Patents by Inventor Owen Williams
Owen Williams 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).
-
Publication number: 20220348327Abstract: The present disclosure provides a release launching system that is operative to receive and retain a drone or other payload in a protected launcher. The launcher helps to reduce the drag of the payload and to protect the payload from environmental factors. The payload is launched when a force initially separates the payload from the launcher and exposes a force generating mechanism. The force generating mechanism may be within the body portion of the device and generate an additional force to assist in separating the payload from the launcher. The payload may be launched using a biasing and fastening mechanism, which may include detachably coupling bracket, to allow for the separation of the payload from the launcher.Type: ApplicationFiled: March 10, 2022Publication date: November 3, 2022Inventors: Nicholas Robert Alley, Jesse Owen Williams, Matthew Gordon Brasher
-
Publication number: 20220347174Abstract: Invented are methods for treating HIV in a human in need thereof which comprises the administration of a therapeutically effective amount of a combination of cabotegravir or a pharmaceutically acceptable salt thereof and rilpivirine or a pharmaceutically acceptable salt thereof, to such human.Type: ApplicationFiled: October 1, 2020Publication date: November 3, 2022Inventors: Herta Maria Ludovica CRAUWELS, Susan L. FORD, David Andrew MARGOLIS, Stefaan Louis F. ROSSENU, William Robert SPREEN, Rodica Mihaela VAN SOLINGEN-RISTEA, Peter Evan Owen WILLIAMS
-
Publication number: 20220274704Abstract: The present disclosure provides rolling release launching system that is operative to receive and retain a drone or other payload in a protected launcher. The launcher helps to reduce the drag of the payload and to protect the payload from environmental factors. The payload is launched when a rotating door opens to expose the payload in a bay area. The rotating door may be parallel or concentric to a longitudinal axis of the body portion of the device. The payload may be launched using a biasing and fastening mechanism, which may include detachably coupling bracket, to induce an angular moment and releasing force on the payload during launch.Type: ApplicationFiled: January 3, 2022Publication date: September 1, 2022Inventors: Nicholas Robert Alley, Jesse Owen Williams, Matthew Gordon Brasher
-
Patent number: 11214370Abstract: The present disclosure provides rolling release launching system that is operative to receive and retain a drone or other payload in a protected launcher. The launcher helps to reduce the drag of the payload and to protect the payload from environmental factors. The payload is launched when a rotating door opens to expose the payload in a bay area. The rotating door may be parallel or concentric to a longitudinal axis of the body portion of the device. The payload may be launched using a biasing and fastening mechanism, which may include detachably coupling bracket, to induce an angular moment and releasing force on the payload during launch.Type: GrantFiled: November 5, 2020Date of Patent: January 4, 2022Assignee: Area-I Inc.Inventors: Nicholas Robert Alley, Jesse Owen Williams, Matthew Gordon Brasher
-
Publication number: 20210403143Abstract: An unmanned aerial vehicle with deployable components (UAVDC) may comprise a foldable propeller blade with a locking mechanism. Foldable propeller blades may have a stowed configuration and a deployed configuration relative to the UAVDC, and the foldable propeller blades may pivot about a hinge to move between configurations. In the deployed configuration, the foldable propeller may experience forward folding forces acting upon it. The locking mechanism may lock the foldable propeller blade in the deployed configuration. The locking mechanism may keep the foldable propeller locked into place to prevent forward folding tendency.Type: ApplicationFiled: September 10, 2021Publication date: December 30, 2021Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme
-
Publication number: 20210339865Abstract: The present disclosure provides rolling release launching system that is operative to receive and retain a drone or other payload in a protected launcher. The launcher helps to reduce the drag of the payload and to protect the payload from environmental factors. The payload is launched when a rotating door opens to expose the payload in a bay area. The rotating door may be parallel or concentric to a longitudinal axis of the body portion of the device. The payload may be launched using a biasing and fastening mechanism, which may include detachably coupling bracket, to induce an angular moment and releasing force on the payload during launch.Type: ApplicationFiled: November 5, 2020Publication date: November 4, 2021Inventors: Nicholas Robert Alley, Jesse Owen Williams, Matthew Gordon Brasher
-
Patent number: 11117649Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement. The UAVDC may also comprise a foldable propeller blade with a locking mechanism.Type: GrantFiled: March 28, 2017Date of Patent: September 14, 2021Assignee: Area-I Inc.Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme
-
Publication number: 20200139097Abstract: An injection device for injecting a solid dose formulation into a human or animal body, the injection device comprising an actuator having a cassette mounting portion; a cassette holder having a cassette storage portion; and a cassette selectively movable between the cassette storage portion and the cassette mounting portion, wherein, the cassette comprises a solid dose formulation and the actuator is receivable in the cassette holder to selectively move the cassette between the cassette storage portion and the cassette mounting portion.Type: ApplicationFiled: December 5, 2019Publication date: May 7, 2020Inventors: Colin CONLON, Derek FENLON, Pascal LAUNOIS, Martina MOYNE, Owen William RYAN
