Patent Application
20160169310
The present disclosure relates to position sensors, and more particularly, to contactless linear position sensors.
Conventional aircraft systems, including braking systems, utilize various types of sensors to relay information to control systems. Such information may include the position of various components relative to other components. Sensors may be used, for example, to relay the linear position of an actuator, such as an electromechanical actuator. Further, such sensors may utilize moving parts or parts that are in physical contact with other parts.
Sensors and their components may become worn or damaged from continued use. Therefore, it may be beneficial to provide sensors of a contactless nature, which may reduce damage or wear associated with moving and contacting components of the sensors.
In various embodiments, a contactless position sensor system may comprise a piston disposed within a housing having a channel along a portion of an inner surface and configured to be linearly displaced, a magnet coupled to the piston, and a RF-based magnetic sensor positioned within a portion of the channel and configured to detect the position of the magnet within the piston. The magnet may be embedded in a tab coupled to the piston. The RF-based magnetic sensor may comprise an electronic circuit and may also include an antenna. The piston may comprise a fully extended position and a fully retracted position, and the sensor may be configured to detect the linear displacement of the piston between the fully extended position and the fully retracted position.
In various embodiments, a brake system may comprise an electromechanical actuator, a piston configured to be linearly displaced within the housing, and a RF-based magnetic sensor positioned within a channel of the housing and configured to detect a magnetic field of a magnet coupled to the piston. The RF-based magnetic sensor may comprise an electronic circuit and may transmit positional data to a sensor interface, which may process the signal into a linear position in the X direction. The magnet may be embedded in a tab coupled to the piston. The RF-based magnetic sensor may comprise an electronic circuit and may also include an antenna. The piston may comprise a fully extended position and a fully retracted position, and the sensor may be configured to detect the linear displacement of the piston between the fully extended position and the fully retracted position.
The subject matter of the present disclosure is particularly pointed out and distinctly claimed in the concluding portion of the specification. A more complete understanding of the present disclosure, however, may best be obtained by referring to the detailed description and claims when considered in connection with the drawing figures, wherein like numerals denote like elements.
The detailed description of exemplary embodiments herein makes reference to the accompanying drawings, which show exemplary embodiments by way of illustration and their best mode. While these exemplary embodiments are described in sufficient detail to enable those skilled in the art to practice the disclosure, it should be understood that other embodiments may be realized and that logical changes may be made without departing from the spirit and scope of the disclosure. Thus, the detailed description herein is presented for purposes of illustration only and not of limitation. For example, the steps recited in any of the method or process descriptions may be executed in any order and are not necessarily limited to the order presented. Furthermore, any reference to singular includes plural embodiments, and any reference to more than one component or step may include a singular embodiment or step.
The present disclosure describes exemplary contactless position sensor systems which may be used in aircraft applications. For example, contactless sensor systems may be utilized with new braking system designs, or retrofitted into existing braking systems. Various potential applications include electromechanical actuators, cockpit pedal sensors, brake accumulators, and multi-position switches, among others. Further, contactless position sensor systems of the present disclosure may be used in systems other than aircraft systems, including any system that utilizes telescoping concentric tubes.
With initial reference to
With initial reference to
Actuator 102 may further comprise a piston 204 located within housing 206. For example, piston 204 may be configured to move linearly, along an X axis, within housing 206. In various embodiments, piston 204 may move linearly between a fully extended position 220 and a fully retracted position 222.
In various embodiments, actuator 102 may comprise a sensor system 208. For example, sensor system 208 may comprise a permanent magnet 212. Magnet 212 may, for example, be coupled to piston 204. In various embodiments, magnet 212 may be embedded in or coupled to a tab 214 located on piston 204. Any manner of coupling magnet 212 and piston 204 is within the scope of the present disclosure.
Housing 206 may define a channel 218 along a portion of an inner surface 224, which may be aligned with tab 214 of piston 204. In various embodiments, piston 204 is positioned such that tab 214 moves linearly (i.e., along the X axis) within housing 206.
