SUPPLEMENTAL POWER FOR REDUCTION OF PRIME MOVER

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SUPPLEMENTAL POWER FOR REDUCTION OF PRIME MOVER

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SIMONETTI JOSEPH LAWRENCE / BYSTRY MARK DENTON / DEVITA MICHAEL JOSEPH / TARASCIO MATTHEW J / STRAUSS MICHAEL PETER / REEVE HAYDEN M / DESAI NIRANJAN / ST ROCK BRIAN / LENTS CHARLES E / ZEIDNER LAWRENCE E / ... [more]

Abstract

Embodiments are directed to selecting, by a computing device comprising a processor, the size of at least one prime mover associated with an aircraft to satisfy a baseline power requirement for operation of the aircraft during a steady state load condition, selecting at least one power source configuration to supplement power provided by the at least one prime mover during a transient load condition associated with the operation of the aircraft, and selecting, by the computing device, a parameter of the at least one power source configuration to provide a total power in an amount that is greater than a threshold during the transient condition.

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Title :

SUPPLEMENTAL POWER FOR REDUCTION OF PRIME MOVER

Additional title:

ZUSÄTZLICHE LEISTUNG ZUR REDUZIERUNG EINES ANTRIEBSAGGREGATS
ÉNERGIE SUPPLÉMENTAIRE POUR RÉDUCTION D'UN MOTEUR D'ENTRAINEMENT

Contributors:

SIMONETTI JOSEPH LAWRENCE (author) / BYSTRY MARK DENTON (author) / DEVITA MICHAEL JOSEPH (author) / TARASCIO MATTHEW J (author) / STRAUSS MICHAEL PETER (author) / REEVE HAYDEN M (author) / DESAI NIRANJAN (author) / ST ROCK BRIAN (author) / LENTS CHARLES E (author) / ZEIDNER LAWRENCE E (author)

Publication date :

2020-02-19

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT