Supplemental power for reduction of prime mover
Supplemental power for reduction of prime mover
- New search for: SIMONETTI JOSEPH LAWRENCE
- New search for: BYSTRY MARK DENTON
- New search for: DEVITA MICHAEL JOSEPH
- New search for: TARASCIO MATTHEW J
- New search for: STRAUSS MICHAEL PETER
- New search for: REEVE HAYDEN M
- New search for: DESAI NIRANJAN
- New search for: ST ROCK BRIAN
- New search for: LENTS CHARLES E
- New search for: ZEIDNER LAWRENCE E
- New search for: SMILEY ALFRED RUSSELL
- New search for: SIMONETTI JOSEPH LAWRENCE
- New search for: BYSTRY MARK DENTON
- New search for: DEVITA MICHAEL JOSEPH
- New search for: TARASCIO MATTHEW J
- New search for: STRAUSS MICHAEL PETER
- New search for: REEVE HAYDEN M
- New search for: DESAI NIRANJAN
- New search for: ST ROCK BRIAN
- New search for: LENTS CHARLES E
- New search for: ZEIDNER LAWRENCE E
- New search for: SMILEY ALFRED RUSSELL
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.
Document information
Supplemental power for reduction of prime mover
2020-02-25
Patent
Electronic Resource
English
| IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Similar titles
| NTRS | 1992
| NTIS | 1992