Aircraft with skylight on wing

A technology of aircraft and skylights, applied in the field of aircraft, can solve the problems of high energy consumption, inability to take off and land vertically, low safety and stability, etc., and achieve the effect of simple control and stable flight

Inactive Publication Date: 2016-01-27
FOSHAN SHENFENG AVIATION SCI & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Traditional aircraft need a runway to take off and land, cannot take off and land vertically, and are not convenient for ultra-low speed or hovering flight, and it is also difficult to take off and land in a short distance
Traditional helicopters have high energy consumption, low efficiency, low safety and stability

Method used

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  • Aircraft with skylight on wing
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Examples

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Embodiment Construction

[0009] The present invention will now be described in detail with reference to the drawings: an aircraft with a sunroof on the wing, including a fuselage 1, a left composite wing 2, a right composite wing 3, a tail 4 and a landing gear 5. The fuselage 1 is equipped with a control system and airborne equipment. The tail 4 is located at the tail of the fuselage 1, and the tail 4 includes a horizontal tail and a vertical tail. The horizontal stabilizer functions as a horizontal stabilizer and pitch control, and the vertical stabilizer functions as a vertical stabilizer and rudder. The landing gear 5 adopts a wheeled structure. The left composite wing 2 and the right composite wing 3 have the same structure, and they are installed symmetrically on the left and right sides of the fuselage 1.

[0010] The specific structure of the left composite wing 2 is: the left composite wing 2 includes a main wing 21, a movable wing 22, a rotor 23, an engine 24 and a bracket 25. The leading edg...

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PUM

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Abstract

The invention relates to an aircraft with a skylight on a wing, which belongs to the technical field of aircrafts. The aircraft with the skylight on the wing comprises an aircraft body, a left composite wing, a right composite wing, a tail wing and a landing gear. An operation system and airborne equipment are mounted in the aircraft body. The tail wing is positioned at the tail part of the aircraft body; and the tail wing comprises a horizontal tail wing and a vertical tail wing. The landing gear uses a wheel type structure or a skid and wheel combined structure. The left composite wing and the right composite wing have same structures and are symmetrically mounted on the left and right sides of the aircraft body. The left composite wing comprises a main wing, a movable wing, a rotor wing, an engine and a bracket. The front edge of the main wing is higher than the back edge of the main wing; the right end of the main wing is connected with the aircraft body; a push-and-pull skylight is arranged at the middle part, close to the aircraft body, of the main wing; the movable wing can cover the window of the skylight under the pushing and pulling of external forces; and the skylight is opened when the movable wing is inserted into the left section of the main wing. The rotor wing and the engine are mounted right under the window through the bracket. The rotating plane of the rotor wing is horizontally placed. The aircraft can vertically take off and land and is safe, energy-saving and efficient.

Description

Technical field [0001] An aircraft with a skylight on its wing belongs to the technical field of aircraft, in particular to an aircraft with a skylight on its wing. Background technique [0002] Traditional airplanes require runways for take-off and landing. They cannot take off and land vertically, and are not convenient for flying at ultra-low speeds or hovering. Short-distance takeoffs and landings are also difficult. Traditional helicopters have high energy consumption, low efficiency, and low safety and stability. Summary of the invention [0003] The purpose of the present invention is to overcome the above-mentioned shortcomings of traditional airplanes and helicopters, and to invent an efficient, safe and stable aircraft with skylights on wings that is convenient for short-distance take-off and landing and even vertical take-off and landing. [0004] An aircraft with a skylight on the wing includes a fuselage, a left composite wing, a right composite wing, a tail wing and a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C27/22B64C29/02B64C9/02B64C21/00
Inventor 王志成
Owner FOSHAN SHENFENG AVIATION SCI & TECH
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