CN108622393A - A kind of multiple-energy-source fusion aircraft and its control method - Google Patents
A kind of multiple-energy-source fusion aircraft and its control method Download PDFInfo
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- CN108622393A CN108622393A CN201810444597.7A CN201810444597A CN108622393A CN 108622393 A CN108622393 A CN 108622393A CN 201810444597 A CN201810444597 A CN 201810444597A CN 108622393 A CN108622393 A CN 108622393A
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- 238000000034 method Methods 0.000 title claims abstract description 35
- 230000004927 fusion Effects 0.000 title claims abstract description 19
- 239000002828 fuel tank Substances 0.000 claims abstract description 29
- 230000005520 electrodynamics Effects 0.000 claims abstract description 10
- 230000005611 electricity Effects 0.000 claims description 18
- 238000001514 detection method Methods 0.000 claims description 16
- 239000000446 fuel Substances 0.000 claims description 14
- 230000009471 action Effects 0.000 claims description 10
- 230000001276 controlling effect Effects 0.000 claims description 6
- 230000006870 function Effects 0.000 claims description 5
- 230000005484 gravity Effects 0.000 claims description 3
- 230000001105 regulatory effect Effects 0.000 claims description 3
- 230000008450 motivation Effects 0.000 claims 1
- 230000007812 deficiency Effects 0.000 abstract description 3
- 239000003921 oil Substances 0.000 description 16
- 238000005516 engineering process Methods 0.000 description 3
- 238000005273 aeration Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 239000011469 building brick Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000009123 feedback regulation Effects 0.000 description 1
- 239000010705 motor oil Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B2201/00—Hybrid airships, i.e. airships where lift is generated aerodynamically and statically
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
The invention discloses a kind of multiple-energy-source fusion aircraft and its control method, the multiple-energy-source fusion aircraft includes：Aircraft body, motorised units, pneumatic unit, electrodynamic element, multiple sensors and chip control module, the motorised units include fuel-flow controller, fuel tank, engine and main screw, the pneumatic unit includes the gas tank being sequentially connected, gas pressure regulator and air bag, the electrodynamic element packet electric power controller, accumulator, motor and secondary propeller, the multiple sensor is uniformly distributed in the surface of aircraft and is connected with chip control module, the chip control module be set to inside aircraft body and respectively with fuel-flow controller, electric power controller is connected with gas pressure regulator.The present invention can solve existing aircraft, and using the single energy, there are function deficiency, the low problems of control flexibility ratio.
Description
Technical field
The present invention relates to aircraft power control technology fields, and in particular to a kind of multiple-energy-source fusion aircraft and its control
Method.
Background technology
The industrial revolution of 19th century brings the huge leap forward of science and technology, and people breach the beam of air in this stage
It ties up, 1903, the Lai Te brother in the U.S. takes the lead in being manufactured that the aircraft that can be flown.Then, aircraft and relevant science skill
Art has obtained development at full speed.
Aviation aircraft is the aircraft for being operated in endoatmosphere, they produce by the relative motion of aerostatic buoyancy or air
Raw air force lift-off flight.And now aviation aircraft mostly by the single energy energy supply (such as gas internal energy, fuel chemical energy and
Electric energy), the flying instrument of single energy energy supply gradually exposes many problems, although as gas internal energy is stablized, flexibly
Spend low, volume is more huge, lacks sufficient maneuverability, action is clumsy, and it is motor-driven to be unfavorable for aircraft；Internal combustion engine chemical energy
Efficient, loading capacity is big, but control accuracy more difficult to control is low, and noise is big；Electric energy aircraft controllability is strong, but gross energy
Few, energy consumption is high, and work, cruise duration are short, and energy utilization rate is low.If various energy resources are used in mixed way, energy support construction
Diversification uses a variety of different energy supply strategies under different demands situation, the advantages of each energy is maximumlly played
Come, disadvantage avoids as far as possible, then the service ability of aircraft will obtain qualitative leap.
