An anti-ice arrangement (301) for a gas turbine engine (300) comprises an engine static structure (236), a fan blade (242) housed for rotation within the engine static structure (236), and a magnetic field source (310a, 310b, 310c) mounted in close proximi...

An example method of aircraft engine control includes detecting a difference between a temperature detected by a first temperature sensor (52) and a temperature detected by a second temperature sensor (58). Anti-icing activity is initiated in response to t...

A flight display for an aircraft includes a virtual ice accretion meter having a liquid water content portion and an ice thickness portion. A method for determining ice accretion includes integrating over a time period a constant K multiplied by a liquid w...