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MINIMUM STANDARD FOR OXYGEN PRESSURE REDUCERS
- Aerospace Standard
Published September 01, 1991 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This standard is designed to cover all types of pressure reducers required for oxygen systems and for all performance profiles without regard for a particular inlet pressure or outlet pressure performance curve. Special attention will be given, however, to construction requirements essential in reducers where critical high initial oxygen pressures such as 1850 to 2250 psig (12.76 to 15.51 MN/m2 gauge) at 70° F (21.1° C) are involved.
Data Sets - Support Documents
|[Unnamed Dataset 1]|
Welcome to the SAE A-10 Aircraft Oxygen Equipment Committee public forum area.The SAE A-10 Aircraft Oxygen Equipment Committee develops standards and practices in the design and information compiled from users, equipment suppliers, aircraft manufacturers, regulatory agencies and medical groups in the aeronautical oxygen field. The A-10 Committee also promotes safety in the aviation oxygen field. It defines the needs and encourages research needed in the area of aviation physiology, as it relates to respiratory functions and oxygen equipment performance.
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