A kind of multiple-energy-source fusion aircraft of present invention offer and its control method, multiple-energy-source of the invention merge flying instrument
There are electrodynamic element, pneumatic unit and motorised units, can solve the problems, such as the every of the single energy, working energy form is closed
At the aircraft in the form of the more energy-efficient compound energy of acquisition.
Invention content
The purpose of the present invention is to provide a kind of multiple-energy-source fusion aircraft and its control methods, to solve existing flight
There are function deficiency, the low problems of control flexibility ratio using the single energy for device.
To achieve the above object, the technical scheme is that providing a kind of multiple-energy-source fusion aircraft, the multiple-energy-source
Merging aircraft includes：Aircraft body, motorised units, pneumatic unit, electrodynamic element, multiple sensors and chip controls mould
Block, the motorised units include fuel-flow controller, fuel tank, engine and main screw, and the fuel tank is connected with fuel-flow controller,
The fuel-flow controller provides fuel by the oil mass in regulating oil tank for engine, and the engine provides rotation for main screw
Rotation energy, the pneumatic unit includes the gas pressure regulator, gas tank and air bag being sequentially connected, and the gas pressure regulator passes through adjusting
Air pressure in the valve control air bag of gas tank, the electrodynamic element packet electric power controller, accumulator, motor and secondary propeller,
The accumulator is connected with electric power controller, and the electric power controller provides electricity by controlling the electricity of accumulator for motor
Can, the motor is that pair propeller provides rotation function, the multiple sensor be uniformly distributed in the surface of aircraft and with
Chip control module is connected, the chip control module be set to inside aircraft body and respectively with fuel-flow controller, electric power
Controller is connected with gas pressure regulator.
The aircraft body includes the first main body and the second main body, first main body as a preferred technical solution,
It is fixedly connected on the upper surface of the second main body.
The upper end centre position of first main body is provided with main screw as a preferred technical solution, and described second
The side centre position of main body is evenly arranged with multiple first connecting rods, and the end of each first connecting rod is equipped with secondary propeller.
First main body is internally provided with aircraft detection module, the aircraft as a preferred technical solution,
Detection module is connected with air bag, fuel tank, accumulator and chip control module.
The side bottom end of second main body is symmetrically arranged with multiple second connecting rods as a preferred technical solution, each
The end of second connecting rod is connected with air bag, and air bag is connected to gas tank by tracheae.
The ring-shaped gasbag that the air bag is integrally formed as a preferred technical solution, air bag are located at multiple-energy-source fusion and fly
The periphery of row device.
As a preferred technical solution, air valve and fuel tap, the air valve connection are respectively arranged on the gas tank and fuel tank
To gas pressure regulator, the fuel tap is connected to fuel-flow controller.
A kind of control method of multiple-energy-source fusion aircraft is provided, the control method includes pneumoelectric mixing control method,
The pneumoelectric mixing control method includes：It keeps the oil pump capacity of fuel tank to stablize during aircraft flight, aircraft is made steadily to fly
Row；The state of flight of aircraft is transferred to chip control module by sensor；Aircraft detection module detects gas tank gas reserves
With accumulator electric-quantity and be transferred to chip control module；Chip control module is to state of flight, gas tank gas reserves and accumulator
Electricity is analyzed, and generates distribution instruction according to the target action to be completed of aircraft；Chip control module instructs distribution
It is transferred to gas pressure regulator and electric power controller；Gas pressure regulator controls gas tank to airbag aeration, and electric power controller controls electric power storage
Pond provides power to motor makes secondary propeller rotate.
The control method further includes oily electric mixing control method as a preferred technical solution, the oil electricity mixing control
Method processed includes：The stable gas pressure that air bag is kept during aircraft flight, makes aircraft smooth flight；Sensor is by aircraft
State of flight be transferred to chip control module；The oil mass and accumulator electric-quantity of aircraft detection module detection fuel tank are simultaneously transferred to
Chip control module；Chip control module analyzes state of flight, the oil mass of fuel tank and accumulator electric-quantity, and according to flight
The target action that device to be completed generates distribution instruction；Distribution instruction is transferred to fuel-flow controller and electric power control by chip control module
Device processed；Fuel-flow controller control fuel tank changes engine oil inlet amount to change the rotating speed of main screw, and electric power controller control stores
Battery provides power to motor makes secondary propeller rotate.
