Patents by Inventor Colin Hodges
Colin Hodges 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: 20230079478Abstract: Methods and systems describe providing face mesh deformation with detailed wrinkles. A neutral mesh based on a scan of a face is provided along with initial control point positions on the neutral mesh and user-defined control point positions corresponding to a non-neutral facial expression. A radial basis function (RBF) deformed mesh is generated based on RBF interpolation of the initial control point positions and the user-defined control point positions. Predicted wrinkle deformation data is then generated by one or more cascaded regressors networks. Finally, a final deformed mesh is provided with wrinkles based on the predicted wrinkle deformation data.Type: ApplicationFiled: February 10, 2021Publication date: March 16, 2023Inventors: Colin HODGES, David GOULD, Mark SAGAR, Tim WU, Sibylle VAN HOVE, Alireza NEJATI, Werner OLLEWAGEN, Xueyuan ZHANG
-
Patent number: 11164469Abstract: A method for aiding in the piloting of an aircraft landing on a runway comprises determining current flight conditions of the aircraft, determining a first approach distance using the current flight conditions, determining a current aircraft position and selection of a first point on a cockpit screen that is a function of the current position of the aircraft, selecting a second point in proximity to the landing runway, and controlling the display on the cockpit screen, of a first circular arc centered on the second point and whose radius is a function of the first approach distance, the first circular arc intersecting at a third point with a straight line passing through the first point and through the second point and the length of a part of the first circular arc situated between the third point and a first end of the first circular arc, comprising a predetermined length.Type: GrantFiled: March 18, 2019Date of Patent: November 2, 2021Assignee: Airbus Operations SASInventors: Colin Hodges, Elodie Saby, Philippe Toulemonde
-
Publication number: 20190304315Abstract: A method for aiding in the piloting of an aircraft landing on a runway comprises determining current flight conditions of the aircraft, determining a first approach distance using the current flight conditions, determining a current aircraft position and selection of a first point on a cockpit screen that is a function of the current position of the aircraft, selecting a second point in proximity to the landing runway, and controlling the display on the cockpit screen, of a first circular arc centered on the second point and whose radius is a function of the first approach distance, the first circular arc intersecting at a third point with a straight line passing through the first point and through the second point and the length of a part of the first circular arc situated between the third point and a first end of the first circular arc, comprising a predetermined length.Type: ApplicationFiled: March 18, 2019Publication date: October 3, 2019Inventors: Colin HODGES, Elodie SABY, Philippe TOULEMONDE
-
Patent number: 10228702Abstract: A method for optimizing the take-off parameters of an aircraft. The aircraft comprises a system for automatically controlling the high lift devices at the moment when the wheels of the aircraft leave the ground. The method comprises a step of selecting a first configuration of the high lift devices at the start of the take-off phase and a selection of an acceleration speed of the aircraft. The method is advantageous in that, on reception of an actual aircraft take-off detection signal, a control unit is configured to transmit a control command making it possible to bring the high lift devices into a second configuration, in which they are retracted relative to the first position, and consecutively accelerate the speed of the aircraft automatically to an acceleration speed entered by the pilot.Type: GrantFiled: May 31, 2017Date of Patent: March 12, 2019Assignee: Airbus Operations SASInventors: Jean-Pierre Demortier, Eric Petit, Christophe Homehr, Cyrille Thiers, Colin Hodges, Christian Lulla
-
Patent number: 9957134Abstract: An elevator roller guide assembly that provides enhanced ride comfort. The assembly includes a chassis, a stop plate mounted to the chassis, a face wheel enclosure that at least partially encloses the face wheel and is connected to a plurality of leaf springs, and a pair of side wheel enclosures connected to the face wheel enclosure by the plurality of leaf springs. The side wheel enclosures each support a side wheel in a fixed relation to the other side wheel. The side wheel enclosures are operably connected to the stop plate by a pair of vertical plates. A multi-axis damper extends from the stop plate to engage the face wheel enclosure and dampen oscillation of the wheel enclosures during operation. A set of delta diameter wheels across all four guides reduces coincident flat spots to improve ride quality. Also, a wheel force gauge is integrated with the face wheel enclosure.Type: GrantFiled: June 6, 2017Date of Patent: May 1, 2018Inventor: Colin Hodge
-
Publication number: 20170362057Abstract: An elevator roller guide assembly that provides enhanced ride comfort. The assembly includes a chassis, a stop plate mounted to the chassis, a face wheel enclosure that at least partially encloses the face wheel and is connected to a plurality of leaf springs, and a pair of side wheel enclosures connected to the face wheel enclosure by the plurality of leaf springs. The side wheel enclosures each support a side wheel in a fixed relation to the other side wheel. The side wheel enclosures are operably connected to the stop plate by a pair of vertical plates. A multi-axis damper extends from the stop plate to engage the face wheel enclosure and dampen oscillation of the wheel enclosures during operation. A set of delta diameter wheels across all four guides reduces coincident flat spots to improve ride quality. Also, a wheel force gauge is integrated with the face wheel enclosure.Type: ApplicationFiled: June 6, 2017Publication date: December 21, 2017Inventor: Colin HODGE
-
