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Aircraft braking system architecture and process for managing an aircraft braking system architecture

机译:飞机制动系统架构和用于管理飞机制动系统架构的过程

摘要

"AIRCRAFT BRAKING SYSTEM ARCHITECTURE AND MANAGEMENT PROCESS FOR AN AIRCRAFT BRAKING SYSTEM ARCHITECTURE". The invention relates to an architecture for a braking system for an aircraft equipped with a plurality of landing gear, each supporting a plurality of wheels, at least some of which are fitted with brakes (1, 2, ..., 8), the architecture comprising at least two braking computers (A, B), each having two modules (A1, B4), so that in each computer one of the modules (A1, B1) controls a first fraction of the brakes. (1, 4, 5, 8) and the other module (A2, B2) controls a second fraction of the brakes (2, 3, 6, 7) complementary to the first. According to the invention, the architecture is configured to operate in any of the following modes of operation: a first normal mode in which both modules (A1, A2) of one of the braking computers are active to control all brakes; . a second normal mode in which both modules (B1, B2) of the other braking computer are active to control all brakes; and an alternative mode in which a module (A2) of one braking computer and a module (B1) of the other braking computer are active to control all brakes.
机译:“飞机制动系统体系结构和飞机制动系统体系结构的管理过程”。本发明涉及一种用于飞机的制动系统的结构,该飞机配备有多个起落架,每个起落架支撑多个轮子,其中至少一些轮子装有制动器(1、2,...,8),该架构包括至少两个制动计算机(A,B),每个制动计算机具有两个模块(A1,B4),从而在每个计算机中,模块(A1,B1)中的一个控制第一部分制动器。 (1、4、5、8)和另一个模块(A2,B2)控制与第二个制动器互补的第二个制动器(2、3、6、7)。根据本发明,该体系结构被配置为以以下任何一种操作模式进行操作:第一正常模式,其中一个制动计算机的两个模块(A1,A2)均处于活动状态,以控制所有制动器; 。第二种正常模式,其中另一台制动计算机的两个模块(B1,B2)均处于活动状态,以控制所有制动器;一种替代模式,其中一个制动计算机的模块(A2)和另一台制动计算机的模块(B1)处于活动状态,以控制所有制动器。

著录项

  • 公开/公告号BRPI0405729A

    专利类型

  • 公开/公告日2005-08-30

    原文格式PDF

  • 申请/专利权人 MESSIER-BUGATTI;

    申请/专利号BR2004PI05729

  • 发明设计人 STEPHANE MALLEVAIS;JEAN-PIERRE GARCIA;

    申请日2004-12-21

  • 分类号B64C25/02;B60T7/00;

  • 国家 BR

  • 入库时间 2022-08-21 22:18:23

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