The control method further includes oily electric mixing control method as a preferred technical solution, the oil electricity mixing control
Method processed includes：In flight course, keep that fuel tank fuel delivery is constant makes engine with constant speed and power continuous service；When
Aircraft need to hover or it is slow when driving, fuel-flow controller and electric power controller controls engine respectively and accumulator stops supplying
Can, gas pressure regulator controls gas tank to airbag aeration until aircraft has the lift more than its own gravity, at this point, aircraft is only
The lifting flight provided by air bag；When aircraft raises speed, gas pressure regulator controls air valve and opens, and air bag orientation is deflated as flight
Device provides the thrust advanced, and fuel-flow controller and electric power controller control engine are improved with accumulator and energized at this time, aircraft
Accelerate flight.
The invention has the advantages that：
(1) various energy resources are used in mixed way, energy support construction diversification；
(2) a variety of different energy supply strategies are used under different demands situation, and the advantages of each energy is maximumlly sent out
It shoots and；
(3) deficiency for significantly reducing single energy energy supply, can effectively arrange energy in different operating environments
Source policy adapts to flight demand；
(4) efficient, the clean utilization for realizing the energy provide huge liter to the voyage of aircraft, control etc.
Grade space.
Description of the drawings
Fig. 1 is the basic structure schematic diagram that a kind of multiple-energy-source provided by the invention merges aircraft.
Fig. 2 is the component connection diagram that a kind of multiple-energy-source provided by the invention merges aircraft.
In figure：First main body 01, the second main body 02, motorised units 03, pneumatic unit 04, electrodynamic element 05, multiple sensings
Device 06, chip control module 07, fuel-flow controller 08, fuel tank 09, engine 10, main screw 11, gas pressure regulator 12, gas tank
13, air bag 14, electric power controller 15, accumulator 16, motor 17, secondary propeller 18, aircraft detection module 19, first connecting rod
20, second connecting rod 21.
Specific implementation mode
The following examples are used to illustrate the present invention, but are not intended to limit the scope of the present invention..
Embodiment 1
The present invention provides a kind of multiple-energy-source fusion aircraft, and the multiple-energy-source fusion aircraft includes：Aircraft body, machine
Moving cell 03, pneumatic unit 04, electrodynamic element 05, multiple sensors 06 and chip control module 07, the motorised units 03 are wrapped
Fuel-flow controller 08, fuel tank 09, engine 10 and main screw 11 are included, the fuel tank 09 is connected with fuel-flow controller 08, described
Fuel-flow controller 08 is that engine 10 provides fuel by the oil mass in regulating oil tank 09, and the engine 10 is main screw 11
Rotation function is provided, the pneumatic unit 04 includes gas tank 13, gas pressure regulator 12 and the air bag 14 being sequentially connected, the air pressure
Air pressure in valve control air bag 14 of the controller 12 by adjusting gas tank 13,05 packet electric power controller 15 of the electrodynamic element,
Accumulator 16, motor 17 and secondary propeller 18, the accumulator 16 are connected with electric power controller 15, the Electric control
Device 15 is that motor 17 provides electric energy by controlling the electricity of accumulator 16, and the motor 17 is that secondary propeller 18 provides rotation
Kinetic energy, the multiple sensor 06 are uniformly distributed in the surface of aircraft and are connected with chip control module 07, the chip control
Molding block 07 be set to inside aircraft body and respectively with 12 phase of fuel-flow controller 08, electric power controller 15 and gas pressure regulator
Even.
