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.
Cross References:SAE AS5860
ISO 2093
SAE AS5857
ISO 2669
SAE AS4716
ISO 8079
SAE AS5861
ISO 11218
ISO 8625-2
ISO 8625-3
SAE AS5782
ISO 7137
ISO 8078
ISO 2671
SAE AS4088
ISO 8625-1
SAE AS5781
MIL-STD-810
ISO 3323
SAE AIR1244
ISO 8081
ISO 5855-2
ISO 3601-1
SAE ARP1383
ISO 21849
SAE AS 1290
ISO 5855-3
SAE AS 4059
ISO 5855-1
SAE AS 8879
ISO 7320
All current amendments available at time of purchase are included with the purchase of this document. | File Size : | 1
file
, 1.7 MB |
| ISBN(s) : | 9780580996085 |
| Note : | This product is unavailable in Russia, Ukraine, Belarus |
| Number of Pages : | 58 |
| Product Code(s) : | 30371800, 30371800, 30371800 |
| Published : | 10/08/2019 |
| Same As : | BS ISO 18387:2019 |
