G - Physics – 01 – L
Patent
G - Physics
01
L
G01L 3/24 (2006.01) B64D 45/00 (2006.01)
Patent
CA 2614828
The invention concerns a piloting indicator (1) comprising data sources (2) which determine the parameter values concerning the propeller and the turbine of the turboprop, as well as the parameter values concerning the aircraft, processing means (3) which calculate, based on said values, a power parameter which takes into account the ratio between the current power of the turboprop engine and the maximum power obtained without air bleed at sea level in standard atmosphere, and display means (5) which display, on a viewing screen (7), at least one characteristic symbol (11) illustrating said power parameter.
L'indicateur de pilotage (1) comporte des sources d'informations (2) qui déterminent les valeurs de paramètres relatifs à l'hélice et à Ia turbine du turbopropulseur, ainsi que les valeurs de paramètres relatifs à l'aéronef, des moyens de traitement (3) qui calculent, à partir de ces valeurs, un paramètre de puissance qui tient compte du rapport entre la puissance courante du turbopropulseur et la puissance maximale obtenue sans prélèvement d'air au niveau de la mer en atmosphère standard, et des moyens d'affichage (5) qui présentent, sur un écran de visualisation (7), au moins un signe caractéristique (11) illustrant ledit paramètre de puissance.
Airbus
Robic
LandOfFree
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