B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 43/00 (2006.01) B64D 31/00 (2006.01) B64D 45/00 (2006.01) G01C 23/00 (2006.01) G01D 7/04 (2006.01)
Patent
CA 2495862
A device for indicating a residual power margin of aircraft turbine engines includes a measuring stage associated with at least one turbine engine of an aircraft to measure a number of first parameters related to a power output of the engine; a calculating unit associated with the measuring unit to calculate at least one second parameter indicating the power output of the engine on the basis of the first parameters; and a display. The display includes a power scale having at least one reference indicator indicating an operating limit of the engine; and at least one cursor cooperating with the power scale and the reference indicator to simultaneously display a current value of the second parameter and an available power margin of the engine.
Agusta S.p.a.
Ridout & Maybee Llp
LandOfFree
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