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Mounting plate with anti-icing function

A technology for mounting boards and functions, applied in deicing devices, transportation and packaging, aircraft parts, etc., can solve the problems of no heating capacity and inability to meet aircraft anti-icing conditions, and achieve fast heating speed, small structure, and rapid heat generation The effect of conduction

Pending Publication Date: 2022-03-11
TAIYUAN AERO INSTR
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the installation part of the stall warning device at the leading edge of the aircraft wing has no heating capacity, and cannot meet the anti-icing conditions of a certain type of aircraft.

Method used

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  • Mounting plate with anti-icing function
  • Mounting plate with anti-icing function
  • Mounting plate with anti-icing function

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Embodiment Construction

[0026] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with 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] Such as figure 1 and 2 , a mounting plate with anti-icing function, comprising: wing-shaped laminating plate 7, heating plate I2, heating plate II6, pressing plate II5, pressing plate III8, and pressing plate I4, wherein the outer side of the wing-shaped laminating plate 7 is the windward side, and the inner type The surface is a three-dimensional curved surface in space that is bonded to the wing skin, and the middle part of the wing-s...

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Abstract

The invention belongs to the field of aviation instruments and meters, and particularly relates to a mounting plate with an anti-icing function. Comprising a wing-shaped attaching plate, a heating piece I, a heating piece II, a pressing plate II, a pressing plate III and a pressing plate I. The outer side of the wing-shaped attaching plate is a windward side, the molded surface of the inner side of the wing-shaped attaching plate is a spatial three-dimensional curved surface attached to a wing skin, a weather vane passing hole is formed in the middle of the wing-shaped attaching plate, and an outer circle pit of the wing-shaped attaching plate is connected with a wing. The heating piece I and the heating piece II are arranged on the inner side face of the wing-shaped attaching plate and located above and below the weather vane passing hole respectively. The heating sheet I and the heating sheet II are respectively pressed and fixed on the inner side of the wing-shaped attaching plate through a pressing plate II and a pressing plate III; and leads of the heating sheet I and the heating sheet II are fixed through a pressing plate I and are led out. The anti-icing effect of the windward side of the mounting plate is achieved through the two heating piece structures.

Description

technical field [0001] The invention belongs to the field of aviation instruments and meters, and in particular relates to a mounting plate with an anti-icing function. Background technique [0002] At present, the installation part of the stall warning device at the leading edge of the aircraft wing has no heating capacity, which cannot meet the anti-icing conditions of a certain type of aircraft. Contents of the invention [0003] The purpose of the present invention is to provide a mounting plate with anti-icing function. [0004] Technical scheme of the present invention: [0005] A mounting plate with anti-icing function, comprising: wing-shaped laminated plate 7, heating plate I2, heat-generating plate II6, pressure plate II5, pressure plate III8, and pressure plate I4, wherein the outer side of the wing-shaped laminated plate 7 is the windward surface, and the inner surface is In order to fit the three-dimensional curved surface of the wing skin, the middle part o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D15/12B64D43/00H05B3/06
CPCB64D15/12B64D43/00H05B3/06
Inventor 冯华李欣伟方嘉民吴慧龙梁争谊
Owner TAIYUAN AERO INSTR