A brake system includes a reservoir and a motor-driven master cylinder operable during a backup braking mode by actuation of an electric motor of the master cylinder to generate brake actuating pressure at first and second MC outputs. A power transmission unit provides pressurized hydraulic fluid to a PTU output for actuating first and second pairs of wheel brakes in a normal non-failure braking mode. The power transmission unit includes a side-mounted electric PTU motor configured to selectively pressurize the hydraulic fluid by transmitting rotary motion to a ball nut assembly of the power transmission unit via a force translator mechanically interposed between the electric PTU motor and the ball nut assembly. First and second two-position three-way valves each selectively control hydraulic fluid flow from a chosen one of the master cylinder and the power transmission unit to a corresponding pair of wheel brakes.

A brake system for selectively actuating at least one wheel brake includes a reservoir and a power transmission unit for selectively providing pressurized hydraulic fluid for actuating at least a selected one of the wheel brakes during a braking event. A first electronic control unit at least partially controls at least one of the power transmission unit and a selected one of the pair of rear brake motors. A second electronic control unit at least partially controls at least one of the power transmission unit and an other one of the pair of rear brake motors. The first electronic control unit controls at least one SAP valve, an isolation valve, and a dump valve for a selected two of the wheel brakes, and the second electronic control unit controls at least one SAP valve, an isolation valve, and a dump valve for an other two of the wheel brakes.

A brake system includes a brake master cylinder assembly that is configured to connect to a brake pedal, and includes a master cylinder housing and a master cylinder piston being moveable inside the master cylinder housing and defining a compression chamber inside the master cylinder housing. A displacement sensor is mounted on the brake master cylinder assembly. An electro-hydraulic assembly is disposed separately from the brake master cylinder assembly, the electro-hydraulic assembly and the brake master cylinder assembly are connected by a connecting oil pipe and are in communication by a brake fluid in the connecting oil pipe, and the electro-hydraulic assembly is configured to connect to a wheel brake. A controller is connected to the displacement sensor and the electro-hydraulic assembly, and controls, according to an action of the brake pedal or a brake command, the electro-hydraulic assembly to output the brake fluid to the wheel brake.

A brake control system (BCS) may comprise a shutoff valve configured to receive pressurized fluid, a one-way check valve configured to route the pressurized fluid, a first pressure transducer coupled between the one-way check valve and the shutoff valve, and an accumulator configured to supply pressurized fluid to a brake control valve module (BCVM) in response to the shutoff valve being in a closed position.

A brake system for actuating a pair of front wheel brakes and a pair of rear wheel brakes includes a reservoir and a deceleration signal transmitter. First and second power transmission units are configured for selectively providing pressurized hydraulic fluid during a braking event. The first power transmission unit actuates a selected one of the front wheel brakes and a selected one of the rear wheel brakes. The second power transmission unit actuates the other one of the front wheel brakes and the other one of the rear wheel brakes. First and second electronic control units control the first and second power transmission units. A pair of rear brake motors selectively electrically actuate rear wheel brakes. Multiplex control of each of the pairs of front and rear wheel brakes is provided by an arrangement of first and second parallel valves for each wheel brake.

A VTOL aircraft (100) including a wheel braking system and a hydraulically coupled shock absorber (5) and brake piston (7). The shock absorber (5) carries the weight of the aircraft (100) when a wheel (1) connected to the shock absorber (5) is in contact with a ground surface. A hydraulic pressure within the shock absorber (5) is proportional to the weight of the aircraft (100) carried by the shock absorber (5). The shock absorber (5) and brake piston (7) are hydraulically coupled such that, when the pressure within the shock absorber (5) exceeds a threshold pressure, the pressure within the shock absorber (5) actuates the brake piston (7) to apply a braking torque to the wheel (1) of the VTOL aircraft (100).

A braking system for a motorcycle has a first braking device operatively connected to a first wheel of the motorcycle and having a first hydraulic supply circuit, a first electric actuator operatively connected to a first electrically or electro-mechanically actuated piston, and a first interface port operatively connected to a first hydraulic device provided with a first manually actuated piston subdivided into a first direct piston and a first indirect piston hydraulically connected to the first hydraulic supply circuit through a first by-pass duct. A hydraulic fluid reservoir is connected to the first hydraulic device by an upstream connection duct of the first indirect piston and a downstream connection duct of the first indirect piston. A processing and control unit is programmed so that, upon actuation of the first interface port, the first electrically or electro-mechanically actuated piston translates so as to occlude the first by-pass duct, fluidically disconnect the first manually actuated piston from the first hydraulic supply circuit, and simultaneously actuate the first braking device.

An aircraft braking system including a braking actuator; a primary hydraulic fluid supply circuit configured to supply pressurised hydraulic fluid to the braking actuator; and a secondary hydraulic fluid supply circuit including a piezoelectric pump configured to supply pressurised hydraulic fluid to the braking actuator.

The present disclosure relates to an electronic brake system. The electronic brake system includes a reservoir in which a pressurized medium is stored, an integrated master cylinder having a master chamber and a simulation chamber, a reservoir flow path provided to communicate the integrated master cylinder with the reservoir, a hydraulic pressure supply device provided to generate a hydraulic pressure by operating a hydraulic piston according to an electrical signal output in response to a displacement of the brake pedal, a hydraulic control unit including a first hydraulic circuit provided to control the hydraulic pressure to be transferred to two wheel cylinders, and a second hydraulic circuit provided to control the hydraulic pressure to be transferred to the other two wheel cylinders, and an electronic control unit configured to control valves based on hydraulic pressure information and displacement information of the brake pedal.

Disclosed herein an electronic brake system includes a hydraulic pressure supply device including a first pressure chamber and a second pressure chamber partitioned by a hydraulic piston, and a hydraulic control unit, wherein the hydraulic control unit comprises a first hydraulic flow path connecting the first pressure chamber and one of the first and second hydraulic circuits, a second hydraulic flow path branched from the first hydraulic flow path to connect to the other one of the first and second hydraulic circuits, a third hydraulic flow path branched from the first hydraulic flow path on upstream side of a branch point of the second hydraulic flow path to connect the second pressure chamber, and a fourth hydraulic flow path branched from the first hydraulic flow path on upstream side of a branch point of the third hydraulic flow path to connect the third hydraulic flow path.