Patent classifications
F16D65/84
MECHANICAL BRAKE FOR FLYWHEELS
The flywheel device includes a sealed housing section; a rotor located in the sealed housing section where the rotor is held in a vertical position by a magnetic system; a controller coupled to the magnetic system; and a braking annular ring mounted to the sealed housing section below the rotor, where the rotor contacts the braking annular ring when the rotor is lowered or otherwise dropped from the vertical position. The controller perform operations to provide control signals to provide first power to the magnetic system to hold the rotor in the vertical position and provide second control signals to provide second power to the magnetic system to lower the rotor.
ROTOR DRIVE KEY ASSEMBLY
In some examples, an assembly includes a rotor drive key configured to fit around a wheel boss defined by a wheel of a vehicle. The rotor drive key includes a support member. The assembly further comprises a fastener configured to extend through the wheel boss and the support member in a substantially axial direction of the wheel when the rotor drive key is fit around the wheel boss. A fastening member is configured to engage with a portion of the fastener extending beyond the support member.
ROTOR DRIVE KEY ASSEMBLY
In some examples, an assembly includes a rotor drive key configured to fit around a wheel boss defined by a wheel of a vehicle. The rotor drive key includes a support member. The assembly further comprises a fastener configured to extend through the wheel boss and the support member in a substantially axial direction of the wheel when the rotor drive key is fit around the wheel boss. A fastening member is configured to engage with a portion of the fastener extending beyond the support member.
FAILSAFE PISTON PRESSURE PATH
A piston assembly is disclosed herein. The piston assembly includes a piston having a first end, an opposing second end, and a sidewall extending from the first end to the second end, the piston further including a cavity at least partially defined by the sidewall, a spring guide having a first end and an opposing second end, the spring guide disposed within the cavity of the piston and adjacent the sidewall, an insulator having a first portion extending from the second end of the piston and a second portion disposed within the piston, an insulator shield disposed adjacent the first portion of the insulator, and a component coupled to the second end of the spring guide, the component being offset from the insulator shield by a distance.
FAILSAFE PISTON PRESSURE PATH
A piston assembly is disclosed herein. The piston assembly includes a piston having a first end, an opposing second end, and a sidewall extending from the first end to the second end, the piston further including a cavity at least partially defined by the sidewall, a spring guide having a first end and an opposing second end, the spring guide disposed within the cavity of the piston and adjacent the sidewall, an insulator having a first portion extending from the second end of the piston and a second portion disposed within the piston, an insulator shield disposed adjacent the first portion of the insulator, and a component coupled to the second end of the spring guide, the component being offset from the insulator shield by a distance.
BRAKING SYSTEM FOR AN AIRCRAFT WHEEL
A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).
BRAKING SYSTEM FOR AN AIRCRAFT WHEEL
A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).
CAST IRON AND CERAMIC COMPOSITE DISC BRAKE
A cast iron and ceramic composite disc brake includes a brake surface, wherein the brake surface is provided with a plurality of annularly arranged grooves in a circular direction, the annularly arranged groove is provided with a filler, and the filler is made of a ceramic resin fiber. In the present disclosure, the gray cast iron and the ceramic fiber resin material are composited under a high pressure, which greatly reduces the weight, greatly increases a friction coefficient, and shortens a braking distance by . Moreover, the installation is convenient, and the heat dissipation performance and the heat resistance performance are better, which is safe and reliable to use.
COOLING DUCTS FOR DISC BRAKE CALIPER AND METHOD OF MANUFACTURE THEREOF
The present invention relates to a disc brake caliper body comprising a mounting side bracket and a non-mounting side bracket extending along a circumferential direction of the body, each bracket being configured to hold at least one brake pad. In order to provide improved cooling efficiency while maintaining the required stability of the brake caliper, the caliper body further comprises at least one cooling duct formed by additive manufacturing, at least one cooling duct being an integral part of the caliper body.
BRAKING DEVICE
A braking device configured to brake rotation of a shaft of a transmission is disclosed. The braking device includes a housing attachable to a casing of a transmission, a braking part and a lubrication structure. The braking part is disposed in the interior of the housing, and includes a plurality of braking discs. The lubrication structure includes a supply part and a discharge part, and lubricates the braking discs of the braking part. The supply part supplies oil to the interior of the housing, and includes a first supply port that is provided in a member different from the shaft and is disposed radially inside the braking part. The discharge part discharges the oil, supplied to the interior of the housing, to the casing of the transmission, and includes a discharge flow pathway that axially extends and is provided on the outer peripheral side of the plurality of braking discs.