Further, the aircraft body includes the first main body 01 and the second main body 02, and first main body 01 is fixed
It is connected to the upper surface of the second main body 02.The upper end centre position of first main body 01 is provided with main screw 11, second master
The side centre position of body 02 is evenly arranged with multiple first connecting rods 20, and the end of each first connecting rod 20 is equipped with secondary propeller
18.First main body 01 is internally provided with aircraft detection module 19, the aircraft detection module 19 and air bag 14, fuel tank
09, accumulator 16 is connected with chip control module 07.The side bottom end of second main body 02 is symmetrically arranged with multiple second connecting rods 21,
The end of each second connecting rod 21 is connected with air bag 14, and air bag 14 is connected to gas tank 13 by tracheae, wherein air bag 14 is integrated
Molding ring-shaped gasbag, the diameter of air bag 14 are more than the diameter of multiple-energy-source fusion aircraft, and air bag 14 is located at multiple-energy-source fusion and flies
The periphery of row device.
Air valve and fuel tap are respectively arranged on gas tank 13 and fuel tank 09, the air valve is connected to gas pressure regulator 12, air pressure
For controller 12 by controlling opening or close and controlling the size of air pressure in air bag 14 for air valve, the fuel tap is connected to fuel-flow controller
08, fuel-flow controller 08 by control fuel tap open or close control to oil mass number, to control the rotating speed of engine 10,
The final rotating speed for changing main screw 11.
A kind of multiple-energy-source fusion aircraft provided by the invention uses parallel type hybrid dynamic, a variety of working machines that can drive
The output of aircraft, a kind of working machine directly drives aircraft, and another kind of output is as energy supplement, i.e. principal and subordinate's energy control
Form, (such as by the not strong energy of not easy to control, realtime control：Internal combustion engine, high pressure gas holder) with valve be arranged a moderate strength
Thresholding, export metastable power, control easily controllable working machine with digital controllable switch is changed by feedback regulation
Become working machine output power, compensates the gap between thresholding and target, finally realize target action.
It can be appreciated that the energy supply duration of the response time of energy and unit mass is defined respectively, most by the response time
Short energy is as control energy, using the energy supply time of unit mass longest energy as main energy supply energy, parallel mixed
It closes in dynamical system, gives most action energy supply to main energy supply energy, give rest part to control energy, pass through work
The linear summation of effect, it is relatively high to obtain final purpose action parallel-connection type power Transmission system Energy Efficiency Ratio, advanced electronics skill
Art allows electronic building brick to play a greater role in working machine system so that various transmission components are more effectively managed, will be each
The efficient operation state of the kind energy efficiently uses, can be effective energy saving, reduces discharge.
Control method can be divided into pneumoelectric mixing control method, oil electricity mixing control according to the distribution of principal and subordinate's energy control
Method and multiple-energy-source mixing control method.
The pneumoelectric mixing control method includes：
It keeps the oil pump capacity of fuel tank 09 to stablize during aircraft flight, makes aircraft smooth flight；
The state of flight of aircraft is transferred to chip control module 07 by sensor 06；
Aircraft detection module 19 detects 13 gas reserves of gas tank and 16 electricity of accumulator and is transferred to chip control module
07；
Chip control module 07 analyzes state of flight, 13 gas reserves of gas tank and 16 electricity of accumulator, and according to
The target action that aircraft to be completed generates distribution instruction；
Distribution instruction is transferred to gas pressure regulator 12 and electric power controller 15 by chip control module 07；
Gas pressure regulator 12 controls gas tank 13 and is inflated to air bag 14, and electric power controller 15 controls accumulator 16 to motor 17
There is provided power makes secondary propeller 18 rotate.
The electric mixing control method of oil includes：
The stable gas pressure that air bag 14 is kept during aircraft flight, makes aircraft smooth flight；
The state of flight of aircraft is transferred to chip control module 07 by sensor 06；
The oil mass and 16 electricity of accumulator of the detection fuel tank 09 of aircraft detection module 19 are simultaneously transferred to chip control module 07；
Chip control module 07 analyzes the oil mass and 16 electricity of accumulator of state of flight, fuel tank 09, and according to winged
The target action that row device to be completed generates distribution instruction；
Distribution instruction is transferred to fuel-flow controller 08 and electric power controller 15 by chip control module 07；
Fuel-flow controller 08 controls fuel tank 09 and changes 10 oil inlet quantity of engine to change the rotating speed of main screw 11, electric power control
Device 15 processed controls accumulator 16 makes secondary propeller 18 rotate to the offer power of motor 17.
