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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 , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English

Published date

28-07-2011

Publisher

International Organization for Standardization

Preview

ISO 22072:2011 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 ISO 22072:2011 cover the unique requirements of EHAs.

Committee
ISO/TC 20/SC 10
DevelopmentNote
Supersedes ISO/DIS 22072. (07/2011)
DocumentType
Standard
Pages
12
PublisherName
International Organization for Standardization
Status
Current
Supersedes

Standards Relationship
BS ISO 22072:2011 Identical
PN ISO 22072 : 2007 Identical

SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
SAE ARP 6154 : 2017 AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS
SAE ARP 4752 : 2013 AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS

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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Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
Hardcopy - English
PDF - English
Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
Hardcopy - English
PDF - English
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