Patents by Inventor Robert L. Fox
Robert L. Fox has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 7962252Abstract: A self-contained avionics sensing and flight control system is provided for an unmanned aerial vehicle (UAV). The system includes sensors for sensing flight control parameters and surveillance parameters, and a Global Positioning System (GPS) receiver. Flight control parameters and location signals are processed to generate flight control signals. A Field Programmable Gate Array (FPGA) is configured to provide a look-up table storing sets of values with each set being associated with a servo mechanism mounted on the UAV and with each value in each set indicating a unique duty cycle for the servo mechanism associated therewith. Each value in each set is further indexed to a bit position indicative of a unique percentage of a maximum duty cycle for the servo mechanism associated therewith. The FPGA is further configured to provide a plurality of pulse width modulation (PWM) generators coupled to the look-up table. Each PWM generator is associated with and adapted to be coupled to one of the servo mechanisms.Type: GrantFiled: June 8, 2006Date of Patent: June 14, 2011Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Qamar A. Shams, Michael J. Logan, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox, legal representative, John C. Ingham, Sean A. Laughter, Theodore R. Kuhn, III, James K. Adams, Walter C. Babel, III
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Patent number: 7732998Abstract: A telescoping actuator assembly includes a plurality of cylindrical actuators in a concentric arrangement. Each cylindrical actuator is at least one piezoelectric fiber composite actuator having a plurality of piezoelectric fibers extending parallel to one another and to the concentric arrangement's longitudinal axis. Each cylindrical actuator is coupled to concentrically-adjacent ones of the cylindrical actuators such that the plurality of cylindrical actuators can experience telescopic movement. An electrical energy source coupled to the cylindrical actuators applies actuation energy thereto to generate the telescopic movement.Type: GrantFiled: August 3, 2006Date of Patent: June 8, 2010Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox Chattin, legal representative
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Publication number: 20100118405Abstract: Actuator assemblies are formed by at least one cylinder where each cylinder is formed by at least one piezoelectric fiber composite actuator adapted to have actuation energy applied thereto.Type: ApplicationFiled: August 3, 2006Publication date: May 13, 2010Applicant: United States of America as represented by the Admins of the Ntl Aeronautics and Space AdminsInventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, Melanie L. Fox Chattin
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Patent number: 7580323Abstract: An optical assembly is formed by one or more piezoelectric fiber composite actuators having one or more optical fibers coupled thereto. The optical fiber(s) experiences strain when actuation voltage is applied to the actuator(s). Light passing through the optical fiber(s) is wavelength tuned by adjusting the actuation voltage.Type: GrantFiled: May 23, 2006Date of Patent: August 25, 2009Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdninistrationInventors: Sidney G. Allison, Qamar A. Shams, Robert L. Fox, Christopher L. Fox, legal representative, Melanie L. Fox Chattin, legal representative
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Patent number: 7262543Abstract: A system and method are provided for monitoring performance capacity of a piezoelectric material that may form part of an actuator or sensor device. A switch is used to selectively electrically couple an inductor to the piezoelectric material to form an inductor-capacitor circuit. Resonance is induced in the inductor-capacitor circuit when the switch is operated to create the circuit. The resonance of the inductor-capacitor circuit is monitored with the frequency of the resonance being indicative of performance capacity of the device's piezoelectric material.Type: GrantFiled: September 8, 2004Date of Patent: August 28, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert W. Moses, Christopher L. Fox, legal representative, Melanie L. Fox, legal representative, Richard L. Chattin, Qamar A. Shams, Robert L. Fox, deceased
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Patent number: 7197798Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises making a piezoelectric fiber sheet by providing a plurality of wafers of piezoelectric material, bonding the wafers together with an adhesive material to form a stack of alternating layers of piezoelectric material and adhesive material, and cutting through the stack in a direction substantially parallel to the thickness of the stack and across the alternating layers of piezoelectric material and adhesive material to provide at least one piezoelectric fiber sheet having two sides comprising a plurality of piezoelectric fibers in juxtaposition to the adhesive material. The method further comprises bonding two electrically conductive films to the two sides of the piezoelectric fiber sheet. At least one conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric fiber sheet.Type: GrantFiled: September 3, 2003Date of Patent: April 3, 2007Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Rosemary Jalink, legal representative, Bruce D. Little, Paul H. Mirick, Antony Jalink, Jr., deceased
