Patent ID: 11939047
Assignee: AIRBUS HELICOPTERS
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B

Claim 2:
3. The method according to claim 1,
wherein the method comprises using a position sensor to measure a current position of an interface controlling a mean pitch of each blade of the at least one propeller, the interface being able to move between a first position and a second position shown by ends of the first scale, the first scale being graduated in positions of the interface, the method comprising the following steps:
using the computer to determine the maximum power, the minimum power and the current power;
displaying, on the display controlled by the computer, the index as a function of the current position;
displaying, on the display controlled by the computer, the maximum power mark relative to the index as a function of a first difference between the current power and the maximum power; and
displaying, on the display controlled by the computer, the minimum power mark relative to the index as a function of a second difference between the current power and the minimum power.