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SAE AIR1667A : 2013

Rotor Blade Electrothermal Ice Protection Design Considerations

Standard Details

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. 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 listed in 2.1 .

Cross Reference: AIR4015,AIR5504,ARP5903,ARP5904,ARP5905

General Information

Status : Reaffirmed
Standard Type: Main
Document No: SAE AIR1667A : 2013
Document Year: 2013
Pages: 49

Life Cycle

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Reaffirmed
SAE AIR1667A : 2013
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