This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Gas Turbine Engine Fuel Nozzle Test Procedures
- Aerospace Standard
Published December 10, 2013 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.
This document has been determined to contain stable technology which is not dynamic in nature.
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|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.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.