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ISO 18387:2019

Current Revision

Aerospace - Linear hydraulic utility actuator - General specifications

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This document establishes the general requirements for a linear hydraulic utility actuator, herein referred to as a "utility actuator", for use in flight vehicle hydraulic systems at pressures up to 35 000 kPa (5 000 psi).

These requirements include:

— design requirements;

— test requirements.

This document is intended to be used in conjunction with the detail specification that is particular to each application.

NOTE Although Brake pistons and Landing Gear Bogie (Truck) Pitch Trimmers are utility actuators, they are outside the scope of this document. This is because these devices are considered to be specialist actuator devices due to their specific duty cycles requiring a separate set of tailored requirements.


SDO ISO: International Organization for Standardization
Document Number ISO 18387
Publication Date Not Available
Language en - English
Page Count
Revision Level
Supercedes
Committee ISO/TC 20/SC 10
Publish Date Document Id Type View
Not Available ISO 18387:2019 Revision