Energy-saving and environmentally-friendly non-battery-powered electric aircraft

Abstract

An energy-saving and environmental-friendly non-battery-powered electric aircraft, comprising a fuselage (5), a control mechanism (10), at least one class-I energy-saving and environmental-friendly hybrid generator set device (30), power supply switches (31), an accelerator (40), a controller (50), motors (60) of power systems, motors (110), transmission systems (70), transmission systems (120), aircraft wheels (130), controllable pitch propellers (80), flaps (90), slats (210), and turbofan jet engines (200). The energy-saving and environmental-friendly hybrid generator set device (30) comprises a wind power generation device that is provided with an impeller (11), a main shaft (12), a speed increaser (13), a brake (14), and a power generator (15); an electric power generation device is provided in the wind power generation device; the electric power generation device comprises a storage battery (16), a switch (17), a reverse current protection controller (18) for protecting the storage battery, a motor (19) mounted on a main shaft of the power generator, a feedback power supply control box (20), a switch (21), an automatic charging controller (22), and a charging port (23); the motor (19) is mounted on the main shaft of the power generator; the storage battery (16) is connected and supplies power to a power-using end of the motor (19) by means of the switch (17) and the reverse current protection controller (18); the generator set is started to generate power, a power output end is provided with at least one electric energy output member that is separately connected and supplies power to the feedback power supply control box (20) and the automatic charging controller (22), and the other electric energy output members supply power to an electrical system of the aircraft; the feedback power supply control box (20) regulates portion of electric energy and feeds same back to the motor (19) for power supply, and the automatic charging controller (22) controls portion of electric energy to automatically charge the storage battery (16) by means of the charging port (23); when the feedback power supply control box (20) performs feedback power supply, the switch of the storage battery (16) is turned off, and the motor (19) continues to drive the main shaft (12) of the power generator, the speed increaser (13), and a shaft of the power generator (15) to rotate so as to generate power; when the generator set device (30) supplies power to the electrical system of the aircraft by means of the power supply switches (31), the control mechanism (10), the accelerator (40) and the controller (50) are used to control the propeller motors (60), the transmission systems (70), the controllable pitch propellers (80), the aircraft wheel motors (110), the transmission systems (120), and the aircraft wheels (130), thereby causing the aircraft to take off, and meanwhile, the turbines of the turbofan jet engines rotate under the action of airflow generated during takeoff of the aircraft, absorb air to generate air pressure, and eject the air by means of jet nozzles so as to propel the aircraft to take off; when a wind force generated during takeoff reaches a certain value, the impeller (11) rotates under the action of the wind force generated during takeoff of the aircraft and drives the main shaft (12), the speed increaser (13), and the shaft of the power generator (15) to rotate so as to generate power, thereby supplying power to the aircraft; when a flight speed is low and the generated wind force is insufficient, an electric power generation system is started to generate power, and electric power generation and wind power generation are cyclically performed to supply power to the aircraft. Therefore, the present utility model is energy-saving and environmentally-friendly.

Description

Energy-saving and environmentally friendly non-battery electric aircraft Technical Field

[0001] This utility model relates to an electric-powered aircraft, and more particularly to an energy-saving and environmentally friendly non-battery-powered electric-powered aircraft. Background Technology

[0002] As is well known, non-fuel electric aircraft are more energy-efficient, environmentally friendly, and cheaper than fuel-powered aircraft. Compared with battery-powered aircraft, they have higher energy and greater power, and their power generation is not affected by temperature, thus avoiding range and fuel issues. Therefore, the core of this technology is to use energy-efficient and environmentally friendly hybrid generator sets to power various aircraft. In order to solve the pollution and energy problems caused by aircraft engine fuel, it is necessary to use energy-efficient and environmentally friendly hybrid generator sets to power various aircraft. Summary of the Invention

[0003] The technical problem to be solved by this utility model is to provide power to various aircraft by using the electrical energy of energy-saving and environmentally friendly hybrid generator sets, and to provide an energy-saving and environmentally friendly non-battery electric power aircraft.

[0004] Technical solutions to the above problems:

