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10/29/09 - USPTO Class 188 |  1 views | #20090266652 | Prev - Next | About this Page  188 rss/xml feed  monitor keywords

Brake force transducer for electric brakes

USPTO Application #: 20090266652
Title: Brake force transducer for electric brakes
Abstract: An electric brake actuator and force transducer for the brake system of an aircraft is presented. A brake actuator includes a piston driven by a cylindrical nut and screw arrangement, driven by an appropriate motor of the actuator. Application of brake force results in a reactionary force that deflects the top cover of the actuator. The axial component of this deflection correlates directly with the brake force applied. A beam is interposed between this cover and a top cap, such that deflection of the beam correlates to applied brake face. Piezo-resistive devices are connected to the beam and, through a whetstone bridge, provide an electrical output signal correlating to applied brake force. (end of abstract)



Agent: Renner Kenner Greive Bobak Taylor & Weber - Akron, OH, US
Inventors: KEVIN M. DALTON, KEVIN M. DALTON, KURT BURKHALTER, KURT BURKHALTER, MICHAEL P. OSBURN, MICHAEL P. OSBURN, HAROLD R. BOOHER, HAROLD R. BOOHER
USPTO Applicaton #: 20090266652 - Class: 188 111E (USPTO)

Brake force transducer for electric brakes description/claims


The Patent Description & Claims data below is from USPTO Patent Application 20090266652, Brake force transducer for electric brakes.

Brief Patent Description - Full Patent Description - Patent Application Claims
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This is a continuation of application Ser. No. 11/433,020, filed May 11, 2006, for Brake Force Transducer for Electric Brakes, now U.S. Pat. No. ______.

TECHNICAL FIELD

The invention herein resides in the art of vehicle braking systems and, more particularly, to aircraft braking system. Specifically, the invention relates to electric brake systems for use on aircraft, in which motor driven actuators control the application and release of brake force generated in a brake disc stack. The invention specifically relates to a brake force transducer for use in such electric brake systems.

BACKGROUND ART

The use of electric brakes in aircraft systems has become increasingly popular. In such systems, electric motors are employed to drive a piston through gears, screws and the like, into a pressure plate of a brake disc stack. Typically, there are a plurality of actuators about each brake assembly, generally uniformly distributed thereabout.

Control of electric braking requires that the actuator clamping force be known and adjusted similar to adjusting the pedal pressure for a hydraulic brake. With hydraulics, a change in pressure is proportional to a change in clamping force and the brake control is based on this. No similar, simple relation exists with electric actuation as the input power measured in voltage and current can vary widely with clamping force depending on whether the motor is moving fast or slow, forward or reversing, or under load. When no practical feedback sensor can be integrated into the electric actuator, force estimation methods are employed often based on motor position from a reference point, the assumed stiffness of the brake frame, motor current draw and other factors. These become complex algorithms and at best provide only an estimated force output that can be in relatively large error due to changes in the frame stiffness, twist in the frame during braking, and uneven brake disk wear, to name a few. Therefore, it is highly desirable to have a reliable and independent sensor of motor clamping force as the current invention describes.

In electric brake systems, it is important that the brake force applied by the actuators be controllable and, in that regard, readily monitored. In the past, load cells have been proposed and used. In such systems, the load cells have been placed upon the brake actuator housing or carrier plate. However, various problems incident to this structure have been encountered. Particularly, as the carrier plate and/or housing deform under load, the load cells themselves deform and lose accuracy. Moreover, deflection and deformation of the carrier plate or housing, and consequent deformation of the load cells, adds a non-axial component to the force reading. However, it is known that the effective braking force from an electric brake disc actuator is axial. Accordingly, the load cell in the prior art has been found to read components that are not brake force components, and which either do not result in the generation of brake force, or result in more brake force than what was requested by the controller. This greatly reduces the accuracy of the data obtained from such load cells, since only the axial component of any actuator\'s force contributes to brake force. As a consequence, accuracy and integrity of the monitoring system is greatly compromised.

DISCLOSURE OF THE INVENTION

In light of the foregoing, it is a first aspect of the invention to provide an electric brake actuator having a force transducer that responds to the axial component of brake force application.

Another aspect of the invention is to provide an electric brake actuator having a force transducer that remains accurate throughout its operation.

Still another aspect of the invention is the provision of an electric brake actuator having a force transducer that provides an output correlated linearly with brake force.

Yet another aspect of the invention is to provide an electric brake actuator having a force transducer that is pre-loaded to assure accuracy throughout its life.

Yet another aspect of the invention is to provide an electric brake actuator having a force transducer that is protected from the elements and the environment.

A further aspect of the invention is to provide an electric brake actuator having a force transducer using piezo-electric devices in a bridge arrangement for reliable and durable use.

Still a further aspect of the invention is to provide an electric brake actuator having a force transducer that is easy to implement with presently existing components and to be employed in presently existing systems.

The foregoing and other aspects of the invention that will become apparent as the detailed description proceeds are achieved by a force transducer for an electric brake actuator, said force transducer adapted for interposition between a top cover and a cap of the brake actuator, said force transducer comprising: an elongated member adapted to be restrained at an outer portion thereof by the cap and at an inner portion thereof by the top cover, said elongated member receiving a biasing member centrally thereof and normal thereto, said biasing member being adjustably adapted to urge said elongated member away from the top cover and toward the cap, the biasing member being threadedly received by said elongated member and having an end thereof adapted to engage the top cover.

Other aspects of the invention are attained by a force transducer, comprising: an elongated member restrained at each of two opposite ends thereof, and configured for force application at a center region thereof; and a plurality of sensors attached to said elongated member and responding to deflection of said elongated member.

DESCRIPTION OF DRAWINGS

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Brief Patent Description - Full Patent Description - Patent Application Claims

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