SAE AIR1667A
Current
The latest, up-to-date edition.
ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS
Hardcopy , PDF
English
23-04-2013
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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 AIR4015D | 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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