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BS ISO 22072:2011

Current

Current

The latest, up-to-date edition.

Aerospace. Electrohydrostatic actuator (EHA). Characteristics to be defined in procurement specifications

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-08-2011

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Requirements
5 Installation and operating conditions
Bibliography

Describes the general characteristics, requirements and design data to be included in the procurement technical specification of an electrohydrostatic actuator (EHA) to be used to power aircraft control surfaces or other moving parts of an aerospace vehicle.

This International Standard defines the general characteristics, requirements and design data to be included in the procurement technical specification of an electrohydrostatic actuator (EHA) to be used to power aircraft control surfaces or other moving parts of an aerospace vehicle.

This type of actuator is an alternative to the hydraulically powered servo-control actuators that are currently used. It is intended that this International Standard cover the unique requirements of EHAs.

Committee
ACE/69
DevelopmentNote
Supersedes 02/706262 DC. (03/2006) Supersedes 10/30203853 DC. (08/2011)
DocumentType
Standard
Pages
24
PublisherName
British Standards Institution
Status
Current
Supersedes

Standards Relationship
ISO 22072:2011 Identical

EN 2282:1992 Aerospace series - Characteristics of aircraft electrical supplies
RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
ISO 7137:1995 Aircraft — Environmental conditions and test procedures for airborne equipment
SAE ARP 1383 : 2013 AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS

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