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Inlet Airflow Ramps for Gas Turbine Engine Test Cells
- Aerospace Standard
- AIR5306A
- Stabilized
Sector:
Issuing Committee:
Language:
English
Scope
This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of gas turbine engines and particularly for those who might be interested in upgrading their existing engine test facility to meet the airflow requirements for higher thrust engine models. The intellectual property rights on the material contained in this document are protected by US Patent Number 5,293,775 dated March 15, 1994 assigned to United Technologies Corporation, Hartford, Connecticut, USA. Any individual, or organization, attempting to use the system described in this document should get a clearance from United Technologies Corporation, to avoid any potential liability arising from patent infringement.
Rationale
This document has been determined to contain stable technology which is not dynamic in nature.
Recommended Content
| Aerospace Standard | Design Considerations for Enclosed Turbofan/Turbojet Engine Test Cells |
| Aerospace Standard | Test Cell Instrumentation |
Data Sets - Support Documents
No Datasets Available
Issuing Committee
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.
Reference
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