A method of controlling thrust for a gas turbine engine of an aircraft is provided. The method includes determining a fan speed required for minimum thrust to achieve an aircraft operation. The method also includes determining an excess amount of thrust generated by the gas turbine engine. The method also includes reducing the amount of thrust generated by the gas turbine engine.
Aircraft power setting trims for life extension
12.03.2019
Patent
Elektronische Ressource
Englisch
Tema Archiv | 1985
|Online Contents | 2009
Engineering Index Backfile | 1964
Power switching trims digital system weight, cost.
NTRS | 1966
|