SAE International Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves ARP4835A

Description
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).
Description
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).

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Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves - ARP4835A - SAE International
Warrendale, PA, United States
Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves
ARP4835A
Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves ARP4835A
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).

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).

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP4835A
Product Name Recommended Design and Test Requirements for Hydraulic Thermal Expansion Relief Valves
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