Gkn Aerospace Services Limited

David John Armstrong

Peter English

Maxwell E Brown

Aristedis Anthony Ikiades

Thomas Stephen Rowe Richards

George Graham Hare

Glen R Pringle

Mary Konstantaki

Maxwell Edward Brown

Glen Robert Pringle

An ice-protection system has first and second zones of a leading edge of an aerodynamic or streamlined aerodynamic component, each zone having a de-icing apparatus and an ice-detection sensor positioned behind an elongated convex window as to be aero-conformal with the leading edge. The ice-detection sensor is in the form of a module and has a sensor head having a front face and abutments at ends of the window. The ice-detection sensors may have a central light emitter and a plurality of sensor elements peripheral to the light emitter. The ice-protection system also has a control system responsive to the ice-detection sensors to control the respective de-icing apparatus, and may activate automatically a sequence of operation.

Ice protection system

An aircraft wing slat for mounting to a leading portion of an aircraft wing includes a main body section and a forward section, wherein the forward section is demountable from or releasably secured to the main body section. The forward section may have a nose skin with an electrically powered heater. The electrically powered heater may be integral with the nose skin and may be microporous such that it is integrated into surrounding dielectric to contribute to the mechanical strength of the nose skin. A demountable forward section of an aircraft wing slat, a main body section of an aircraft wing slat arranged to receive a demountable forward section, an aircraft wing and an aircraft wing slat with a nose skin with an electrically powered heater are also disclosed.

Aircraft wing slat

Ice detection apparatus for monitoring ice accretion on aircraft surfaces, comprising an array of optical fibres which are mounted flush with an outer surface of an aircraft skin, and an intermediately located electromagnetic radiation emitter which is provided by an optical fibre. In use radiation is emitted by the emitter generally outwardly of the aircraft surface, and the layer of accreted ice diffuses the emitted radiation scattered and reflected. The diffused radiation is detected by the sensors, and the spatial distribution of the detected intensity diffused radiation about the emitter can be used to calculate the thickness of the layer of ice and the type of ice.

Ice detection apparatus and method

Growing community of inventors

Luton, United Kingdom

David John Armstrong