Steering gear installation structure and aircraft

A technology of installation structure and steering gear, which is applied in the direction of aircraft parts, aircraft control, transportation and packaging, etc., and can solve the problem of difficult installation of steering gear

Active Publication Date: 2021-09-14
NINGBO GEELY AUTOMOBILE RES & DEV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the technical problems in the background technology, the present invention provides a steering gear installation structure that solves the problem of difficult installation of the steering gear in the smaller wing box space and effectively improves the installation efficiency of the steering gear

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  • Steering gear installation structure and aircraft
  • Steering gear installation structure and aircraft

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Embodiment Construction

[0021] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the drawings in the embodiments of the present invention. Apparently, the described embodiments are only some of the embodiments of the present invention, but 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 creative efforts fall within the protection scope of the present invention.

[0022] Such as figure 1 As shown, a steering gear installation structure related to the embodiment of the present invention includes: a rectification port cover 1, a mounting plate 2 and a mounting bracket 3; wherein, the rectification port cover 1 is embedded in the first opening 81 of the wing lower skin 8 The rectification port cover 1 is connected with the installation plate 2; the installation plate 2 is arranged on the inner side of the wing lower skin...

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Abstract

The invention discloses a steering gear installation structure and an aircraft. The steering gear installation structure includes a rectification port cover, a mounting plate and a mounting bracket; the rectification port cover is embedded in the first opening of the lower skin of the wing; the rectification port cover connected with the mounting plate; the mounting plate is arranged on the inner side of the lower skin of the wing, the mounting plate is provided with a second opening, and the outline of the second opening and the outline of the mounting plate are respectively Located on the inside and outside of the first opening outline; the mounting bracket includes a fixing portion and a steering gear mounting portion, the mounting bracket is placed on the inside of the lower skin of the wing, the fixing portion is connected to the rectifying opening The cover is connected; the steering gear installation part is used for installing the steering gear. Compared with the traditional small aircraft steering gear installation structure, the steering gear installation structure involved in the present invention solves the problem that the steering gear is difficult to install in a small wing box space, and improves the installation efficiency.

Description

technical field [0001] The invention relates to the technical field of steering gear components, in particular to a steering gear installation structure and an aircraft. Background technique [0002] The steering gear is the driving device for controlling the control surface of the aircraft. It is fixed to the wing structure through the installation structure, and the rotation angle of the steering surface is driven by the connecting rod mechanism, so as to achieve the purpose of controlling the flight state of the aircraft. [0003] The steering gear of a traditional small aircraft is usually fixed on the beam or rib structure of the wing by a separate connection structure. For installation and maintenance, an inspection cover of sufficient size is generally provided at the corresponding upper skin position of the steering gear. However, due to The connecting rod of the steering gear will move to the outside of the wing during the movement. It is also necessary to add a fai...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C9/02
CPCB64C9/02
Inventor 周龙超汤晓明黄雍威陈修贤吕金泽方宜武
Owner NINGBO GEELY AUTOMOBILE RES & DEV CO LTD
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