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基本信息

【标准号】: AIR5273
【中文名称】: Actuation System Failure Detection Methods
【英文名称】: Actuation System Failure Detection Methods
【发布时间】
【实施时间】: 2007-01-01
【有效性】: 有效
【起草人】
【起草单位】
【提出单位】
【归口单位】
【批准单位】
【分类】
【备案号】
【自动关键词】

【范围】

This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation though it includes one augmented-control system. The background to the subject is discussed in terms of the impact that factors such as the system architecture have on the detection methods chosen for the flight control system. The types of failure covered by each monitoring technique are listed and discussed in general. The way in which these techniques have evolved is illustrated with an historical review of the methods adopted for a series of aircraft, arranged approximately in design chronological order. 1.1 Purpose: The purpose of this document is to aid the designers of the systems of the future by showing what succeeded in the past.strRefField

【与前一版的变化】

包含缩略语

BIT：
CBIT：
CCDL：
CCM：
CMM：
CRM：
CSAS：
DDV：
DFCC：
ECU：
EHV：
EICAS：
FAA：
FBW：
FCC：
FHA：
FMEA：
FMECA：
FO / FS：
FO 2 / FS：
FS：
IBIT：
IFCM：
ILM：
JAA：
LCA：
LES：
LRU：
LVDT：
MBIT：
MCV：
MMC：
MTBF：
NPRM：
NVM：
PBIT：
PLOC：
RLS：
RVDT：
RVT：
SVM：
WRA：

引用文件/被引文件

SAE AIR4094: Aircraft Flight Control Systems Descriptions.
SAE AIR4253: FBW Actuation System Descriptions.
SAE Paper 831484: Development of Redundant Flight Control Actuation Systems for the F/A-18 Strike Fighter
MIL-F-9490: Flight Control Systems – Design
MIL-STD-882: System Safety Program Requirements.
AC 25.1309–1A: FAA Advisory Circular
NPA 25C-199: JAA Notice of Proposed Rule Making
RTCA DO-178: Software Considerations in Airborne Systems and Equipment Certification
SAE Publication: Fly-By-Wire A Historical and Design Perspective