Sensor system 208 may further comprise, for example, a sensor 210. In various embodiments, sensor 210 may determine the linear positon (i.e., along the x axis) of piston 204 in a contactless manner. Sensor 210 may, for example, be located within channel 218 of housing 206. In various embodiments, sensor 210 is in proximity to tab 214, which is oriented such that it moves linearly within channel 218. In such embodiments, sensor 210 is aligned with and in proximity to, but not in contact, magnet 212. Sensor 210 may comprise a length in the x direction approximately equal to the range over which the linear position of piston 204 is to be measured. For example, sensor 210 may comprise a length equal to the linear displacement of piston 204 between fully extended position 220 and fully retracted position 222
Sensor 210 may be press-fit or glued into channel 218. However, any manner of securing sensor 210 relative to housing 206 and piston 204 is within the scope of the present disclosure.
In various embodiments, sensor 210 comprises an electronic circuit capable of detecting the position of magnet 212. For example, an electromagnetic effect induced by magnet 212 at certain positions may facilitate detection of the position of magnet 212 by sensor 210. In various embodiments, magnet 212 may impact the shielding characteristics of material (e.g., metal) surrounding an antenna 216 of sensor 210, which may consequently impact an output voltage in sensor 210. The output voltage may then, for example, be interpreted and/or analyzed to determine the position of magnet 212. For example, magnet 212 may decrease the electromagnetic permeability of the material surrounding antenna 216, causing an increased output voltage in sensor 210. The increased output voltage may correspond to the position of magnet 212, and therefore, piston 204. However, any manner of detecting the position of magnet 212 by sensor 210 is within the scope of the present disclosure. For example, in various embodiments, sensor 210 comprises a radio frequency (RF) magnet sensor.
Sensor 210 may, for example, be capable of detecting the position of magnet 212 through a material, such as, for example, a metal. For example, magnet 212 may be entirely embedded in tab 214 such that sensor 210 detects magnet 212 through a wall or portion of tab 214. As such, magnet 212 may be protected from adverse environmental conditions (such as, for example, excessive heat, dirt, and/or humidity).
Sensor system 208 may, for example, comprise an antenna 216. Antenna 216 may be electrically coupled to sensor 210. For example, sensor 210 may comprise an electronic circuit including an antenna. In various embodiments, antenna 216 provides data about the linear position of magnet 212, and therefore piston 204, to a component of an aircraft.
With reference to
In various embodiments, sensor interface 330 processes data provided from sensor system 208 to produce data that accurately relates the linear position of piston 204 to a system interface 332. In various embodiments, system interface 332 comprises a control computer within an aircraft. However, system interface 332 can comprise any computer, processing system, controller, or interface capable of receiving linear position data from sensor interface 330.
Benefits, other advantages, and solutions to problems have been described herein with regard to specific embodiments. Furthermore, the connecting lines shown in the various figures contained herein are intended to represent exemplary functional relationships and/or physical couplings between the various elements. It should be noted that many alternative or additional functional relationships or physical connections may be present in a practical system. However, the benefits, advantages, solutions to problems, and any elements that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as critical, required, or essential features or elements of the disclosure. The scope of the disclosure is accordingly to be limited by nothing other than the appended claims, in which reference to an element in the singular is not intended to mean “one and only one” unless explicitly so stated, but rather “one or more.” Moreover, where a phrase similar to “at least one of A, B, or C” is used in the claims, it is intended that the phrase be interpreted to mean that A alone may be present in an embodiment, B alone may be present in an embodiment, C alone may be present in an embodiment, or that any combination of the elements A, B and C may be present in a single embodiment; for example, A and B, A and C, B and C, or A and B and C.
Systems, methods and apparatus are provided herein. In the detailed description herein, references to “various embodiments”, “one embodiment”, “an embodiment”, “an example embodiment”, etc., indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Further, when a particular feature, structure, or characteristic is described in connection with an embodiment, it is submitted that it is within the knowledge of one skilled in the art to affect such feature, structure, or characteristic in connection with other embodiments whether or not explicitly described. After reading the description, it will be apparent to one skilled in the relevant art(s) how to implement the disclosure in alternative embodiments.
Furthermore, no element, component, or method step in the present disclosure is intended to be dedicated to the public regardless of whether the element, component, or method step is explicitly recited in the claims. No claim element herein is to be construed under the provisions of 35 U.S.C. 112(f), unless the element is expressly recited using the phrase “means for.” As used herein, the terms “comprises”, comprising”, or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
