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SAE AIR 1667 : 2013

Current

Current

The latest, up-to-date edition.

ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

23-04-2013

€157.21
Excluding VAT

1. SCOPE
2. REFERENCES
3. ELECTROTHERMAL ICE PROTECTION SYSTEMS
4. DESIGN CONSIDERATIONS
5. TEST CONSIDERATIONS
6. NOTES
APPENDIX A - OTHER ICE PROTECTION CONCEPTS
APPENDIX B - RATE OF ICE COLLECTION
APPENDIX C - SURFACE EQUILIBRIUM (DATUM)
             TEMPERATURE MODEL

This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection systems.

Committee
AC-9C
DocumentType
Standard
Pages
49
PublisherName
SAE International
Status
Current
Supersedes

SAE ARP 5624 : 2013 AIRCRAFT INFLIGHT ICING TERMINOLOGY
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
JSSG-2009 Revision A:2013 Air Vehicle Subsystems
SAE AIR 1168/4 : 2016 SAE AEROSPACE APPLIED THERMODYNAMICS MANUAL ICE, RAIN, FOG, AND FROST PROTECTION

SAE AIR 4015 : 2013 ICING TECHNOLOGY BIBLIOGRAPHY
FAA AC 20-117 : 1982 HAZARDS FOLLOWING GROUND DEICING AND GROUND OPERATIONS IN CONDITIONS CONDUCIVE TO AIRCRAFT ICING
FAA AC 20-73 : 2006 AIRCRAFT ICE PROTECTION
SAE ARP 5903 : 2015 DROPLET IMPINGEMENT AND ICE ACCRETION COMPUTER CODES
SAE ARP 5905 : 2015 CALIBRATION AND ACCEPTANCE OF ICING WIND TUNNELS
SAE AIR 5504 : 2002 AIRCRAFT INFLIGHT ICING TERMINOLOGY
SAE ARP 5904 : 2002(R2012) AIRBORNE ICING TANKERS
DEFSTAN 00-970/VOL2/1(1984) : 1984 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT

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