SAE AIR 6189 : 2017
SAE AIR 6189 : 2017
DESIGN, CALIBRATION, AND TEST METHODS FOR TURBINE ENGINE ICING TEST FACILITIES
SAE International
DESIGN, CALIBRATION, AND TEST METHODS FOR TURBINE ENGINE ICING TEST FACILITIES
SAE International
1. SCOPE
2. REFERENCES
3. CLARIFICATION OF TERMS
4. REGULATORY ICING ENVELOPES AND REQUIREMENTS
5. COMMENTS ON USE OF REGULATIONS
6. FACILITIES DESCRIPTION
7. SIMULATED ICING CLOUD GENERATION
8. CLOUD MEASUREMENT METHODS
9. ENVIRONMENT MEASUREMENTS
10. ICING CLOUD CALIBRATION
11. NOTES
APPENDIX A - DELEGATION GENERALE POUR LARMEMENT (DGA)
AERO ENGINES
APPENDIX B - GLOBAL AEROSPACE CENTRE FOR ICING AND
ENVIRONMENTAL RESEARCH, INC. (GLACIER)
APPENDIX C - GENERAL ELECTRIC AVIATION WINNIPEG AND PEEBLES
APPENDIX D - NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
PROPULSION SYSTEMS LABORATORY (PSL)
APPENDIX E - NATIONAL RESEARCH COUNCIL CANADA (NRC) GAS
TURBINE LABORATORY (GTL)
APPENDIX F - UNITED STATES AIR FORCE ARNOLD ENGINEERING
DEVELOPMENT CENTER (AEDC)
APPENDIX G - UNITED STATES AIR FORCE MCKINLEY CLIMATIC
LABORATORY
Gives descriptions of test procedures and established practices for the application, use, and administration of the conduct of icing testing for all types of turbine engines in conventional supercooled liquid (14 CFR Part 25 Appendix C) environmental conditions in ground test facilities (sea-level and altitude) for icing certification purposes.
Document Type | Standard |
Status | Current |
Publisher | SAE International |
Committee | EG-1E |