Method and device for controlling disc brakes
AssigneeSociete Nationale Industrielle Aerospatiale
InventorsLouis Signorelli, Alain Yves Louis Marcel Geoffroy
Life of this patent
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Abstract
The present invention relates to a method and device for controlling a hydraulic disc brake, particularly for heavy-transport aircraft, wherein the functioning of the brake is servo-controlled so that the braking torque which it exerts follows the variations of a predetermined reference torque.
Claims10
A method for controlling a hydraulic disc brake, particularly for aircraft, said brake being associated with at least one wheel and actuated by a mobile member, comprising the following steps:
- detecting the braking torque actually exerted on the wheel;
- servo-controlling said actual braking torque by a reference braking torque such that a predetermined value of said reference torque corresponds to a determined displacement of said mobile member, the value of the reference torque increasing with the displacement of said mobile member up to a certain position, beyond which the reference torque takes a maximum threshold value indpendent of said displacement.
A method for controlling a hydraulic disc brake, particularly for aircraft, said brake being associated with at least one wheel and actuated by a mobile member, comprising the following steps:
- detecting the braking torque actually exerted on the wheel;
- servo-controlling said actual braking torque by a reference braking torque such that a predetermined value of said reference torque corresponds to a determined displacement of said mobile member, the actual braking torque being controlled by a first reference torque when the wheel advances at a speed greater than a speed threshold and by a second reference torque when this speed is lower than said speed threshold, the values of the reference torques increasing with the displacement of said mobile member up to certain positions thereof, beyond which the reference torques take maximum threshold values independent of said displacement and the maximum threshold value of the second reference torque being greater than the maximum value of the threshold of the first.
A method for controlling a hydraulic disc brake, particularly for aircraft, said brake being associated with at least one wheel and actuated by a mobile member, comprising the following steps:
- actuating said mobile member for direct control of the brake;
- detecting the braking torque actually exerted on the wheel;
- comparing said detected braking torque with a predetermined value;
- and
- if said detected value is lower than said predetermined value, allowing said mobile member to continue to directly actuate the brake;
- or
- if said detected value is greater than said predetermined value, servo-controlling said detected braking torque by a reference braking torque, such that a determined value of said reference braking torque corresponds to a determined displacement of said mobile member;
- the reference torque being zero at the moment when the braking torque obtained by direct action reaches said predetermined value.
A method for controlling a hydraulic disc brake, particularly for aircraft, said brake being associated with at least one wheel and actuated by a mobile member, comprising the following steps:
- actuating said mobile member for direct control of the brake;
- detecting the braking torque actually exerted on the wheel;
- comparing said detected braking torque with a predetermined value;
- and
- if said detected value is lower than said predetermined value, allowing said mobile member to continue to directly actuate the brake;
- or
- if said detected value is greater than said predetermined value, servo-controlling said detected braking torque by a reference braking torque, such that a determined value of said reference torque corresponds to a determined displacement of said mobile member;
- and
- when the speed of the wheel is lower than a speed threshold, the brake is actuated directly in the sense of braking, whilst the servo-control functions only in the sense of a brake release.
A device for controlling a hydraulic disc brake associated with at least one wheel of a vehicle, particularly an aircraft, and actuated by a mobile actuating member, said device comprising:
- a transducer for converting the displacement of said actuating member into an electric signal and a servo-valve for controlling the hydraulic fluid in the brakes controlled by a control winding;
- at least one sensor producing a first electric signal representing the braking torque actually exerted on the wheel when the brake is actuated by said actuating member and supplying this first electric signal to a device, arranged between said transducer and said control winding, producing, as a function of the displacement of said actuating member, at least a second electric signal representing a reference braking torque to be obtained and controlling the feed of said control winding by said second signal;
- said device further comprising, between the transducer and control winding of the servo-valve, an electric circuit composed of two branches in parallel which may be used alternately, the first of said branches corresponding to the direct action of said member on the brake and the second to the torque servo-control of the functioning of the brake;
- and,
- associated with said second branch of the circuit, at least a first contact which, in rest position, inhibits the action of said branch, whilst with the first branch of circuit is associated a second contact allowing, in rest position, the action of said second branch;
- said device further comprising means producing a signal indicating simultaneously that the servo-valve is energized and that the braking torque is greater than the predetermined value, the signal produced by said first means being able to trip the first and second contacts;
- a third contact whose rest position normally inhibits the functioning of the first circuit branch, mounted in parallel on the second contact, and a fourth contact associated with the second circuit branch, so that at rest, said fourth contact allows the action of said second circuit branch;
- said third and fourth contacts being actuated by second means producing a signal indicating that the speed of the wheel is greater than said speed threshold and, in its operating position, said fourth contact allowing the functioning of the servo-control only in the sense of a brake release.
A device for controlling a hydraulic disc brake associated with at least one wheel of a vehicle, particularly an aircraft, and actuated by a mobile actuating member, said device comprising:
- a transducer for converting the displacement of said actuating member into an electric signal and a servo-valve for controlling the hydraulic fluid in the brakes controlled by a control winding;
- at least one sensor producing a first electric signal representing the braking torque actually exerted on the wheel when the brake is actuated by said actuating member and supplying the first electric signal to an apparatus, arranged between said transducer and said control winding, producing, as a function of the displacement of said actuating member, at least a second electric signal representing a reference braking torque to be obtained and controlling the feed of said control winding by said second signal;
- said device further comprising, between the transducer and control winding of the servo-valve, an electric circuit composed of two branches in parallel which may be used alternately, the first of said branches corresponding to the direct action of said member on the brake and the second to the torque servo-control of the functioning of the brake;
- said second branch comprising a servo-control device functioning both for braking and brake-release, a unidirectional conduction device being associated with said servo-control device in order that only its brake-release action be transmitted to the servo-valve.
Dependencies are inferred from the claim text.