Patents by Inventor Steven F. Griffin
Steven F. Griffin 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: 12348846Abstract: A retrofittable subassembly that enhances the operational availability of a terrestrial optical surveillance system is disclosed. In various embodiments, the subassembly comprises a diffusely reflective and insulating external cover, a highly uniform plate-glass cover, an wide angle FOV camera and a passive thermal control system.Type: GrantFiled: October 12, 2021Date of Patent: July 1, 2025Assignee: The Boeing CompanyInventors: Richard B. Holmes, Steven F. Griffin
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Patent number: 12234015Abstract: An apparatus and method for suppressing free play chatter of a control surface of an aircraft. The free play chatter suppression apparatus includes a containment vessel connected to a control surface of an aircraft. A lossy material is contained within the containment vessel. A body is positioned within the lossy material. The deceleration of the body by the lossy fluid is transmitted to the control surface to dampen vibrations of the control surface.Type: GrantFiled: June 21, 2023Date of Patent: February 25, 2025Assignee: The Boeing CompanyInventors: Steven F. Griffin, Zackary L. Endsley
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Patent number: 12189137Abstract: A system and method are provided for super-resolution imaging beyond the Rayleigh spatial resolution limit of an optical system. In the context of a system, first and second pinhole assemblies are configured to be controllably positioned. The first and second pinhole assemblies define respective pinholes and being configured to be backlit. The system also includes a collimating lens configured to collimate at least a portion of the signals passing through the respective pinholes of the first and second pinhole assemblies. The system further includes an amplitude/phase mask configured to provide amplitude and phase modulation to signals received from the collimating lens and an imaging lens configured to focus the signals received from the amplitude/phase mask upon an image plane to permit objects to be separately identified.Type: GrantFiled: February 23, 2022Date of Patent: January 7, 2025Assignee: The Boeing CompanyInventors: Edwin P. Walker, Steven F. Griffin, Sudhakar Prasad
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Publication number: 20240425172Abstract: An apparatus and method for suppressing free play chatter of a control surface of an aircraft. The free play chatter suppression apparatus includes a containment vessel connected to a control surface of an aircraft. A lossy material is contained within the containment vessel. A body is positioned within the lossy material. The deceleration of the body by the lossy fluid is transmitted to the control surface to dampen vibrations of the control surface.Type: ApplicationFiled: June 21, 2023Publication date: December 26, 2024Inventors: Steven F. Griffin, Zackary L. Endsley
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Publication number: 20240410165Abstract: Methods, systems, and apparatuses are disclosed for reducing sound level, by providing enclosures comprising enclosure walls having integral tunable resonator cavities, and reducing sound levels within the enclosure in response to detected sound levels outside of the enclosure.Type: ApplicationFiled: August 21, 2024Publication date: December 12, 2024Inventors: Naval Kishore Agarwal, Steven F. Griffin
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Patent number: 11987345Abstract: Methods and apparatus for variable stiffness supports in aircraft testing are disclosed. A disclosed example apparatus includes a variable stiffness support including a pad to contact and support the aircraft, and a spring operatively coupled to the pad. The apparatus also includes an actuator operatively coupled to the support, a sensor, at least one memory, machine executable instructions and at least one processor. The at least one processor is to execute the instructions to determine at least one of a movement or a displacement of the pad based on information from the sensor, and control movement of the actuator based on the determined at least one movement or distance of the pad to statically support the aircraft while enabling movement of the pad above a threshold frequency.Type: GrantFiled: July 5, 2022Date of Patent: May 21, 2024Assignee: The Boeing CompanyInventors: Steven F. Griffin, Eric Y. Reichenbach
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Publication number: 20240010329Abstract: Methods and apparatus for variable stiffness supports in aircraft testing are disclosed. A disclosed example apparatus includes a variable stiffness support including a pad to contact and support the aircraft, and a spring operatively coupled to the pad. The apparatus also includes an actuator operatively coupled to the support, a sensor, at least one memory, machine executable instructions and at least one processor. The at least one processor is to execute the instructions to determine at least one of a movement or a displacement of the pad based on information from the sensor, and control movement of the actuator based on the determined at least one movement or distance of the pad to statically support the aircraft while enabling movement of the pad above a threshold frequency.Type: ApplicationFiled: July 5, 2022Publication date: January 11, 2024Inventors: Steven F. Griffin, Eric Y. Reichenbach
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Publication number: 20230266602Abstract: A system and method are provided for super-resolution imaging beyond the Rayleigh spatial resolution limit of an optical system. In the context of a system, first and second pinhole assemblies are configured to be controllably positioned. The first and second pinhole assemblies define respective pinholes and being configured to be backlit. The system also includes a collimating lens configured to collimate at least a portion of the signals passing through the respective pinholes of the first and second pinhole assemblies. The system further includes an amplitude/phase mask configured to provide amplitude and phase modulation to signals received from the collimating lens and an imaging lens configured to focus the signals received from the amplitude/phase mask upon an image plane to permit objects to be separately identified.Type: ApplicationFiled: February 23, 2022Publication date: August 24, 2023Applicant: THE BOEING COMPANYInventors: Edwin P. WALKER, Steven F. GRIFFIN, Sudhakar PRASAD
