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GAS TURBINE ENGINE FUEL NOZZLE TEST PROCEDURES
- Aerospace Standard
Published November 15, 2007 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The intent of this SAE Aerospace Recommended Practice (ARP) is to define and recommend to the Aerospace Industry standardized test procedures for establishing fuel nozzle operating performance including types of tests, controlled and measured parameters, and test configurations.
|Aerospace Standard||Aircraft and Aircraft Engine Fuel Pump Low Lubricity Fluid Endurance Test|
|Aerospace Standard||Detailed Specification for Aircraft Pressure Refueling Nozzle|
|Aerospace Standard||Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583)|
Data Sets - Support Documents
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|Unnamed Dataset 2|
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|Unnamed Dataset 4|
|TABLE C1||Suggested Schedule for Calibration Intervals for the Instrumentation|
|TABLE D1||Secondary Circuit Flow Limits|
|TABLE D2||Fuel Flow Limits|
EG-1E Gas Turbine Test Facilities and Equipment
The SAE EG-1E, Gas Turbine Engine Test Facilities & Equipment committee addresses all facets of test facility design, operation, maintenance, calibration and measurement, relating to gas turbine engine testing. The group is dedicated to creating, preparing, and maintaining all relevant specifications, standards, and requirements in this field.
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