld device, and receiving portion is according to connecing
Received instruction, passes through the startup and stopping of polygon control survey engine；Action letter is sent to dynamoelectric accelerograph system 5 by conducting wire
Breath.
Data computer 7, the various data sent by 485 bus receiving hosts；And pass through special-purpose software.Analyze number
According to；Provide detailed curve and analysis result.
As shown in Fig. 2, oil machine performance monitoring instrument control method provided in an embodiment of the present invention comprises the following steps：
S201：Lighted a fire and started using wireless remote-control system oil feeder, wireless system remote control adjustment dynamoelectric accelerograph to corresponding positions
Put；
S202：By temperature monitoring system, rotational speed monitor system, various parameters are monitored lift monitoring system and profit
Computer end, which is transmitted to, with wireless system carries out data analysis.
Oil machine performance monitoring instrument control method provided in an embodiment of the present invention comprises the following steps：Data computer, passes through
The various data that 485 bus receiving hosts are sent；According to the parameter being originally inputted, data are handled.Normally open first
After dynamic, rotating speed and lift data are received, lift curve is provided according to different rotating speeds and lift data, draw the system synthesis
Lift curve and maximum, minimum lift.According to these curved configuration load.Host monitors throttle size at the same time, is given by fuel tank
Oil pump capacity signal, and detection temperature signal.It can draw fuel consumption and temperature rise of the engine under different rotating speeds difference lift
Situation.And maximum oil consumption and temperature rise situation under limit speed.Optimal fuel tank is configured according to experimental data recommended user, with
And the optimal oil plant amount of laying down during flight.These parameters are configured for flight control computer, and actual data are provided.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
All any modification, equivalent and improvement made within refreshing and principle etc., should all be included in the protection scope of the present invention.
Claims (5)
1. a kind of oil machine performance monitoring instrument control system, it is characterised in that the oil machine performance monitoring instrument control system includes：
DC-AC inverter, the direct current for generator to be sent are converted to the alternating current that native internal module uses；By leading
Line is transported to temperature monitoring module, rotation speed monitoring module, lift monitoring modular, dynamoelectric accelerograph system, wireless remote-control system, data
Computer；
Temperature monitoring module, for monitoring the running temperature of engine；Monitoring is connected with engine by temperature sensor；Pass through
485 buses connect data computer；
Rotation speed monitoring module, for monitoring the rotating speed of engine；Monitoring is connected with engine by speed probe；Pass through 485
Bus connects data computer；
Lift monitoring modular, for monitoring the lift of complete machine；Monitoring is connected with complete machine by lift transducer；Pass through 485 buses
Connect data computer；
Dynamoelectric accelerograph system, the control signal sent according to wireless remote-control system, the throttle by throttle line traffic control engine are big
It is small；
Wireless remote-control system, including launch and receive two parts, emitting portion be handheld device, and receiving portion is according to receiving
Instruction, passes through the startup and stopping of polygon control survey engine；Action message is sent to dynamoelectric accelerograph system by conducting wire；
Data computer, the various data sent by 485 bus receiving hosts；And data are analyzed by special-purpose software；Give
Go out detailed curve and analysis result.
2. a kind of oil machine performance monitoring instrument control method of oil machine performance monitoring instrument control system as claimed in claim 1, it is special
Sign is that the oil machine performance monitoring instrument control method comprises the following steps：
Step 1, is lighted a fire using wireless remote-control system oil feeder and started, wireless system remote control adjustment dynamoelectric accelerograph to relevant position；
Step 2, by temperature monitoring system, rotational speed monitor system, lift monitoring system is monitored and utilizes to various parameters
Wireless system is transmitted to computer end and carries out data analysis.
3. oil machine performance monitoring instrument control method as claimed in claim 2, it is characterised in that the oil machine performance monitoring instrument
Control method comprises the following steps：
The various data that data computer is sent by 485 bus receiving hosts；According to the parameter being originally inputted, to data into
Row processing；After normal startup, rotating speed and lift data are received, lift curve is provided according to different rotating speeds and lift data, is obtained
Go out comprehensive lift curve and maximum, minimum lift；
According to curved configuration load, host monitors throttle size at the same time, and oil mass signal, and detection temperature signal are provided by fuel tank；
Draw fuel consumption and temperature rise situation of the engine under different rotating speeds difference lift and under limit speed maximum oil consumption and
Temperature rise situation；
The fuel tank configured according to experimental data recommended user, and the oil plant amount of laying down during flight.
