High Efficiency Ice Protection System (HEIPS) for Aircraft Engine Inlets

2004-01-3110

11/02/2004

Event
World Aviation Congress & Exposition
Authors Abstract
Content
Goodrich Aerostructures Group and Goodrich De-icing and Specialty Systems Division (DSSD) are jointly developing an electrical High Efficiency Ice Protection system (HEIPS) for aircraft engine inlets. Engine Inlets designed with HEIPS technology, will improve efficiency of the engine and provide a lower weight inlet structure, when compared to a conventional hot air Thermal Anti-ice (TAI) system. In addition eliminating the pressures and temperatures associated with the traditional pneumatic anti-ice system is a breakthrough that allows for new nacelle concepts to be considered, including the use of conventional acoustic treatment in the lip area. The latter is important because aircraft noise is a major driver in current and future aircraft design, since international noise regulations are becoming more and more stringent.
Meta TagsDetails
DOI
https://doi.org/10.4271/2004-01-3110
Pages
8
Citation
Brown, K., Layland, M., and Sweet, D., "High Efficiency Ice Protection System (HEIPS) for Aircraft Engine Inlets," SAE Technical Paper 2004-01-3110, 2004, https://doi.org/10.4271/2004-01-3110.
Additional Details
Publisher
Published
Nov 2, 2004
Product Code
2004-01-3110
Content Type
Technical Paper
Language
English