Pilot indicator for aircraft, designed to display engine...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 43/00 (2006.01) G01D 7/00 (2006.01) G01D 1/12 (2006.01) G01D 13/00 (2006.01)

Patent

CA 2363308

L'indicateur (1) comporte des moyens d'acquisition et de traitement (2, 3) qui déterminent la valeur effective du rapport de pressions moteur et des moyens d'affichage (4) pourvus d'un cadran (6) et d'une aiguille (7) dont la position sur le cadran (6) correspond à ladite valeur effective. De plus, les moyens d'acquisition et de traitement (2, 3) déterminent des valeurs minimale et maximale pour le rapport de pressions moteur, et les moyens d'affichage (4) présentent sur le cadran (6) un secteur circulaire (8) qui est délimité par deux rayons (8A, 8B) dont les posi-tions correspondent respectivement auxdites valeurs minimale et maxi-male.

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