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Publication number: 20230235552Abstract: Methods, systems, and apparatuses are disclosed for reducing sound level, by providing enclosures comprising enclosure walls having integral tunable resonator cavities, and reducing sound levels within the enclosure in response to detected sound levels outside of the enclosure.Type: ApplicationFiled: January 27, 2022Publication date: July 27, 2023Inventors: Naval Kishore Agarwal, Steven F. Griffin
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Patent number: 11676570Abstract: A noise cancellation system for cancelling sounds within a vehicle. The noise cancellation system includes microphones, a camera, a controller, and speakers. The microphones are disposed adjacent to occupant locations, and configured to generate microphone signals representative of noise sounds and cancellation audio sounds. The camera is configured to generate a video signal that captures head configurations of the occupants. The controller is configured to receive rotor control signals, calculate hearing locations based on tracking data of the head configurations of the occupants, and generate a speaker signals based on the hearing locations, the microphone signals, and the rotor control signals. The speakers are configured to generate the cancellation audio sounds. The cancellation audio sounds attenuate the noise sounds.Type: GrantFiled: February 9, 2022Date of Patent: June 13, 2023Assignee: The Boeing CompanyInventor: Steven F. Griffin
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Patent number: 11595759Abstract: An energy harvesting circuit is disclosed and comprises one or more electrical loads that consume direct current (DC) power, a rectifier, and a hybrid acoustic absorber. The rectifier comprises one or more active switching elements that are driven by a gate drive voltage. The hybrid acoustic absorber comprises a diaphragm and a voice coil. The diaphragm is constructed at least in part of a piezoelectric material. The piezoelectric material is configured to generate a diaphragm voltage in response to sound waves deforming the diaphragm. The diaphragm voltage is at least equal to the gate drive voltage to drive the one or more active switching elements of the rectifier. The voice coil is attached to the diaphragm and configured to generate a voice coil voltage that is less than the gate drive voltage of the one or more active switching elements.Type: GrantFiled: April 15, 2020Date of Patent: February 28, 2023Assignee: THE BOEING COMPANYInventors: Steven F. Griffin, Daryn D. Kono, Timothy John Paulitz, James Benjamin Turner
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Patent number: 11548626Abstract: Embodiments herein describe mitigating flexible modes in an airframe of an aircraft by operating a battery for the aircraft as a tuned mass damper. One embodiment comprises an Unmanned Aerial Vehicle (UAV). The UAV includes a flexible airframe, a plurality of propulsors coupled to the flexible airframe that generate thrust for the UAV, a battery that provides electrical power for the plurality of propulsors, and a suspension system that suspends the battery from the flexible airframe and operates the mass of the battery as a tuned mass damper to dampen flexible modes generated in the flexible airframe during flight.Type: GrantFiled: July 11, 2019Date of Patent: January 10, 2023Assignee: The Boeing CompanyInventors: Steven F Griffin, Robert J Atmur, Adam R Weston
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Publication number: 20220375449Abstract: A noise cancellation system for cancelling sounds within a vehicle. The noise cancellation system includes microphones, a camera, a controller, and speakers. The microphones are disposed adjacent to occupant locations, and configured to generate microphone signals representative of noise sounds and cancellation audio sounds. The camera is configured to generate a video signal that captures head configurations of the occupants. The controller is configured to receive rotor control signals, calculate hearing locations based on tracking data of the head configurations of the occupants, and generate a speaker signals based on the hearing locations, the microphone signals, and the rotor control signals. The speakers are configured to generate the cancellation audio sounds. The cancellation audio sounds attenuate the noise sounds.Type: ApplicationFiled: February 9, 2022Publication date: November 24, 2022Applicant: The Boeing CompanyInventor: Steven F. Griffin
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Patent number: 11480603Abstract: A testing system for monitoring a machine under test is disclosed and includes one or more high frequency sensors configured to generate a sensor signal that is representative of an operating parameter of the machine. The high frequency sensors have a required high frequency sampling rate. The testing system also includes a notification device configured to generate a notification indicating the operating parameter monitored by the high frequency sensors has exceeded a predefined threshold value and a data acquisition control module configured to monitor the high frequency sensors at a first sampling rate. The testing system also includes a monitoring control module in electronic communication with the notification device. The monitoring control module is configured to monitor the high frequency sensors at a second sampling rate that is greater than the first sampling rate and at least equal to the required high frequency sampling rate.Type: GrantFiled: March 20, 2020Date of Patent: October 25, 2022Assignee: THE BOEING COMPANYInventors: Steven F Griffin, Matthew Scot Stauffer, Matthew Novick, Daryn D Kono, Kevin P Moore
