Generating electrical power at high thrust conditions

A gas turbine engine for an aircraft comprising a high pressure (HP) spool, HP compressor 105, a first electric machine 117 having a first maximum output power and driven by HP turbine 107, low-pressure (LP) spool, a second electric machine 119 having a second maximum output power and driven by LP t...

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Bibliographische Detailangaben
1. Verfasser:	Caroline Louise Turner
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER DYNAMO-ELECTRIC MACHINES ELECTRICITY ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS GENERATION HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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