This Aerospace Recommended Practice (ARP) provides recommendations for the design and test requirements for a hydraulic thermal relief valve. The thermal relief valve is intended for use in a civil or military aircraft hydraulic system with a rated system pressure up to 5000 psi (34500 kPa). ARP4835 has been updated to Revision A for the following reasons: It has been rewritten to a new format including the title change. It incorporates technical and editorial changes. The references have been updated.
Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves
26.08.2021
Aufsatz (Konferenz)
Englisch