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Patent number: 11459116Abstract: An example system includes a processor and a non-transitory computer-readable medium having stored therein instructions that are executable to cause the system to perform various functions. The functions include: (i) acquiring an image of a first aerial vehicle, the image depicting an object of a second aerial vehicle prior to contact between the object and a surface of the first aerial vehicle; (ii) providing the image as input to a data-driven analyzer that is trained in a supervised setting with example images for determining a predetermined point of contact between the object and the surface of the first aerial vehicle; (iii) determining, based on an output of the data-driven analyzer corresponding to the input, an estimated point of contact between the object and the surface of the first aerial vehicle; and (iv) providing the estimated point of contact to a display system.Type: GrantFiled: June 24, 2020Date of Patent: October 4, 2022Assignee: The Boeing CompanyInventors: Trent M. Kyono, Steven F. Griffin, Jacob A. Lucas, James L. Clayton, Justin C. Hatcher
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Patent number: 11410336Abstract: A method for visual signal processing of a signal includes subdividing a signal, by a signal processor, into a selected number (n) of sets of data. The method also includes assembling the signal, by the signal processor, into an image. The image includes a matrix. The matrix includes a plurality of cells in a predetermined number (m) of columns and the selected number (n) of rows. Each cell of the matrix includes a particular color corresponding to an amplitude of a sample of the signal represented by the cell. The method also includes analyzing the image, by the signal processor, using an image detection algorithm to determine frequency information of the signal.Type: GrantFiled: October 1, 2019Date of Patent: August 9, 2022Assignee: The Boeing CompanyInventor: Steven F. Griffin
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Publication number: 20210403175Abstract: An example system includes a processor and a non-transitory computer-readable medium having stored therein instructions that are executable to cause the system to perform various functions. The functions include: (i) acquiring an image of a first aerial vehicle, the image depicting an object of a second aerial vehicle prior to contact between the object and a surface of the first aerial vehicle; (ii) providing the image as input to a data-driven analyzer that is trained in a supervised setting with example images for determining a predetermined point of contact between the object and the surface of the first aerial vehicle; (iii) determining, based on an output of the data-driven analyzer corresponding to the input, an estimated point of contact between the object and the surface of the first aerial vehicle; and (iv) providing the estimated point of contact to a display system.Type: ApplicationFiled: June 24, 2020Publication date: December 30, 2021Inventors: Trent M. Kyono, Steven F. Griffin, Jacob A. Lucas, James L. Clayton, Justin C. Hatcher
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Publication number: 20210329384Abstract: An energy harvesting circuit is disclosed and comprises one or more electrical loads that consume direct current (DC) power, a rectifier, and a hybrid acoustic absorber. The rectifier comprises one or more active switching elements that are driven by a gate drive voltage. The hybrid acoustic absorber comprises a diaphragm and a voice coil. The diaphragm is constructed at least in part of a piezoelectric material. The piezoelectric material is configured to generate a diaphragm voltage in response to sound waves deforming the diaphragm. The diaphragm voltage is at least equal to the gate drive voltage to drive the one or more active switching elements of the rectifier. The voice coil is attached to the diaphragm and configured to generate a voice coil voltage that is less than the gate drive voltage of the one or more active switching elements.Type: ApplicationFiled: April 15, 2020Publication date: October 21, 2021Inventors: Steven F Griffin, Daryn D. Kono, Timothy John Paulitz, James Benjamin Turner
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Publication number: 20210293875Abstract: A testing system for monitoring a machine under test is disclosed and includes one or more high frequency sensors configured to generate a sensor signal that is representative of an operating parameter of the machine. The high frequency sensors have a required high frequency sampling rate. The testing system also includes a notification device configured to generate a notification indicating the operating parameter monitored by the high frequency sensors has exceeded a predefined threshold value and a data acquisition control module configured to monitor the high frequency sensors at a first sampling rate. The testing system also includes a monitoring control module in electronic communication with the notification device. The monitoring control module is configured to monitor the high frequency sensors at a second sampling rate that is greater than the first sampling rate and at least equal to the required high frequency sampling rate.Type: ApplicationFiled: March 20, 2020Publication date: September 23, 2021Inventors: Steven F. Griffin, Matthew Scot Stauffer, Matthew Novick, Daryn D. Kono, Kevin P. Moore
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Patent number: 11118857Abstract: A spin-stabilizing assembly is usable with a cylindrical barrel having a longitudinal center axis, a vertical center axis, and a distal end. The assembly includes a gimbal piece, a spinner cage, and a spinner body. A first end of the gimbal piece engages an outer diameter surface of the barrel proximate the distal end. The spinner cage is configured to engage a second end of the gimbal piece, and to pivot with respect thereto about the vertical center axis. The spinner body is disposed radially within the spinner cage and defines multiple axial vanes. The vanes, in response to impingement on the axial vanes of exhaust gases discharged from the distal end of the barrel, rotate the spinner body about the longitudinal center axis. Rotation results in impedance along the vertical center axis which minimizes vertical displacement or motion of the distal end.Type: GrantFiled: January 22, 2020Date of Patent: September 14, 2021Assignee: The Boeing CompanyInventors: Steven F. Griffin, Jacob A. Lucas, Alexander Klein