G - Physics – 01 – K
Patent
G - Physics
01
K
G01K 13/02 (2006.01)
Patent
CA 2641923
The invention relates to a method for determining the total temperature of an airflow surrounding an aircraft, comprising the following steps: measurement of a static temperature parameter, measurement of a total temperature parameter, determination of an airflow speed value, determination of a total temperature calculated from the static temperature parameters and the measured total temperature as a function of the airflow speed.
L'invention concerne un procédé de détermination de la température totale du flux d'air environnant un aéronef, comportant les opérations suivantes; mesure d'un paramètre de température statique, mesure d'un paramètre de température totale, détermination d'une valeur de vitesse du flux d'air, détermination d'une température totale calculée à partir des paramètres de température statique mesurée et de température totale mesurée, en fonction de la vitesse du flux d'air.
Brivet Valerie
Gaucheron Philippe
Saint-Aroman Stephane
Airbus France
Airbus Operations Sas
Bcf Llp
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