Aerospace aircraft wing

Abstract

The invention discloses an aircraft wing for aerospace use. The aircraft wing comprises a body, wherein a landing gear is installed in the center of the bottom end of the body; a bottom block is arranged on the right side of a turbine; the top end of the bottom block is connected with wings; first supporting rods are arranged on left and right sides at the bottom end of the bottom block; slide blocks are arranged on outer walls of the first supporting rods in a sleeving manner; first baffles are arranged on inner sides of the slide blocks; second springs are arranged on the left and right sides at the bottom ends of the second baffles; a convex block is connected to the center of the top of an inner groove in a sleeving manner; a first rotating rod is connected to the center of a first insert block in a sleeving manner; and runners are installed on the left and right sides of the first rotating rod. According to the aircraft wing for aerospace use, when the body is subjected to landingbuffer, an assisted buffering operation is performed when the body lands by virtue of match of the bottom block and the landing gear, so that less flutter is produced during landing, and a flutteringeffect of the body is effectively reduced.

Description

technical field [0001] The invention relates to the technical field of aircraft wing equipment, in particular to an aircraft wing for aerospace. Background technique [0002] The wing is one of the important parts of the aircraft. It is installed on the fuselage. Its main function is to generate lift. At the same time, ammunition warehouses and fuel tanks can be built inside the wing. The landing gear can be stored during flight. In addition, the wing Flaps to improve take-off and landing performance and ailerons for lateral manipulation of the aircraft are also installed on the aircraft, and some devices are also equipped with slats and other lift-increasing devices on the leading edge of the wing. In the prior art, such as the application number is The utility model patent of 201620266403.5 includes a fuselage and wings, the fuselage is fixedly installed above the empennage, the wings are installed on both sides of the fuselage, and the surface of the wings is provided wit...

AI Technical Summary

Problems solved by technology

[0002] The wing is one of the important parts of the aircraft. It is installed on the fuselage. Its main function is to generate lift. At the same time, ammunition warehouses and fuel tanks can be built inside the wing. The landing gear can be stored during flight. In addition, the wing Flaps to improve take-off and landing performance and ailerons for lateral manipulation of the aircraft are also installed on the aircraft, and some devices are also equipped with slats and other lift-increasing devices on the leading edge of the wing. In the prior art, such as the application number is The utility model patent of 201620266403.5 includes a fuselage and wings, the fuselage is fixedly installed above the empennage, the wings are installed on both sides of the fuselage, and the surface of the wings is provided with wing knives, the wings The inside of the wing is provided with a spar, and the left side of the spar is provided with a reinforcing rib, and the inside of the wing is provided with a rib, and the inside of the rib is provided with stringers. Although this patent avoids flutter of the aircraft, But the effect of avoiding flutter is not perfect, and it still produces flutter when landing

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