Propulsion system and canard coaxial rotating device of tilting power general-purpose plane

Abstract

The invention discloses a propulsion system and canard coaxial rotating device of a tilting power general-purpose plane. The tilting power general-purpose plane comprises wings, a fuselage, an empennage, a canard, a plane tail connecting rod auxiliary device, power devices and the propulsion system and canard coaxial rotating device. The power devices comprise the first power device, the second power device, the third power device and the fourth power device; the canard is arranged at the front end of the fuselage; the first power device and the second power device are arranged at the two endsof the canard correspondingly; the wings are arranged on the positions, at the two ends of the fuselage, behind the canard correspondingly; the plane tail connecting rod auxiliary device is arrangedbehind the wings; the third power device and the fourth power device are arranged at the two ends of the plane tail connecting rod auxiliary device correspondingly; the empennage is arranged behind the plane tail connecting rod auxiliary device; and the propulsion system and canard coaxial rotating device is arranged inside the fuselage. The shortcomings that as for a general-purpose plane, oil consumption is high, the passenger capacity is less, the range is limited, conditional constraints of take-off and landing exist, and the cost is high are overcome.

Description

technical field [0001] The invention relates to the field of general-purpose aircraft, in particular to a propulsion system and a canard coaxial rotating device of a general-purpose aircraft with tilting power. Background technique [0002] General-purpose aircraft are widely used in real life, and the potential of general-purpose aircraft in the future market will be huge. It restricts the development, popularization and application of general-purpose aircraft. As a result, the advantages of general-purpose aircraft cannot be maximized. [0003] Now the world's famous tilt-rotor aircraft is the American combat transport aircraft V-22 "Osprey". It is a two-rotor aircraft that can take off and land vertically like a helicopter. aircraft of this type. [0004] However, there are still some problems in the field of general aviation: at this stage, there is no precedent for the flight of power-tilted jet general-purpose aircraft, and only helicopters play a major role in gene...

AI Technical Summary

Problems solved by technology

[0006] In order to solve the problems existing in the prior art, the present invention provides a three-wing small general-purpose aircraft with tilting power, which solves the problems of high fuel consumption, small passenger capacity, limited voyage, and conditional constraints on take-off and landing of the general-purpose aircraft. Disadvantages of high cost

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