HYBRID BRAKE SYSTEMS AND METHODS

A braking system (200) for an aircraft (100) is disclosed herein. The braking system (200) may comprise: a brake assembly (118; 218); a hydraulic braking subsystem (202) having a hydraulic brake actuator (217) configured to operate the brake assembly (118; 218); an electric braking subsystem (204) a...

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Bibliographische Detailangaben
Hauptverfasser:	GEORGIN, Marc, POISSON, Richard A
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL PERFORMING OPERATIONS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A braking system (200) for an aircraft (100) is disclosed herein. The braking system (200) may comprise: a brake assembly (118; 218); a hydraulic braking subsystem (202) having a hydraulic brake actuator (217) configured to operate the brake assembly (118; 218); an electric braking subsystem (204) and a hydraulic braking subsystem (202). During a flight, one of the electric braking subsystem (204) and the hydraulic braking subsystem (202) may be selected as a primary braking system (200). The braking system (200) may be configured to command braking of a brake assembly (118; 218) by the hydraulic braking subsystem (202) and the electric braking subsystem (204) during an RTO phase of the flight. The braking system (200) may be configured to command braking of a brake assembly (118; 218) by a secondary braking system (200) in response to a failure of a primary braking system (200) during the RTO phase of the flight.