-
Publication number: 20200102065Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: ApplicationFiled: December 2, 2019Publication date: April 2, 2020Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Patent number: 10537724Abstract: An injection device for injecting a solid dose formulation into a human or animal body, the injection device comprising an actuator (10) having a cassette mounting portion (14); a cassette holder (20) having a cassette storage portion; and a cassette selectively movable between the cassette storage portion and the cassette mounting portion, wherein, the cassette (34) comprises a solid dose formulation and the actuator is receivable in the cassette holder to selectively move the cassette between the cassette storage portion and the cassette mounting portion.Type: GrantFiled: February 2, 2016Date of Patent: January 21, 2020Assignee: ENESI PHARMA LIMITEDInventors: Colin Conlon, Derek Fenlon, Pascal Launois, Martina Moyne, Owen William Ryan
-
Patent number: 10494081Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: GrantFiled: December 22, 2016Date of Patent: December 3, 2019Assignee: Area-I Inc.Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Patent number: 9954502Abstract: A multiport amplifier MPA is provided with an N-input input network, INET, an N-output output network, ONET, and N amplifiers interposed between the INET and the ONET, the MPA comprising N wanted signal paths and N.(N?1) null signal paths wherein N is divisible by 2, half of the N amplifier paths comprise a signal inversion with respect to the other half of the N amplifier paths, the INET and the ONET each comprise one or more quadrature hybrid couplers, QHC, wherein a pair of amplifier paths is arranged between the output of a first QHC in the INET and the input of a second QHC at the ONET, and each signal inversion is arranged in one of the amplifier paths of each pair of amplifier paths such that the ideal amplitude gain of at least one of the N.(N?i) null signal paths is zero.Type: GrantFiled: March 17, 2015Date of Patent: April 24, 2018Assignee: Airbus Defence and Space LimitedInventor: Owen William Clarke
-
Patent number: 9902488Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: GrantFiled: December 22, 2016Date of Patent: February 27, 2018Assignee: AREA-I INC.Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Patent number: 9902487Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: GrantFiled: December 22, 2016Date of Patent: February 27, 2018Assignee: AREA-I, INC.Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Publication number: 20180028798Abstract: An injection device for injecting a solid dose formulation into a human or animal body, the injection device comprising an actuator (10) having a cassette mounting portion (14); a cassette holder (20) having a cassette storage portion; and a cassette selectively movable between the cassette storage portion and the cassette mounting portion, wherein, the cassette (34) comprises a solid dose formulation and the actuator is receivable in the cassette holder to selectively move the cassette between the cassette storage portion and the cassette mounting portion.Type: ApplicationFiled: February 2, 2016Publication date: February 1, 2018Inventors: Colin CONLON, Derek FENLON, Pascal LAUNOIS, Martina MOYNE, Owen William RYAN
-
Publication number: 20170291684Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: ApplicationFiled: December 22, 2016Publication date: October 12, 2017Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Publication number: 20170291685Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: ApplicationFiled: December 22, 2016Publication date: October 12, 2017Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Publication number: 20170291686Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.Type: ApplicationFiled: December 22, 2016Publication date: October 12, 2017Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme, Jonathan Caleb Phillips
-
Publication number: 20170197702Abstract: An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement. The UAVDC may also comprise a foldable propeller blade with a locking mechanism.Type: ApplicationFiled: March 28, 2017Publication date: July 13, 2017Inventors: Nicholas Robert Alley, Joshua Lemming Steele, Jesse Owen Williams, Daniel Kuehme
-
Patent number: 9703452Abstract: A mobile communications device user interface is described. In an implementation, a method is implemented by a computing device that includes displaying content in conjunction with a first level of a hierarchical menu in a user interface on a display device of the computing device. Responsive to receipt of an input to navigate to a second level of the hierarchical menu that is a sublevel of the first level, the second level in displayed conjunction with the content on the display device, the content having a reduced display richness when displayed in conjunction with the second level than when displayed in conjunction with the first level.Type: GrantFiled: September 10, 2015Date of Patent: July 11, 2017Assignee: Microsoft Technology Licensing, LLCInventors: Michael J. Kruzeniski, Michael A. Smuga, Michael K. Henderlight, Brian M. Wilson, Chad A. Voss, Paula Guntaur, Jonathan David Friedman, Patrick S. Corrigan, Dustin Owen Williams, Joseph P. McLaughlin, Ryan T. Murphy