[0005] An energy-saving and environmentally friendly non-battery electric-powered aircraft includes: an aircraft body, a control system, an accelerator, a controller, a power system motor, a transmission system, an adjustable pitch propeller, a turbofan jet, slats, flaps, aircraft wheels, an auxiliary system, at least one stage of an energy-saving and environmentally friendly hybrid generator set, a power switch, wiring, etc. The auxiliary system includes: an auxiliary power supply, air conditioning, lighting, a defrosting device, etc. The energy-saving and environmentally friendly hybrid generator set includes a wind power generation device and an electric power generation device. The wind power generation device includes: an impeller, a main shaft, a speed increaser, a brake, a generator, etc. The impeller uses the wind power generated by the aircraft's flight to drive the speed increaser and generator shaft to rotate and generate electricity. An electric power generation device is installed within the wind power generation device, including: a battery and a switching device, a reverse controller for battery protection, a motor, a control box and switching device for feedback power supply, an automatic charging controller, and a charging port. The energy-saving and environmentally friendly hybrid generator set is powered by the battery through the switch and reverse... The controller starts the generator set to generate electricity, and the motor drives the generator shaft to rotate and generate electricity. There is at least one electrical output at the generator output terminal, which is connected to the control box for feedback power supply and the controller for automatic charging and supply power respectively. After feedback power supply, the battery switch is turned off, the generator set continues to generate electricity, and other electrical energy is output. Power is supplied to the aircraft through the power switch. After power is supplied, the control mechanism, accelerator and controller control the motor of the power system to drive the transmission system, aircraft wheels and adjustable pitch propeller to take off. At the same time, the turbofan jet uses the wind power generated when the aircraft takes off to rotate and compress air and jet, which helps the aircraft take off and fly. At the same time, when the aircraft takes off at a certain speed, the impeller uses the wind power generated when the aircraft takes off to rotate and drive the generator main shaft, speed increaser and generator shaft to rotate and generate electricity. The electricity generated by wind power supplies the aircraft with power. When the wind is insufficient, the electric power generation system starts to generate electricity to supply the aircraft. Electricity and wind power are circulated to generate electricity to supply the aircraft's electrical system.

[0006] Furthermore, the battery is connected to the on end of the reverse controller via a switching device, and the off end of the reverse controller is connected to the power consumption end of the motor.

[0007] Furthermore, the motor is mounted on the generator main shaft, and the motor shaft is connected to the main shaft.

[0008] Furthermore, the electrical input terminal of the feedback power supply control box is connected to the generator output terminal, and the electrical output terminal of the feedback power supply control box is connected to the motor's power consumption terminal via a switch. The control box collects a portion of the electrical energy and supplies it to the motor via a feedback switch.

[0009] Furthermore, the electrical input terminal of the automatic charging controller is connected to the generator output terminal, the electrical output terminal of the automatic charging controller is connected to the charging port, and the other end of the charging port is connected to the battery. The automatic charging controller controls a portion of the electrical energy to automatically charge the battery.

[0010] By adopting the above technical solution, the beneficial technical effects of this utility model are as follows:

[0011] This energy-saving and environmentally friendly non-battery electric aircraft eliminates the need for refueling, eliminates range anxiety, and saves time, money, and energy.

[0012] By using a hybrid generator set that combines electric and wind power to generate electricity, various aircraft electrical systems are supplied with power. This method is energy-efficient and environmentally friendly. Furthermore, the inclusion of a feedback power supply device and an automatic charging device in the generator set solves the problems of range anxiety and downtime charging. Attached Figure Description

[0013] Figure 1 is a simplified structural diagram of the energy-saving and environmentally friendly non-battery electric-powered aircraft of this utility model.

[0014] Figure 2 is a schematic diagram of the energy-saving and environmentally friendly hybrid generator set shown in Figure 1. Detailed Implementation

[0015] The present invention will be further described in detail below through specific embodiments and with reference to the accompanying drawings.

[0016] Example 1

[0017] An energy-saving and environmentally friendly non-battery electric-powered aircraft, as shown in Figures 1 and 2, includes an aircraft body 5, a control mechanism 10, an energy-saving and environmentally friendly hybrid generator set 30 (A, B), a power switch 31 (a, b), an accelerator 40, a controller 50, a motor 60 (a, b) driving the propeller, a transmission system 70 (a, b), an adjustable pitch propeller 80 (a, b), a turbofan jet 200 (A, B), flaps 90 (a, b), slats 210 (a, b), an aircraft wheel motor 110 (a, b), and a transmission system. 120 (a, b), aircraft wheels 130 (a, b, c, d, e), the energy-saving and environmentally friendly hybrid generator set 30 includes a wind power generation device: impeller 11, main shaft 12, speed increaser 13, brake 14, generator 15, etc. The impeller 11 uses the wind power generated during takeoff to rotate and drive the shafts of the main shaft 12, speed increaser 13, and generator 15 to rotate and generate electricity. An electric power generation device is installed in the wind power generation device, the electric power generation device including: a battery 16 and a switching device 17, a reverse controller 18 to protect the battery, and installed on... The generator main shaft includes a motor 19, a feedback power supply control box 20 and a switch device 21, an automatic charging controller 22, and a charging port 23. The shaft of the motor 19 is connected to the main shaft 12. The battery 16 is connected to the power consumption terminal of the motor 19 through a switch 17 and a reverse controller 18 to supply power. The input terminal of the feedback power supply control box 20 is connected to the power output terminal of the generator 15. The output terminal of the feedback power supply control box 20 is connected to the power consumption terminal of the motor 19 through a switch 21 to provide feedback power. The automatic charging controller 22... The input terminal is connected to the output terminal of the generator 15. The output terminal of the automatic charging controller 22 is connected to the storage battery 16 through the charging port 23 and automatically charges. The storage battery 16 starts the motor 19 through the switch 17 and the reverse controller 18. The motor 19 drives the shaft of the speed increaser 13 and the generator 15 to rotate and generate electricity. After generating electricity, part of the electrical energy in the control box 20 is organized and fed back to the motor 19 through the switch 21. After the feedback power supply, the motor 19 continues to drive the main shaft 12 to rotate and generate electricity, and the switch 17 of the storage battery is turned off.Two generator sets 30 are installed on the two wings. The electrical energy generated by the generator sets 30 is supplied through the power switch 31. After power is supplied, the control mechanism 10, accelerator 40 and controller 50 control the motors 60 (a, b) of the power system to drive the transmission system 70 (a, b), the adjustable pitch propeller 80 (a, b), the aircraft wheel motor 110 (a, b), the transmission system 120 (a, b), and the aircraft wheels 130 (a, b, c, d, e) to take off. At the same time, the turbine of the turbofan jet uses the wind power generated during takeoff to rotate and absorb gas to generate air pressure. The gas is then expelled through the nozzle to propel the aircraft for takeoff and flight. When the wind power generated during takeoff reaches a certain value, the impeller 11 drives the shaft of the speed increaser 13 and the generator 15 to rotate and generate electricity. The wind power supplies the aircraft's electrical system. When the wind power generated during flight is insufficient, the electric power generation system automatically starts generating electricity. Electricity and wind power are cyclically generated, saving energy and protecting the environment.

