Description / Abstract:
This SAE Aerospace Standard (AS) specifies the general requirements
for hydraulic system reservoirs
that are installed in commercial and military aircraft and helicopters
and also in missile
hydraulic systems.
This document includes design, test (production and qualification)
criteria for various types
of reservoirs. Appendix A provides information on hydraulic fluid
volume requirements and
reservoir sizing.
This document also provides a basis for the Procurement Specification
to completely define
individual reservoir requirements
Reservoir Types:
Type A - Separated, hydraulically pressurized - (commonly referred to
as a "bootstrap reservoir")
Type B - Separated, gas pressurized - (commonly through an engine
bleed system or by a pressurized
gas charge)
Type C - Separated, mechanically pressurized - (usually by a spring
and for emergency use)
Type D - Non-separated, gas pressurized - (commonly through an engine
bleed system)
Type E - Non-separated, non-pressurized - (commonly referred to as an
open reservoir)