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ROTOR BLADE ELECTROTHERMAL ICE PROTECTION DESIGN CONSIDERATIONS
- Aerospace Standard
- AIR1667
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This 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. Although various concepts of ice protection are mentioned in this report, the text is limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A. Applications consider main rotor blades, conventional tail rotor blades, and other types of antitorque devices. The information contained in this report is also limited to the identification of factors that should be considered and why the factor is important. Specific design, analysis and test methodologies are not included. For additional information refer to the references in Section 7.
Topic
Data Sets - Support Documents
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Issuing Committee
AC-9C Aircraft Icing Technology Committee
Furthers the advancement of technology related to the research, design, test and utilization of aircraft environmental and anti-icing/deicing systems. Develops and updates standards, recommended practices, and information reports contributing to the quality, economy, and safety of commercial and military aircraft.
A list of the technical reports developed by the AC-9C Sub- Committee can be obtained by searching on 'aircraft icing' and selecting 'standards', from the SAE Home Page. AC-9C StandardsReference
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