AIRCRAFT BRAKING SYSTEM

The present disclosure relates to hybrid brake systems. The hybrid brake systems may comprise one or more electromechanical actuators (222-1, 222-2; 322-1, 322-2) and one or more hydraulic adjusters (224-1 to 224-6; 324-1 to 324-4). The hybrid brake system may further comprise a housing (226; 326) configured to store and/or conduct fluid. The hybrid brake system may also further comprise a fluid reservoir (328-1, 328-2). The hybrid brake system may be redundant.