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Brake characteristics

A technology of brakes and processors, applied in the directions of brakes, brake types, brake components, etc., to solve the problem of aircraft not being allowed to fly

Pending Publication Date: 2020-10-30
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In this case, the aircraft in question may not be cleared to fly

Method used

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  • Brake characteristics
  • Brake characteristics
  • Brake characteristics

Examples

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Embodiment Construction

[0034] figure 1 It is a simplified schematic diagram of aircraft 100. The aircraft 100 includes a plurality of landing gear assemblies 102. The landing gear assembly 102 may include a main landing gear and a nose landing gear that can be extended during takeoff and landing. Each landing gear assembly 102 includes wheels such as wheels 104. The aircraft 100 also includes a computing system 106 that includes one or more processors and one or more computer-readable storage media. The aircraft 100 also includes a set of sensors 108, which may include sensors for measuring environmental characteristics and sensors associated with various components of the aircraft 100 and measuring values ​​of various physical properties of the corresponding components. Although in figure 1 The sensor 108 is represented by a single box in the schematic diagram, but it will be understood that the sensor 108 may be located at various positions on the aircraft 100. The aircraft 100 may also include ...

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PUM

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Abstract

Disclosed is a non-transitory computer readable storage medium having stored thereon instructions which, when executed by a processor, cause the processor to: determine whether an aircraft wheel brakeis capable of performing a future rejected take-off event. The determination comprises determining from a rejected take-off energy parameter and a set of brake parameters whether a predicted mass ofthe brake is sufficient to perform the future rejected take-off event. Further, a method for determining whether the aircraft wheel brake is capable of performing a future rejected take-off event is disclosed.

Description

Technical field [0001] The present invention relates to determining whether the wheel brakes of an aircraft can perform future rejected take-off events. Background technique [0002] The wheel brakes of aircraft will experience wear and oxidation. The amount of wear on the brake can be checked and the brake can be viewed visually to identify signs of oxidation. If the amount of wear and / or oxidation has reached a certain level, it can be considered that the brake needs to be repaired or replaced. In this case, the aircraft in question may not be allowed to fly. Summary of the invention [0003] The first aspect of the present invention provides a non-transitory computer-readable storage medium having instructions stored thereon that, when executed by a processor, cause the processor to perform the following operations: determine whether the aircraft wheel brakes can perform the future The interrupted take-off event includes determining whether the estimated quality of the brake...

Claims

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Application Information

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IPC IPC(8): B64F5/60B60T17/22
CPCB64F5/60B60T17/22B60T8/1703B60T13/662B60T17/221B60T8/325B64C25/42F16D66/00F16D66/022F16D2066/001B60T2270/413
Inventor 安德鲁·比尔
Owner AIRBUS OPERATIONS GMBH