Publication number: 20170358226Abstract: A device includes a unit for defining evaluation criteria relating to the aircraft and to its flight, a unit for predicting an energy status of the aircraft at the end of a given segment of a flight trajectory, a unit for verifying whether at least one event will occur on the given segment, and a unit for identifying at least one action to be performed on given segment and the position where this action must be performed on this segment, the purpose of an action being to generate a change of flight configuration of the aircraft leading to a modification of the energy of said aircraft. The device is configured to form a predicted energy trajectory, from a current position of the aircraft to the end of the flight trajectory, the predicted energy trajectory indicating all identified actions and positions along the flight trajectory where these actions must be performed.Type: ApplicationFiled: June 6, 2017Publication date: December 14, 2017Applicant: Airbus Operations S.A.S.Inventors: Colin Hodges, Charles Renault Leberquer
-
Publication number: 20170351269Abstract: A method for optimizing the take-off parameters of an aircraft. The aircraft comprises a system for automatically controlling the high lift devices at the moment when the wheels of the aircraft leave the ground. The method comprises a step of selecting a first configuration of the high lift devices at the start of the take-off phase and a selection of an acceleration speed of the aircraft. The method is advantageous in that, on reception of an actual aircraft take-off detection signal, a control unit is configured to transmit a control command making it possible to bring the high lift devices into a second configuration, in which they are retracted relative to the first position, and consecutively accelerate the speed of the aircraft automatically to an acceleration speed entered by the pilot.Type: ApplicationFiled: May 31, 2017Publication date: December 7, 2017Inventors: Jean-Pierre Demortier, Eric Petit, Christophe Homehr, Cyrille Thiers, Colin Hodges, Christian Lulla
-
Patent number: 8727349Abstract: The present invention provides lottery tickets each of which incorporates one or more set(s) of random results data generated by random data generating software. Each set of random results data corresponding to possible results of game play, a sports event or a sporting contest, and incorporates a verification code for each set of random results data.Type: GrantFiled: March 5, 2010Date of Patent: May 20, 2014Assignee: Pro-Active Games Pty Ltd.Inventors: Christopher Joseph Colin Hodges, Robert William Holden
-
Publication number: 20110319150Abstract: The present invention provides lottery tickets each of which incorporates one or more set(s) of random results data generated by random data generating software. Each set of random results data corresponding to possible results of game play, a sports event or a sporting contest, and incorporates a verification code for each set of random results data.Type: ApplicationFiled: March 5, 2010Publication date: December 29, 2011Applicant: PRO-ACTIVE GAMES PTY LTDInventor: Christopher Joseph Colin Hodges
-
Publication number: 20070244525Abstract: A phototherapy light device for directing light onto an infant. The phototherapy light device has a base containing an illumination source and a gooseneck type of elongated neck that extends outwardly from the base and has a distal end adapted to be positioned to direct the light onto the infant. An optical fiber transmits the light from the illumination source to the distal end through the optical fiber where the light is passed through a light emanating device located at the distal end of the elongated neck. The elongated neck has two flexible sections, one of which has two coaxial springs to provide flexibility in positioning as well as to impart sufficient strength and rigidity to the elongated neck. The dual spring concept provides a system having reduced stresses while creating a double fault structural system without compromising the flexibility of the elongated neck.Type: ApplicationFiled: April 17, 2006Publication date: October 18, 2007Inventors: Colin Hodge, Michael Mackin
-
Publication number: 20070162091Abstract: A phototherapy light device for directing light onto an infant. The phototherapy light device has a base containing an illumination source and a gooseneck type of elongated member that extends outwardly from the base and has a conical shaped shade at its distal end. An optical fiber transmits the light from the illumination source to the shade through the optical fiber where the light is passed through a plastic Fresnel lens at the distal end of the shade. By the use of the Fresnel lens and the means of affixing the shade onto the elongated member, the distal end of the phototherapy light device is relatively light and which alleviates the problem of that distal end sagging downwardly to contact the infant undergoing treatment.Type: ApplicationFiled: January 6, 2006Publication date: July 12, 2007Inventor: Colin Hodge
-
Publication number: 20050165369Abstract: A protective device that is used in a medical suction system withdrawing liquids from a patient. The device is located upstream of a vacuum regulator and protects that regulator and other downstream components from contacting the liquid being withdrawn from the patient. The protective device has an inlet and an outlet and an actuator mechanism that can move between a contracted position where a gas can communicate through the protective device between the inlet and the outlet and an expanded position where the actuator mechanism occludes both the inlet and the outlet to shut off the vacuum supply to the patient. An electrical circuit having a pair of sensing electrodes provides an electrical discharge to trigger a shape-metal alloy wire to move the actuator mechanism from the contracted position to the expanded position when the sensing electrodes detect the presence of a liquid therebetween.Type: ApplicationFiled: January 23, 2004Publication date: July 28, 2005Inventors: Colin Hodge, Matthew Severns
-
Patent number: 4903726Abstract: A vacuum regulating cartridge (10) having a roller diaphragm (52), a coil spring (54) and a cantilevered spring arm (68) to form a regulation system for regulating vacuum in a medical regulating vacuum controller (26).Type: GrantFiled: August 10, 1987Date of Patent: February 27, 1990Assignees: Aeros Instruments, Inc., The BOC Group, Inc., Ohmeda DivisionInventors: Gordon D. Martin, Douglas D. Carden, Colin Hodge