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https://drivepatents.com/patents/1004826 · 29 Feb 2012
The method involves determining (22) and displaying (24) a possible continuous utilization duration (DELTA-T) of a first power e.g. maximum takeoff power, when an engine e.g. turboshaft engine, of a power plant of an aircraft develops a second power greate...
https://drivepatents.com/patents/1098532 · 5 Feb 2003
A control strategy for a gas turbine engine exchanges future lifetime of the engine for present thrust. Gas turbine engines, such as those used in aircraft, sometimes incur damage, as when they ingest birds, or are struck with ballistic objects fired by an...