A reciprocating linear motion roller wing lift generating device

Abstract

The invention provides a reciprocating linear movement roller airfoil lift force generating device and belongs to the technical field of aviation. The reciprocating linear movement roller airfoil lift force generating device comprises a spindle, a rack, a turntable, a slide block, a translation frame, a roller airfoil, a front press plate and a rear press plate. The turntable is horizontally installed at the upper end of the spindle. A front guide rod is installed on the rack through a front left linear bearing and a front right linear bearing. A rear guide rod is installed on the rack through a rear left linear bearing and a rear right linear bearing. A guide rail is connected with the slide block, and the slide block can flexibly slide along the guide rail back and forth. The translation frame with the roller airfoil can be driven by the turntable and the slide block to perform left-right reciprocating translation. The front press plate is attached to the front end of the roller airfoil and located at upper portion of the roller airfoil. The rear press plate is attached to the rear end of the roller airfoil and located at the upper portion of the roller airfoil. When the translation frame performs leftward movement, the roller airfoil rotates clockwise. When the translation frame performs rightward movement, the roller airfoil rotates anticlockwise. Under the driving of power, the reciprocating linear movement roller airfoil lift force generating device can produce thrust and can be applied to a vertical lifting aircraft to serve as a lift force device.

Description

technical field [0001] A roller wing lift generating device with reciprocating linear motion belongs to the field of aviation technology, and in particular relates to a roller wing lift generating device. Background technique [0002] Traditional aircraft rely on wings or rotors to generate lift. The structure of aircraft wings and helicopter rotors is similar. Their cross-sections are all airfoils. When determined, the magnitude of the lift they produce is related to the angle of attack, the size of the airfoil and the velocity of the incoming flow, and the adjustment of the magnitude of the lift is achieved by changing the angle of attack, speed or the size of the airfoil. The relative thickness of the wing and the rotor is relatively thin, and the structural strength is relatively poor. The low-speed flight performance of fixed-wing aircraft is not high, the required wing area is large, and it cannot vertically lift. The rotor speed of the helicopter is very high to gen...

AI Technical Summary

Problems solved by technology

The relative thickness of the wing and the rotor are relatively thin, and the structural strength is poor

The low-speed flight performance of fixed-wing aircraft is not high, the required wing area is large, and it cannot vertically lift

The rotor speed of the helicopter is very high to generate greater lift, and it is difficult to control the balance

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