Ice Detection Systems - A Historical Perspective
Document Number: 2007-01-3325
Date Published: September 2007
Author(s):
Darren Jackson - Goodrich Sensor Systems
Joshua Goldberg - Retired, Hamilton Sundstrand Corporation
Abstract:
Ice protection systems were installed on DC-3s, B-29s and other aircraft during World War II. Initially ice detection was not considered a requirement for aircraft safety. One of the earliest ice detectors installed on a production aircraft (C-130) was pneumatic. Subsequently many other technologies have been applied to detect the presence of meteorological icing. Ice detectors employing visible light, infrared light, alpha radiation, natural resonance frequency, capacitance, speed of sound, heat of fusion, and microwaves have all been developed over the years. This paper will review the different ice detection technologies and explore some of the similarities, differences, benefits and drawbacks for the purposes of performing their intended function. One of the drivers for developing new ice detection technology has been aircraft icing accidents and incidents. For example, a number of MD-80 accidents caused by engine flame-outs during take-off have prompted development of surface-based ice detection solutions that could detect ice accretion on wing surfaces prior to take-off. Other accidents such as the Comair CRJ crash in Fredericton, New Brunswick, Canada and the American Eagle ATR-42/72 crash in Roselawn, Indiana have spurred research into different ice detection technologies related to the Ludlam Limit and Supercooled Large Droplets (SLD) respectively. This paper will review various aircraft accidents and incidents that have had an impact on ice detection technology. While no Federal Aviation Regulations (FARs) exist today which deal specifically with ice detection systems, there has been some industry guidance material published which provides information on the design of ice detection systems. Due to the increased industry awareness of aircraft icing issues, a number of industry committees such as EUROCAE and IPHWG have been established to develop new guidance material and proposed regulation changes related to ice detection systems. The release of the ED-103/104 Minimum Operational Performance Specifications and other guidance material such as the recent updates to AC 20-73 published by the FAA have had an impact on the development and certification of ice detection systems. This paper will review the regulation changes that impact ice detection system design and certification, including a discussion regarding the ability of ice detection technologies to meet these requirements and to be certified as a Primary system.
File Size: 414K
Product Status: In Stock
See other papers presented at 2007 SAE Aircraft and Engine Icing International Conference, September 2007, Seville, SPAIN, Session: In-flight Ice Detection Systems
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