HYBRID ENGINE ACCESSORY POWER SYSTEM

A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient change in power demand, a control valve operated by the control...

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Bibliographic Details
Main Authors SMITH, PETER, GERALD, WALTHER, RONALD, S, HAGAMAN, EDWARD, T, SCHRYVER, MATTHEW, J, SPOCK, WAYNE, R, GUKEISEN, ROBERT, L, MORRIS, TIMOTHY, M
Format Patent
LanguageEnglish
French
German
Published 26.07.2006
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:A system for generating accessory power from a gas turbine engine is provided by the present invention. The system includes an electronic control device for monitoring at least one parameter which provides information about an incipient change in power demand, a control valve operated by the control device for supplying bleed air from the engine during a transient state in response to the at least one monitored parameter, and a pneumatically operated device for receiving the bleed air and for generating power to operate equipment onboard an aircraft. The pneumatically operated device may be an air turbine or a pneumatically integrated generator.
Bibliography:Application Number: EP20040796461