Air Conformal Ice Detection System (A.C.I.D.S) for the Power Optimised, Ice Protected Aircraft / Rotorcraft

2003-01-2103

06/16/2003

Event
FAA In-flight Icing / Ground De-icing International Conference & Exhibition
Authors Abstract
Content
Ice accretion on flying surfaces affects the aerodynamic performance and handling qualities of the aircraft, and may require different pilot corrective action, dependent upon the surface that ice is accreting onto. The current methodology for ice detection usually relies on an indirect method, normally based on ambient air temperature, and liquid water content. When a pre-set threshold level is reached, the ice protection system is activated, whether or not ice is accreting on critical surfaces. This method is not cost effective or efficient for an ice protection system.
Air Conformal Ice Detection obviates these problems by using a ‘direct’ method of detection, local to the critical area being monitored.
Meta TagsDetails
DOI
https://doi.org/10.4271/2003-01-2103
Pages
7
Citation
Armstrong, D., Hare, G., Kloeppel, V., Lawrence, M. et al., "Air Conformal Ice Detection System (A.C.I.D.S) for the Power Optimised, Ice Protected Aircraft / Rotorcraft," SAE Technical Paper 2003-01-2103, 2003, https://doi.org/10.4271/2003-01-2103.
Additional Details
Publisher
Published
Jun 16, 2003
Product Code
2003-01-2103
Content Type
Technical Paper
Language
English