EMERGENCY BRAKE SYSTEM WITH DUAL INPUT

EMERGENCY BRAKE SYSTEM WITH DUAL INPUT

Systems and methods for emergency brake systems are provided herein. In this regard, a brake system (10) may comprise a summing lever (20) having a first end (50) and a second end (52), a brake handle (12) coupled to the first end (50) of the summing lever (20), the brake handle (12) rotatably coupl...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SUMMERS, Herbert S, AYICHEW, Efrem E
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL
AVIATION
BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL
CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BYMECHANICAL FEATURES ONLY
CONTROLLING
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES
REGULATING
TRANSPORTING
VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF
VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:Systems and methods for emergency brake systems are provided herein. In this regard, a brake system (10) may comprise a summing lever (20) having a first end (50) and a second end (52), a brake handle (12) coupled to the first end (50) of the summing lever (20), the brake handle (12) rotatably coupled about a first axis (40), and a linear actuator (22) having a plunger (23), the plunger (23) being coupled to the second end (52) of the summing lever (20). In various embodiments, an idler link (18) may be coupled between the brake handle (12) and the first end (50) of the summing lever (20). The brake system (10) may further comprise a brake cable (30) coupled between the summing lever (20) and a brake metering valve (36). The brake metering valve (36) may be actuated in response to at least one of the brake handle (12) being rotated about the first axis (40) or the linear actuator (22) being actuated.