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
28-07-2011
€65.00
Excluding VAT
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 ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| SAE ARP6154 | Aerospace Fluid Power Electrohydrostatic Module, Design, Performance and Test Recommendations |
| SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
| EN 2282:1992 | Aerospace series - Characteristics of aircraft electrical supplies |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
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