Disc type airplane with pneumatic wings
A wing disc type, aerodynamic technology, applied in aircraft control, aircraft parts, vertical take-off and landing aircraft, etc., can solve the problems of high wing speed and large comprehensive lift
Inactive Publication Date: 2015-03-18
雷万军
View PDF4 Cites 2 Cited by
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
As the wings and hood rotate and fly, because the rotation speed of the wings is relatively slow, but the speed of the airflow accelerated by circulation is relatively fast, so the relative speed of the wings is very high, and the comprehensive lift generated is relatively large
Method used
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View moreImage
Smart Image Click on the blue labels to locate them in the text.
Smart ImageViewing Examples
Examples
Experimental program
Comparison scheme
Effect test
Embodiment Construction
[0033] The production test of this model is not easy, and it is necessary to carry out the production and test flight of a small toy model according to the set scale.
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More PUM
Login to View More Abstract
The invention relates to a disc type airplane with pneumatic wings. The disc type airplane with pneumatic wings mainly comprises a hood, wings, a cabin and the like; 12 pneumatic bottom wings are designed, peripheral air of a critical plane can be highly accelerated to generate high-speed airflows according to the high-speed fluid critical plane negative-pressure principle, and thus, airflows flowing through the surfaces of the wings are accelerated to generate lifting force; and the wings and the hood rotate and the inside cabin and a nozzle at the center of the bottom cannot rotate and translate when the airplane is in flight; the pneumatic wings can generate high lifting force due to high relative rotating speed, the nozzle can spray downwards when the airplane goes up, and the comprehensive lifting force is high; a spherical tricyclic nozzle (a semi-spherical gimbaled nozzle) automatic control system can achieve jet power adjustment in any direction on the semi-spherical plane under the horizontal line of the airplane bottom, and automatic control can be easily realized; and a clutch is arranged at the bottom of the cabin, the connecting position of the clutch and a rotating wing can realize braking, the cabin can be hovered in air and does circular steering motion, the airplane body can turn around easily, and the airplane can be lifted vertically and can land without a lane, a rotating body rotates outside the airplane, air resistance and the generated antigravity action can be reduced, and the energy consumption can be reduced.
Description
technical field [0001] The invention relates to a design of a wing and hood rotating and moving aircraft mainly using air flow as the lifting power, which belongs to the mechanical category, and is characterized in that the disc-shaped rotating and moving has good anti-gravity effect and can reduce energy consumption. Background technique [0002] At present, high-altitude flying objects such as airplanes move in a straight line, and their air resistance is large, and their lift lifting capacity is limited. To this end, an aerodynamic wing disc-shaped aircraft is designed. According to the principle of negative pressure on the critical surface of high-speed fluid, the air around the critical surface will be accelerated at a high rate to generate high-speed airflow, thereby accelerating the airflow flowing through the surface of the wing to generate lift. And because the engine nozzle can be adjusted to spray downward, it can provide greater lift for the aircraft. As the win...
Claims
the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More Application Information
Patent Timeline
Login to View More Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/00B64C29/04B64C15/02
Inventor 雷万军
Owner 雷万军
