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Double-duct tilt aircraft

A technology of tilting aircraft and ducts, which is applied in the field of transportation, can solve the problems of large volume and high fuel consumption, and achieve the effects of stable take-off and landing, good field of view, and high flying speed in the air

Active Publication Date: 2015-12-23
友铂空天动力(深圳)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Traditional air vehicles, such as fixed-wing aircraft and helicopters, are bulky, fuel-intensive, and require special venues for flight. They are not suitable for use as personal air vehicles. Aircraft that take off and land vertically on lawns, roads, open areas, etc. and have low flight costs

Method used

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Embodiment Construction

[0015] The present invention will be further described below in conjunction with specific embodiments. The exemplary embodiments and descriptions of the present invention are used to explain the present invention, but not as a limitation to the present invention.

[0016] A double-duct tilting aircraft, comprising a ducted rotor seat 1, a fuselage 2, a ducted rotor 3, flaps 4, a driven synchronous pulley 5, a synchronous belt 6, an active synchronous pulley 7, landing gear 8, Turbine 9, main wing 10, battery pack 11, cockpit 12, electronic control device 13, hydraulic pump station 14, servo motor 15, worm 16, worm support 17, driven bevel gear 18, driving bevel gear shaft 19, kerosene piston type The engine 20, the first crank 21, the first hydraulic cylinder 22, the second hydraulic cylinder 23, and the second crank 24 are characterized in that: the ducted rotor seat 1 is hinged in the mounting hole on the side of the fuselage 2, and can be used in the second hydraulic pressur...

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Abstract

The invention provides a double-duct tilt aircraft. The double-duct tilt aircraft comprises duct rotor seats, a machine body, duct rotors, flaps, driven synchronous pulleys, synchronous belts, a driving synchronous pulley, an undercarriage, a turbine, a main wing, a storage battery set, a cockpit, an electronic operating device, a hydraulic power unit, a servo motor, a worm, a worm support, driven bevel gears, driving bevel gear shafts, a kerosene reciprocating engine, first cranks, first hydraulic cylinders, second hydraulic cylinders and second cranks. The flying speed and posture of the double-duct tilt aircraft are controlled by the duct rotors, the flaps and the main wing jointly, so that the double-duct tilt aircraft has the characteristics of being large in lift force, smooth and steady in taking off and landing and high in air flying speed. The cockpit is arranged on utmost upper portion of the double-duct tilt aircraft, so that a pilot has a good sight range, and the operation of the double-duct tilt aircraft is greatly facilitated. The main wing can be driven by the servo motor to rotate by 90 degrees and keep parallel to the machine body when parked, so that space is saved, and traffic jam in a city is eased.

Description

technical field [0001] The invention relates to an air vehicle, in particular to a double-duct tilting aircraft, which belongs to the field of transportation. Background technique [0002] With the continuous development of modern transportation technology, land transportation has gradually become the main way of travel for people, but with the increase of urban population, land transportation is becoming more and more congested, so it is necessary to develop air transportation technology. Traditional air vehicles, such as fixed-wing aircraft and helicopters, are bulky, fuel-intensive, and require special venues for flight. They are not suitable for use as personal air vehicles. Aircraft that take off and land vertically on lawns, roads, open areas, etc. and have low flight costs. Contents of the invention [0003] In view of the above problems, the present invention provides a double-ducted tilting aircraft, each of which has a ducted rotor seat at the front and rear of ...

Claims

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Application Information

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IPC IPC(8): B64C27/28B64C27/20
Inventor 徐金鹏
Owner 友铂空天动力(深圳)有限公司
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