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Patent number: 7086593Abstract: Magnetic field response sensors designed as passive inductor-capacitor circuits produce magnetic field responses whose harmonic frequencies correspond to states of physical properties for which the sensors measure. Power to the sensing element is acquired using Faraday induction. A radio frequency antenna produces the time varying magnetic field used for powering the sensor, as well as receiving the magnetic field response of the sensor. An interrogation architecture for discerning changes in sensor's response frequency, resistance and amplitude is integral to the method thus enabling a variety of measurements. Multiple sensors can be interrogated using this method, thus eliminating the need to have a data acquisition channel dedicated to each sensor. The method does not require the sensors to be in proximity to any form of acquisition hardware. A vast array of sensors can be used as interchangeable parts in an overall sensing system.Type: GrantFiled: April 30, 2004Date of Patent: August 8, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Stanley E. Woodard, Bryant D. Taylor, Qamar A. Shams, Christopher L. Fox, legal representative, Melanie L. Fox, legal representative, Robert G. Bryant, Robert L. Fox, deceased
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Patent number: 7038358Abstract: An electro-active transducer includes a ferroelectric material sandwiched by first and second electrode patterns. When the device is used as an actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto. In each case, the electrode patterns are designed to cause the electric field to: i) originate at a region of the ferroelectric material between the first and second electrode patterns, and ii) extend radially outward from the region of the ferroelectric material (at which the electric field originates) and substantially parallel to the ferroelectric material's plane.Type: GrantFiled: January 16, 2003Date of Patent: May 2, 2006Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Robert L. Fox
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Patent number: 7019621Abstract: A piezoelectric transducer comprises a piezoelectric component, an acoustic member attached to one of the surfaces of the piezoelectric component and a dampening material of low elastic modulus attached to one or both surfaces of the piezoelectric transducer. The piezoelectric component may comprise either an unimorph or a bimorph structure including a piezoceramic wafer made of lead zirconate titanate and a layer of dampening material sandwiched between the piezoelectric component and the acoustic member. The acoustic member comprises a surrounding wall portion and an end portion which form an acoustic chamber when the member is mounted on a surface of the piezoelectrie component. The end portion has an orifice to form a passageway from the chamber through the end portion to the outside of the member.Type: GrantFiled: January 2, 2001Date of Patent: March 28, 2006Inventors: Stanley E. Woodard, Robert L. Fox, Robert G. Bryant
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Patent number: 6919669Abstract: An electro-active transducer for sonic applications includes a ferroelectric material sandwiched by first and second electrode patterns to form a piezo-diaphragm coupled to a mounting frame. When the device is used as a sonic actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sonic sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto.Type: GrantFiled: March 12, 2003Date of Patent: July 19, 2005Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Robert L. Fox
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Patent number: 6734603Abstract: A method for forming ferroelectric wafers is provided. A prestress layer is placed on the desired mold. A ferroelectric wafer is placed on top of the prestress layer. The layers are heated and then cooled, causing the ferroelectric wafer to become prestressed. The prestress layer may include reinforcing material and the ferroelectric wafer may include electrodes or electrode layers may be placed on either side of the ferroelectric layer. Wafers produced using this method have greatly improved output motion.Type: GrantFiled: January 24, 1997Date of Patent: May 11, 2004Assignee: The United States of America as represented by the National Aeronautics and Space AdministrationInventors: Richard F. Hellbaum, Robert G. Bryant, Robert L. Fox, Antony Jalink, Jr., Wayne W. Rohrbach, Joycelyn O. Simpson
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Publication number: 20040040132Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises making a piezoelectric fiber sheet by providing a plurality of wafers of piezoelectric material, bonding the wafers together with an adhesive material to form a stack of alternating layers of piezoelectric material and adhesive material, and cutting through the stack in a direction substantially parallel to the thickness of the stack and across the alternating layers of piezoelectric material and adhesive material to provide at least one piezoelectric fiber sheet having two sides comprising a plurality of piezoelectric fibers in juxtaposition to the adhesive material. The method further comprises bonding two electrically conductive films to the two sides of the piezoelectric fiber sheet. At least one conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric fiber sheet.Type: ApplicationFiled: September 3, 2003Publication date: March 4, 2004Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Antony Jalink, Bruce D. Little, Paul H. Mirick
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Patent number: 6629341Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises providing a piezoelectric material that has two sides and attaching one side upon an adhesive backing sheet. The method further comprises slicing the piezoelectric material to provide a plurality of piezoelectric fibers in juxtaposition. A conductive film is then adhesively bonded to the other side of the piezoelectric material, and the adhesive backing sheet is removed. The conductive film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezoelectric material. The first and second conductive patterns of the conductive film each have a plurality of electrodes to form a pattern of interdigitated electrodes. A second film is then bonded to the other side of the piezoelectric material. The second film may have a pair of conductive patterns similar to the conductive patterns of the first film.Type: GrantFiled: October 29, 1999Date of Patent: October 7, 2003Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: W. Keats Wilkie, Robert G. Bryant, Robert L. Fox, Richard F. Hellbaum, James W. High, Antony Jalink, Jr., Bruce D. Little, Paul H. Mirick