A kind of 4. gyroplane for being provided with oil machine performance monitoring instrument control system described in claim 1.
A kind of 5. unmanned plane for being provided with oil machine performance monitoring instrument control system described in claim 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711286770.7A CN107992075A (en) | 2017-12-07 | 2017-12-07 | A kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711286770.7A CN107992075A (en) | 2017-12-07 | 2017-12-07 | A kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane |
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| Publication Number | Publication Date |
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| CN107992075A true CN107992075A (en) | 2018-05-04 |
Family
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| CN201711286770.7A Pending CN107992075A (en) | 2017-12-07 | 2017-12-07 | A kind of oil machine performance monitoring instrument control system and method, gyroplane, unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114684373A (en) * | 2020-12-29 | 2022-07-01 | 中国科学院沈阳自动化研究所 | Electric multi-rotor flight state monitoring system |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0378302B1 (en) * | 1989-01-09 | 1993-03-24 | Westland Helicopters Limited | Helicopters |
| EP2517080A1 (en) * | 2009-12-21 | 2012-10-31 | The Boeing Company | Calculation and display of warning speed for thrust asymmetry control |
| CN104454188A (en) * | 2014-10-30 | 2015-03-25 | 长城汽车股份有限公司 | Gasoline injection amount control method and system for dual-fuel engine |
| CN105083588A (en) * | 2015-08-17 | 2015-11-25 | 华南农业大学 | Performance test platform and method for multi-rotor unmanned aerial vehicle |
| CN105923169A (en) * | 2016-07-06 | 2016-09-07 | 西安交通大学 | Testing platform and testing method for power supply system of gasoline-electric hybrid unmanned aerial vehicle |
| CN106005398A (en) * | 2016-05-20 | 2016-10-12 | 程靖 | Automatic matching control method for variable propeller pitch rotorcraft accelerator propeller pitch |
| CN107024310A (en) * | 2017-06-01 | 2017-08-08 | 上海未来伙伴机器人有限公司 | A kind of Power System of Flight Vehicle test device |
| CN206656739U (en) * | 2017-04-20 | 2017-11-21 | 佛山科学技术学院 | A kind of depopulated helicopter state monitoring apparatus |
-
2017
- 2017-12-07 CN CN201711286770.7A patent/CN107992075A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0378302B1 (en) * | 1989-01-09 | 1993-03-24 | Westland Helicopters Limited | Helicopters |
| EP2517080A1 (en) * | 2009-12-21 | 2012-10-31 | The Boeing Company | Calculation and display of warning speed for thrust asymmetry control |
| CN104454188A (en) * | 2014-10-30 | 2015-03-25 | 长城汽车股份有限公司 | Gasoline injection amount control method and system for dual-fuel engine |
| CN105083588A (en) * | 2015-08-17 | 2015-11-25 | 华南农业大学 | Performance test platform and method for multi-rotor unmanned aerial vehicle |
| CN106005398A (en) * | 2016-05-20 | 2016-10-12 | 程靖 | Automatic matching control method for variable propeller pitch rotorcraft accelerator propeller pitch |
| CN105923169A (en) * | 2016-07-06 | 2016-09-07 | 西安交通大学 | Testing platform and testing method for power supply system of gasoline-electric hybrid unmanned aerial vehicle |
| CN206656739U (en) * | 2017-04-20 | 2017-11-21 | 佛山科学技术学院 | A kind of depopulated helicopter state monitoring apparatus |
| CN107024310A (en) * | 2017-06-01 | 2017-08-08 | 上海未来伙伴机器人有限公司 | A kind of Power System of Flight Vehicle test device |
Non-Patent Citations (1)
| Title |
|---|
| 沈天皓: "无人涵道飞行器发动机控制系统设计与实现", 《中国优秀硕士学位论文全文数据库（电子期刊）》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114684373A (en) * | 2020-12-29 | 2022-07-01 | 中国科学院沈阳自动化研究所 | Electric multi-rotor flight state monitoring system |
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Application publication date: 20180504 |
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