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A kind of vertical-horizontal dual-purpose aircraft and its flight mode switching method

A flight mode and aircraft technology, applied in the field of aircraft, can solve the problems of reduced maneuverability, no backup power, no intermediate transition mode, etc., to achieve the effect of increasing maneuverability and improving maneuverability

Active Publication Date: 2019-04-16
齐继国
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Existing aircraft flight mode conversion methods mostly adopt a single conversion mode (for example: China's vertical-level dual-purpose aircraft "Blue Whale", American Osprey V-22), there is no intermediate transition mode, no backup power, and the aircraft is switching flight modes The flight is extremely unstable, the controllability is reduced, and it is extremely dangerous
The existing technology has reached the limit bottleneck, and it is difficult to break through for a while, so we can only resort to methods and structures other than technology

Method used

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  • A kind of vertical-horizontal dual-purpose aircraft and its flight mode switching method
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  • A kind of vertical-horizontal dual-purpose aircraft and its flight mode switching method

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Embodiment Construction

[0022] The technical solution of this patent will be described in further detail below in conjunction with specific embodiments.

[0023] See Figure 1-7 , A vertical and horizontal dual-purpose aircraft and its flight mode conversion method, comprising a nose 1, a fuselage 2, a tail 3, an upper propeller 4, a lower propeller 5, an engine 6, a wing 7 and a landing gear 8. The head 1 is located at the front end of the fuselage 2, and the tail 3 is located at the tail end of the fuselage 2. The wings 7 are located on the left and right sides of the fuselage 2, and the propellers are installed on the wing 7. The wing 7 is vertically 2N rows or more, and horizontally 2N rows. Above (N is a positive integer), the horizontal 2N rows of propellers are separated from the middle. The upper part of the propeller is the upper propeller 4, and the lower part of the propeller is the lower propeller 5; the wing 7 is equipped with an engine 6 which drives the propeller.

[0024] Further, the fli...

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Abstract

The invention discloses a vertical-horizontal dual-purpose aircraft and its flight mode conversion method, including three conversion modes. The first one is that the upper and lower propellers rotate 90 degrees in the axial direction of the wing and the forward horizontal direction of the fuselage at the same time, changing the flight mode. Mode; the second, the upper propeller first, the lower propeller behind the wing axis, and the fuselage forward and horizontally rotate 90 degrees to change the flight mode; the third, the lower propeller first, the upper propeller behind the wing axis, and the fuselage direction Rotate the front horizontally 90 degrees to change the flight mode, and complete the conversion from multi-rotor flight mode to fixed-wing flight mode. Conversely, to switch the flight mode from the fixed-wing flight mode to the multi-rotor flight mode, it is only necessary to perform the steps of the above three flight mode conversion methods in reverse order.

Description

Technical field [0001] The invention relates to the technical field of aircraft, in particular to a vertical and horizontal dual-purpose aircraft and a flight mode conversion method thereof. Background technique [0002] Aircraft is a large category of aircraft, which refers to any machine that obtains aerodynamic lift and flight through the relative movement of the fuselage and the air (not the reaction of the air on the ground). Including balloons, airships, airplanes, gliders, rotorcraft, helicopters, flapping wing aircraft, tilt rotor aircraft, etc. An airplane is a common type of aircraft. [0003] Existing aircraft flight mode conversion methods mostly adopt a single conversion mode (for example: China's vertical dual-purpose aircraft "Blue Whale", American Osprey V-22), there is no intermediate transition mode, no backup power, the aircraft is switching flight modes The down flight is extremely unstable and the controllability is reduced, which is extremely dangerous. The...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/28B64C27/26B64C27/08
CPCB64C27/08B64C27/26B64C27/28B64U30/10B64U30/20
Inventor 齐继国
Owner 齐继国
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