[0018] It should be noted that the above content is a further detailed description of the present utility model in conjunction with specific embodiments, and it should not be considered that the specific implementation of the present utility model is limited to these descriptions. For example, the motor installed on the generator main shaft can be installed after the speed increaser and connected to the shaft of the generator 15. The generator set can generate electricity in two stages, three stages, etc., and amplify electrical energy. The switch can be a remote control switch, a smart switch, etc. The impeller can be an adjustable blade pitch impeller. The motor installed on the generator main shaft can be an AC motor. If the speed of the impeller is sufficient, the speed increaser is not required. Multiple jet engines can be installed. The jet engines can be electric jet engines, etc. For those skilled in the art, several simple deductions or substitutions can be made without departing from the concept of the present utility model, and all of these should be considered to fall within the protection scope of the present utility model.

Claims

1. An energy-saving and environmentally friendly non-battery electric-powered aircraft, comprising: The aircraft comprises an airframe, control system, accelerator, controller, power system motor, transmission system, adjustable pitch propeller, turbofan jet, slats, flaps, aircraft wheels, auxiliary system, at least one level of energy-saving and environmentally friendly hybrid generator set, power switch, and wiring. The auxiliary system includes: auxiliary power supply, power steering system, air conditioning, lighting, defrosting device, windshield wipers, etc. The energy-saving and environmentally friendly hybrid generator set includes wind power generation device and electric power generation device. The characteristic feature is that the power source of the energy-saving and environmentally friendly non-battery electric power aircraft is the energy-saving and environmentally friendly hybrid generator set.

2. The energy-saving and environmentally friendly non-battery electric-powered aircraft according to claim 1, characterized in that: The energy-saving and environmentally friendly hybrid generator set generates electricity and wind power in a cycle. The wind power generation device includes: impeller, main shaft, speed increaser, brake, generator, etc. The impeller rotates under the action of the wind force generated when the aircraft takes off, which drives the speed increaser and generator shaft to rotate and generate electricity.

3. The energy-saving and environmentally friendly non-battery electric-powered aircraft according to claim 2, characterized in that: Electricity generation devices are installed in wind power generation systems.

4. The energy-saving and environmentally friendly non-battery electric-powered aircraft according to claim 3, characterized in that: The power generation device includes: at least one motor, a battery and a switching device, and a reverse controller for protecting the battery, all mounted on the generator main shaft. The battery is connected to the power consumption terminal of the motor via the switch and the reverse controller to start the generator set and generate electricity.

5. The energy-saving and environmentally friendly non-battery electric-powered aircraft according to claim 4, characterized in that: A feedback power supply device and an automatic charging device are installed in the power generation unit. After the battery starts the generator set to generate electricity, at least one electrical energy is output from the generator output terminal, which is connected to and supplies power to the feedback power supply control box and the automatic charging controller, respectively. The other electrical energy output supplies power to the aircraft's electrical system. A portion of the electrical energy in the feedback power supply control box is connected to the motor's power terminal through a feedback switch and fed back to the system. After the feedback power supply is completed, the battery switch is turned off, and the motor continues to drive the speed increaser and generator shaft to rotate and generate electricity. The energy-saving and environmentally friendly hybrid generator set is installed on the aircraft wing. The generator set outputs electrical energy through a switch to supply power to the aircraft's electrical system. After power is supplied, the accelerator and controller control the electric motor of the power system to drive the transmission system and the adjustable pitch propeller to take off. At the same time, the turbine of the turbofan jet uses the wind generated during takeoff to rotate, absorb gas and generate air pressure. The air pressure is ejected from the nozzle, and the reaction force propels the aircraft to take off and fly. When the wind generated during takeoff reaches a certain value, the impeller of the generator set uses the wind power to rotate and drive the speed increaser and generator shaft to rotate to generate electricity, which supplies power to the aircraft's electrical system. When the wind power generated at low flight speed is insufficient, the power generation system starts to generate electricity. Electricity and wind power are circulated to generate electricity to supply power to the aircraft's electrical system, which is energy-saving and environmentally friendly.

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