Aircraft gas turbine engine control

Details Aircraft gas turbine engine control Aircraft gas turbine engine control

1991-12-09

1994-02-15

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 39281, F02C 928

Patent

active

052856348

ABSTRACT:
A normal acceleration schedule limits the rate of engine acceleration A second acceleration schedule permits a higher acceleration, which causes higher thermal stress in the hot engine parts. The higher schedule is enabled only during a landing approach, thus limiting the number of such stress cycles, while achieving improved performance for the selected mode.

REFERENCES:
patent: 4432201 (1984-02-01), Hawes
patent: 4449360 (1984-05-01), Evans
patent: 4500966 (1985-02-01), Zagranski et al.
patent: 4507915 (1985-04-01), Evans
patent: 4625510 (1986-12-01), Evans
patent: 5072578 (1991-12-01), Moore

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