Dual-motor, low energy consumption, low carbon, and plane crush resistant passenger helicopter
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A dual-power, helicopter technology, used in air transportation, rotorcraft, motor vehicles, etc., can solve the problems of slow and expensive passenger and cargo transportation in remote mountainous areas, high consumption, high pollution, high fees, and short flight distance, reducing take-off resistance. , The effect of reducing rotor load and energy consumption
Inactive Publication Date: 2014-07-02
师伟
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[0004] The existing mode of helicopter technology is advanced, but the disadvantage is that it only relies on fuel and rotors to provide power lift, the flight distance is short, high consumption, high pollution and high cost are not suitable for public passenger transportation, so that the helicopter, a convenient flying tool, can only be used in a very small range. costly use
[0006] Although the road leads to the village, due to the long distance and high cost of transportation, the transportation of passengers and goods in rural areas and remote mountainous areas is slow and expensive
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[0034] The implementation plan of the dual-power, low-consumption and low-carbon anti-air disaster passenger helicopter of this embodiment is:
[0035] exist figure 1 Among them, the body (5) is provided with solar film (2) empennage (3) rotor (4) rotor wind generator (6) lower fixed wing (7) upper fixed wing (8) middle fixed wing (9) fixed wing shaft ( 10) power cabin (11) front pull paddle (12) fixed wing hydraulic device (13), tail thruster (1) is set on the empennage (3), fixed wing (7) upper fixed wing (8) middle fixed wing ( 9) paste the solar film (2) on the top, and paste the solar film (2) on the empennage (3).
[0036] exist figure 2 Among them, the oil-electric engine (14) motor (17) pillar (16) is arranged in the power cabin (11), and the flexible shaft (15) is connected with the tail thruster (1) oil-electric engine (14), and the upper fixed wing (8) rotor (4) be located on the pillar (16), paste solar film (2) establish rotor wind generator (6) on the body (5...
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Abstract
The invention relates to a dual-motor, low energy consumption, low carbon, and plane crush resistant passenger helicopter. The helicopter comprises a helicopter body (5), the helicopter body (5) is provided with solar membranes (2), an empennage (3), a rotor (4), a rotor motor (6), a lower fixed wing (7), an upper fixed wing (8), a medium fixed wing (9), a fixed wing shaft (10), an engine compartment (11), a pulling paddle (12), and a fixed wing hydraulic device (13); the empennage (3) is provided with a pushing paddle (1); solar membranes (2) are pasted on the lower fixed wing (7), the upper fixed wing (8), and the medium fixed wing (9); an oil / electric motor (14), a motor (17), and a pillar (16) are arranged in the engine compartment (11); the pushing paddle (1) is connected to the oil / electric motor (14) through a soft shaft (15); and a passenger compartment (19), an air bag (20), a puncture-proof layer (21), and a battery (22) are arranged in the helicopter compartment (18). The puncture-proof layer and the air bag can protect the life safety of passengers. The oblate shape of the helicopter and the three fixed wings can generate a floating force for the helicopter. The wind generated by the rotor and solar energy are two green and costless power sources, thus the oil consumption, carbon discharge, and costs are all reduced, and moreover the flying distance is prolonged at the same time.
Description
technical field [0001] The invention relates to a dual-power, low-consumption and low-carbon anti-air disaster passenger transport helicopter. technical background [0002] Fixed-wing airliners are highly efficient, but they need to invest huge sums of money to build a huge airport, occupying a large amount of arable land, and have to spend huge sums of money to build transportation from the city to the airport; passengers have to travel tens of kilometers to the airport to wait for their flight by ground transportation a long time in advance; After the plane, you need to run dozens of kilometers into the urban area by ground transportation. Due to the huge investment, it is not cost-effective to build fixed-wing airports in small towns and mountainous areas within 600 kilometers. These places have to travel thousands of miles back and forth to the airport by ground transportation. [0003] Due to the huge investment, many fixed-wing airports have been operating at a loss f...
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