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Landing flap guide for aircraft

A technology of guiding parts and guiding elements, applied in aircraft parts, wing adjustment, aircraft control, etc., can solve the problems of high cost, cost, maintenance weight, etc., and achieve the effect of light weight, low manufacturing and maintenance cost, and small number of

Inactive Publication Date: 2011-11-09
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] This may require a relatively expensive construction with several guide rollers, the disadvantages of which are essentially cost, maintenance and weight

Method used

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  • Landing flap guide for aircraft
  • Landing flap guide for aircraft
  • Landing flap guide for aircraft

Examples

Experimental program
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Effect test

Embodiment Construction

[0012] exist figure 1 and 2 In the embodiment shown, the landing flap 1 of the landing flap slider 4 is supported on and guided in a landing flap carrier 3 supported on the wing, which is located on the wing. figure 1 for along figure 2 Schematic partial cross-sectional view of the landing flap guide at line AA'.

[0013] For extending and retracting the landing flap 1 , the landing flap 1 is connected to the slide 4 and is supported and guided in slideways 42 and 44 of the landing flap carrier 3 .

[0014] In this case, the slide 4 absorbs all the forces exerted on it both vertically and transversely with respect to the guide rail 3 .

[0015] figure 1 The landing flap 1 is schematically shown, which is connected to the landing flap slider 4 by means of swivel joints 45 and 46, which are only schematically shown in the figure, wherein the swivel axis of the swivel joint 45 is located in the figure within the plane.

[0016] Sliding elements 41 and 43 mounted on the lan...

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PUM

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Abstract

The invention proposes a landing flap guide for aircraft, in which the translatory landing flap (1) movement is realized with a glide slide (4) that is supported and guided in slideways of the landing flap carrier (3). The slide (4) is connected to the landing flap (1) and, in order to extend and retract the landing flap (1), guided along the flap carrier (3) by means of at least one glide guide(41, 42, 43, 44).

Description

technical field [0001] The invention relates to a landing flap guide for an aircraft, wherein the guide element is connected to a landing flap which is supported on guide rails and is adjustable between a take-off position and a landing position. Background technique [0002] The landing flap, which performs a proportional translational movement, is usually guided by a landing flap carrier which is guided on the landing flap carrier. The landing flap support needs to absorb all the forces acting on it both vertically and transversely with respect to the raceways of the support. [0003] This may require a relatively expensive construction with a plurality of guide rollers, the disadvantages of which are essentially cost, maintenance and weight. Contents of the invention [0004] It is thus an object of the present invention to provide a landing flap guide for an aircraft which provides a simplified, safe and stable landing flap guide and is highly reliable. [0005] This...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C9/16B64C3/50
CPCB64C9/16Y02T50/44Y02T50/40
Inventor 雷纳·加特尔曼博多·察普夫克努特·哈赫曼
Owner AIRBUS OPERATIONS GMBH
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