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Publication number: 20030173872Abstract: An electro-active transducer includes a ferroelectric material sandwiched by first and second electrode patterns. When the device is used as an actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto. In each case, the electrode patterns are designed to cause the electric field to: i) originate at a region of the ferroelectric material between the first and second electrode patterns, and ii) extend radially outward from the region of the ferroelectric material (at which the electric field originates) and substantially parallel to the ferroelectric material's plane.Type: ApplicationFiled: January 16, 2003Publication date: September 18, 2003Applicant: Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Robert L. Fox
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Publication number: 20030173874Abstract: An electro-active transducer for sonic applications includes a ferroelectric material sandwiched by first and second electrode patterns to form a piezo-diaphragm coupled to a mounting frame. When the device is used as a sonic actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sonic sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto.Type: ApplicationFiled: March 12, 2003Publication date: September 18, 2003Applicant: USA as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Robert L. Fox
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Publication number: 20030056351Abstract: A method for fabricating a piezoelectric macro-fiber composite actuator comprises providing a piezo-electric material which has a first side and a second side. The method further comprises cutting the piezoelectric material to provide a plurality of piezoelectric fibers in juxtaposition. Two electrically conductive films are then adhesively bonded to the two sides of the piezo-electric material. The first film has first and second conductive patterns formed thereon which are electrically isolated from one another and in electrical contact with the piezo-electric material. In one embodiment, the second film does not have any conductive patterns. The first and second conductive patterns of the first film each have a plurality of electrodes to form a pattern of interdigitated electrodes. In another embodiment, the second film has a pair of conductive patterns similar to the conductive patterns of the first film.Type: ApplicationFiled: October 29, 1999Publication date: March 27, 2003Inventors: W. KEATS WILKIE, ROBERT G. BRYANT, ROBERT L. FOX, RICHARD F. HELLBAUM, JAMES W. HIGH, ANTONY JALINK, JR., BRUCE D. LITTLE, PAUL H. MIRICK
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Publication number: 20020121966Abstract: A personal communication device comprises a housing, a receiver component, a processor and a multi-functional piezoelectric transducer. The transducer is mounted within the housing, is electrically connected to the processor, and produces mechanical vibrations in response to the electrical signals transmitted by the processor. These mechanical vibrations are over a broad range of frequencies and are of a force sufficient to generate a tactile alert, an audible alert, and audible sound over the audible frequency range.Type: ApplicationFiled: January 2, 2001Publication date: September 5, 2002Inventors: Stanley E. Woodard, Robert L. Fox, Robert G. Bryant
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Publication number: 20010043027Abstract: A method for forming ferroelectric wafers is provided. A prestress layer is placed on the desired mold. A ferroelectric wafer is placed on top of the prestress layer. The layers are heated and then cooled, causing the ferroelectric wafer to become prestressed. The prestress layer may include reinforcing material and the ferroelectric wafer may include electrodes or electrode layers may be placed on either side of the ferroelectric layer. Wafers produced using this method have greatly improved output motion.Type: ApplicationFiled: January 24, 1997Publication date: November 22, 2001Inventors: RICHARD F. HELLBAUM, ROBERT G. BRYANT, ROBERT L. FOX, ANTONY JALINK, WAYNE W. ROHRBACH, JOYCELYN O. SIMPSON
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Patent number: 6259188Abstract: An alert apparatus for a personal communication device includes a mechanically prestressed piezoelectric wafer positioned within the personal communication device and an alternating voltage input line coupled at two points of the wafer where polarity is recognized. The alert apparatus also includes a variable frequency device coupled to the alternating voltage input line, operative to switch the alternating voltage on the alternating voltage input line at least between an alternating voltage having a first frequency and an alternating voltage having a second frequency. The first frequency is preferably sufficiently high so as to cause the wafer to vibrate at a resulting frequency that produces a sound perceptible by a human ear, and the second frequency is preferably sufficiently low so as to cause the wafer to vibrate at a resulting frequency that produces a vibration readily felt by a holder of the personal communication device.Type: GrantFiled: August 31, 1999Date of Patent: July 10, 2001Assignee: Projects Unlimited, Inc.Inventors: Stanley E. Woodard, Richard F. Hellbaum, Robert H. Daugherty, Raymond C. Scholz, Bruce D. Little, Robert L. Fox, Gerald A. Denhardt, SeGon Jang, Rizza Balein
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Patent number: 6190589Abstract: A molded magnetic article and fabrication method are provided. Particles of ferromagnetic material embedded in a polymer binder are molded under heat and pressure into a geometric shape. Each particle is an oblate spheroid having a radius-to-thickness aspect ratio approximately in the range of 15-30. Each oblate spheroid has flattened poles that are substantially in perpendicular alignment to a direction of the molding pressure throughout the geometric shape.Type: GrantFiled: February 11, 2000Date of Patent: February 20, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Robert G. Bryant, Min Namkung, Russell A. Wincheski, Robert L. Fox