AC BUS TIE CONTACTOR INPUT INTO RAT AUTO-DEPLOY

AC BUS TIE CONTACTOR INPUT INTO RAT AUTO-DEPLOY

A system includes a first AC bus (102) configured to supply power from a first generator (104). A first generator line contactor (GLC) (106) selectively connects the first AC bus to the first generator. A second AC bus (108) is configured to supply power from a second generator (110). A second GLC (...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: IVES, Kyle, MYROTH, Jeffrey D, TRASER, Shane R, GOOD, Jef William, BUZZARD, John N, VANEVENHOVEN, Jordan K
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER
CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
COSMONAUTICS
ELECTRICITY
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERATION
PARACHUTES
PERFORMING OPERATIONS
SYSTEMS FOR STORING ELECTRIC ENERGY
TRANSPORTING
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Beschreibung
Zusammenfassung:A system includes a first AC bus (102) configured to supply power from a first generator (104). A first generator line contactor (GLC) (106) selectively connects the first AC bus to the first generator. A second AC bus (108) is configured to supply power from a second generator (110). A second GLC (112) selectively connecting the second AC bus to the second generator. An auxiliary generator line contactor (ALC) (114) is connected to selectively supply power to the first and second AC buses from an auxiliary generator (116). A first bus tie contactor (BTC) (118) electrically connects between the first GLC and the ALC. A second BTC (120) electrically connects between the ALC and the second GLC. A ram air turbine (RAT) automatic deployment controller (122) is operatively connected to automatically deploy a RAT (124) based on the combined status of the first GLC, the second GLC, the ALC, the first BTC, and the second BTC.