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High-stability and firmly-mounted fixed wing aircraft wing

A stable and fixed-wing technology, applied in the field of fixed-wing aircraft, can solve the problems of unstable installation and inconvenient wing installation, and achieve the effects of reliable installation and positioning, convenient and quick installation, and avoiding damage

Pending Publication Date: 2019-04-05
江西冠一通用飞机有限公司 +1
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  • Abstract
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Problems solved by technology

[0004] The purpose of the present invention is to provide a fixed-wing aircraft wing with strong stability and firm installation, so as to solve the problem that the existing fixed-wing aircraft wing proposed in the above-mentioned background technology is inconvenient to install and cannot be quickly installed and stabilized. The problem

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Embodiment Construction

[0026] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0027] see Figure 1-6 , the present invention provides a technical solution: a fixed-wing aircraft wing with strong stability and firm installation, comprising a first wing 1 and a mounting groove 2, the left lower end of the first wing 1 is provided with a mounting groove 2, The first wing 1 is connected to the installation groove 2 through socket connection, and the surface end of the left lower end of the first wing 1 is penetrated with a fix...

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Abstract

The invention discloses a high-stability and firmly-mounted fixed wing aircraft wing. The high-stability and firmly-mounted fixed wing aircraft wing comprises a first wing and a mounting groove; the mounting groove is formed in the lower end of the left side of the first wing; the first wing is connected with the mounting groove in a sleeving manner; a fixing clamping seat is arranged to penetratethrough the surface end of the lower end of the left side of the first wing; and the fixing clamping seat is connected with the first wing in a through manner. According to the high-stability and firmly-mounted fixed wing aircraft wing, by arranging a support reinforcing plate at the perpendicularly intersected part of the first wing and a second wing, the support reinforcing plate can enable a suffered impact force to be stable to prevent a phenomenon that the first wing and the second wing cannot fall off; and therefore,damages of the first wing and the second wing caused by fall-off are avoided so that the service life of the integral structure of the fixed wing aircraft wing can be prolonged; and moreover, influences caused by factors such as a clearance and a manufacturing error areeliminated while the connecting strength between the first wing and an aircraft body and the connecting strength between the second wing and the aircraft body are guaranteed.

Description

technical field [0001] The invention belongs to the related technical field of fixed-wing aircraft, and in particular relates to a fixed-wing aircraft wing with strong stability and firm installation. Background technique [0002] Since the wing of a vertical take-off and landing fixed-wing aircraft usually needs to be installed with a vertical lift system, it is required that the connecting mechanism between the wing and the fuselage not only bear the gravity of the fuselage, but also bear the torque caused by the inertia of the vertical lift system. The wing installation mechanism of the fixed-wing aircraft puts forward higher requirements. [0003] The wing technology of existing fixed-wing aircraft has the following problems: the wing bolt connection of existing fixed-wing aircraft refers to the use of multiple bolts to directly fix the wing on the fuselage, which has high reliability, but the installation process Slower, the wing is fixed through the cooperation of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/26B64C3/18B64F5/10
CPCB64C1/26B64C3/182B64C3/187B64F5/10Y02T50/40
Inventor 李宁康梁飞刘韬罗友
Owner 江西冠一通用飞机有限公司
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