The multiple-energy-source mixing control method includes：In flight course, keep that 09 fuel delivery of fuel tank is constant makes engine 10
With constant speed and power continuous service；When aircraft need to hover or it is slow when driving, fuel-flow controller 08 and electric power control
Device 15 processed controls engine 10 and accumulator 16 stops energy supply, and gas pressure regulator 12 controls gas tank 13 and inflated to air bag 14 until flying
Row utensil has the lift more than its own gravity, at this point, aircraft only leans on the lifting flight that air bag 14 provides；When aircraft raises speed
When, gas pressure regulator 12 controls air valve and opens, and the orientation of air bag 14, which is deflated, provides the thrust of advance, at this time fuel-flow control for aircraft
Device 08 and electric power controller 15 control engine 10 and improve energy supply with accumulator 16, and aircraft accelerates flight.
Although above having used general explanation and specific embodiment, the present invention is described in detail, at this
On the basis of invention, it can be made some modifications or improvements, this will be apparent to those skilled in the art.Therefore,
These modifications or improvements without departing from theon the basis of the spirit of the present invention belong to the scope of protection of present invention.
Claims (10)
1. a kind of multiple-energy-source merges aircraft, which is characterized in that the multiple-energy-source merges aircraft and includes：Aircraft body, machine
Moving cell (03), pneumatic unit (04), electrodynamic element (05), multiple sensors (06) and chip control module (07), the machine
Moving cell (03) includes fuel-flow controller (08), fuel tank (09), engine (10) and main screw (11), the fuel tank (09) with
Fuel-flow controller (08) is connected, and the fuel-flow controller (08) is provided by the oil mass in regulating oil tank (09) for engine (10)
Fuel, the engine (10) are that main screw (11) provides rotation function, and the pneumatic unit (04) includes being sequentially connected
Gas pressure regulator (12), gas tank (13) and air bag (14), the valve control that the gas pressure regulator (12) passes through adjusting gas tank (13)
Air pressure in air bag (14) processed, electrodynamic element (05) the packet electric power controller (15), accumulator (16), motor (17) and pair
Propeller (18), the accumulator (16) are connected with electric power controller (15), and the electric power controller (15) is by controlling electric power storage
The electricity in pond (16) is that motor (17) provides electric energy, and the motor (17) is that secondary propeller (18) provides rotation function, institute
It states multiple sensors (06) to be uniformly distributed in the surface of aircraft and with chip control module (07) be connected, the chip controls mould
Block (07) be set to inside aircraft body and respectively with fuel-flow controller (08), electric power controller (15) and gas pressure regulator
(12) it is connected.
2. a kind of multiple-energy-source as described in claim 1 merges aircraft, which is characterized in that the aircraft body includes first
Main body (01) and the second main body (02), first main body (01) are fixedly connected on the upper surface of the second main body (02).
3. a kind of multiple-energy-source as claimed in claim 2 merges aircraft, which is characterized in that the upper end of first main body (01)
Centre position is provided with main screw (11), and the side centre position of second main body (02) is evenly arranged with multiple first and connects
The end of bar (20), each first connecting rod (20) is equipped with secondary propeller (18).
4. a kind of multiple-energy-source as claimed in claim 2 merges aircraft, which is characterized in that the inside of first main body (01)
It is provided with aircraft detection module (19), the aircraft detection module (19) and air bag (14), fuel tank (09), accumulator (16)
It is connected with chip control module (07).
5. a kind of multiple-energy-source as claimed in claim 2 merges aircraft, which is characterized in that the side of second main body (02)
Bottom end is symmetrically arranged with multiple second connecting rods (21), and the end of each second connecting rod (21) is connected with air bag (14), air bag
(14) gas tank (13) is connected to by tracheae.
6. a kind of multiple-energy-source as described in claim 1 merges aircraft, which is characterized in that the air bag (14) is integrally formed
Ring-shaped gasbag, air bag (14) be located at multiple-energy-source fusion aircraft periphery.
