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Active standard | Published: 01/04/2013
SAE AIR1667A
Rotor Blade Electrothermal Ice Protection Design Considerations
Available languages: English
Available design: electronic design (pdf), Print design
from 144.20 EUR
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Detail information
Designation: SAE AIR1667A
Publication date: 01/04/2013
Pages: 0
Country: American technical standard
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You can buy at www.mystandards.bizAnotation
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.
SUBJECT TAXONOMY: Aircraft deicing, Certification
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
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