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US 2024/0228028 A1Published application
Anti-lock braking system
AssigneeSafran Landing Systems UK LTD
InventorTom LOVE
Life of this patent
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Abstract
An anti-lock braking system for an aircraft, including a braking actuator configured to apply a braking pressure to a brake stator, and a piezoelectric actuator connected in series with the braking actuator. The piezoelectric actuator is operable to modify the braking pressure applied to the brake stator to provide anti-skid protection.
Claims15
An anti-lock braking system for an aircraft, comprising:
- a braking actuator configured to apply a braking pressure to a brake stator;
- and
- a piezoelectric actuator integrated with the braking actuator, wherein the piezoelectric actuator is operable to modify the braking pressure applied to the brake stator to provide anti-skid protection.
An aircraft landing gear comprising:
- an anti-lock braking system for an aircraft, comprising:
- a braking actuator configured to apply a braking pressure to a brake stator;
- and
- a piezoelectric actuator integrated with the braking actuator, wherein the piezoelectric actuator is operable to modify the braking pressure applied to the brake stator to provide anti-skid protection.
1 more element
An aircraft comprising an aircraft landing gear, the aircraft landing gear comprising:
- an anti-lock braking system for an aircraft, comprising:
- a braking actuator configured to apply a braking pressure to a brake stator;
- and
- a piezoelectric actuator integrated with the braking actuator, wherein the piezoelectric actuator is operable to modify the braking pressure applied to the brake stator to provide anti-skid protection.
1 more element
Dependencies are inferred from the claim text.