7. a kind of multiple-energy-source as described in claim 1 merges aircraft, which is characterized in that the gas tank (13) and fuel tank (09)
On be respectively arranged with air valve and fuel tap, the air valve is connected to gas pressure regulator (12), and the fuel tap is connected to fuel-flow controller
(08)。
8. a kind of control method of multiple-energy-source fusion aircraft as described in claim 1-7 is any, which is characterized in that the control
Method processed includes pneumoelectric mixing control method, and the pneumoelectric mixing control method includes：
It keeps the oil pump capacity of fuel tank (09) to stablize during aircraft flight, makes aircraft smooth flight；
The state of flight of aircraft is transferred to chip control module (07) by sensor (06)；
Aircraft detection module (19) detects gas tank (13) gas reserves and accumulator (16) electricity and is transferred to chip controls mould
Block (07)；
Chip control module (07) analyzes state of flight, gas tank (13) gas reserves and accumulator (16) electricity, and root
Distribution instruction is generated according to the target action to be completed of aircraft；
Distribution instruction is transferred to gas pressure regulator (12) and electric power controller (15) by chip control module (07)；
Gas pressure regulator (12) controls gas tank (13) and is inflated to air bag (14), and electric power controller (15) controls accumulator (16) to electricity
Motivation (17), which provides power, makes secondary propeller (18) rotate.
9. a kind of control method of multiple-energy-source fusion aircraft as claimed in claim 8, which is characterized in that the control method
Further include oily electric mixing control method, the electric mixing control method of oil includes：
The stable gas pressure that air bag (14) are kept during aircraft flight, makes aircraft smooth flight；
The state of flight of aircraft is transferred to chip control module (07) by sensor (06)；
The oil mass and accumulator (16) electricity of aircraft detection module (19) detection fuel tank (09) are simultaneously transferred to chip control module
(07)；
Chip control module (07) analyzes the oil mass and accumulator (16) electricity of state of flight, fuel tank (09), and according to
The target action that aircraft to be completed generates distribution instruction；
Distribution instruction is transferred to fuel-flow controller (08) and electric power controller (15) by chip control module (07)；
Fuel-flow controller (08) control fuel tank (09) changes engine (10) oil inlet quantity and changes the rotating speed of main screw (11), electricity
Force controller (15) control accumulator (16) provides power to motor (17) makes secondary propeller (18) rotate.
10. a kind of control method of multiple-energy-source fusion aircraft as claimed in claim 8, which is characterized in that the controlling party
Method includes going back multiple-energy-source mixing control method, and the multiple-energy-source mixing control method includes：In flight course, fuel tank (09) is kept
Fuel delivery is constant to make engine (10) with constant speed and power continuous service；When aircraft needs to hover or slowly travels
When, fuel-flow controller (08) and electric power controller (15) control engine (10) and accumulator (16) stopping energy supply, air pressure respectively
Controller (12) controls gas tank (13) to air bag (14) inflation until aircraft has the lift more than its own gravity, at this point, flying
Row device only leans on the lifting flight that air bag (14) provides；When aircraft raises speed, gas pressure regulator (12) controls air valve and opens, air bag
(14) orientation, which is deflated, provides the thrust of advance for aircraft, and fuel-flow controller (08) and electric power controller (15) control at this time is started
Machine (10) is improved with accumulator (16) and is energized, and aircraft accelerates flight.
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| CN201810444597.7A CN108622393A (en) | 2018-05-10 | 2018-05-10 | A kind of multiple-energy-source fusion aircraft and its control method |
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| CN201810444597.7A CN108622393A (en) | 2018-05-10 | 2018-05-10 | A kind of multiple-energy-source fusion aircraft and its control method |
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| CN206544591U (en) * | 2017-02-28 | 2017-10-10 | 南昌航空大学 | A kind of rotor dirigible of new culvert type four |
| CN206766315U (en) * | 2017-02-28 | 2017-12-19 | 南昌航空大学 | A kind of novel airbag type multi-rotor aerocraft |
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Application publication date: 20181009 |