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SAE AIR 6189 : 2017

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SAE AIR 6189 : 2017

DESIGN, CALIBRATION, AND TEST METHODS FOR TURBINE ENGINE ICING TEST FACILITIES

SAE International

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Table of Contents

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

Abstract

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.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee EG-1E