Patents by Inventor Robert Kyle
Robert Kyle 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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Publication number: 20230047003Abstract: A computerized data transfer system allows data transfers to be initiated over a network between senders and recipients. Individual senders initiate data transfers over the network by selecting a recipient from a list at a sender device. The system includes a data store of sender specific recipients, a data transfer history data store of past transfers; and a master participant data store storing profiles of recipients for which transfers can be initiated. The system includes a computing device that for selected senders, retrieves entries of the data store of sender specific recipients, master participant data store and data transfer history data store; generates a predicted transfer profile for each recipient for the sender, based on past data transfers and the master participant data store to identify deviations therefrom; and updates the data store of sender specific recipients for the selected sender to update entries for recipients associated with identified deviations.Type: ApplicationFiled: November 1, 2022Publication date: February 16, 2023Applicant: The Toronto-Dominion BankInventors: Robert Kyle MILLER, Sonja TORBICA, Helene Nicole ESPOSITO, Harrison Michael James REILLY, Matta WAKIM, Kyryll ODOBETSKIY, Dexter Lamont FICHUK, Adam Douglas McPHEE, Omas ABDULLAH
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Publication number: 20220412179Abstract: Systems and methods presented herein provide for cutting in a borehole or casing. A cutting device can include a first arm having a cutting blade, wherein the cutting blade has side cutting teeth and an axis of rotation that is substantially at a right angle with respect to an axis of the tool body. The cutting device can also include a second arm with a bumper. The first and second arms articulate away from the elongate body in different directions to reduce vibrations while cutting. A control device can automate the cut based on hydraulic pressure measurements. Additionally, the cutting device can also be extended or rotated on a rotary index. The cutting device can rotate around a J slot, in an example.Type: ApplicationFiled: June 27, 2022Publication date: December 29, 2022Inventors: Todor Sheiretov, Joseph Matthew Casassa, Gregory Jay Giem, David Engel, Maxim Alekseevich Klyuzhev, Joshua Wurtz, Albert Dionisio, Robert Kyle Wiesenborn, Philip Stevenson
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Publication number: 20220412180Abstract: Devices, systems and methods for cutting openings in a wellbore tubular by a slot cutting assembly having an anchoring system and a slot cutting tool. The anchoring assembly anchors the slot cutting assembly within the wellbore. The slot cutting tool has an extendable cutting blade that is pushed into the wellbore tubular to cut an opening through the tubular. The slot cutting tool may have an extendable stabilizing arm to stabilize and assist with cutting by the blade. The slot cutting assembly may have azimuth and depth sensors to assist with positioning the tool at a desired position downhole. A surface system may be used to control the position of the slot cutting assembly downhole.Type: ApplicationFiled: June 27, 2022Publication date: December 29, 2022Inventors: Joshua Wurtz, Joseph Matthew Casassa, Christopher Albert Babin, Robert Kyle Wiesenborn, Pierre-Arnaud Foucher, David Engel, Todor Sheiretov
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Patent number: 11536107Abstract: A mechanical service tool that may include one or more anchors, a cutter, a communication and control system, and one or more sensors, as well as methods for operating the mechanical service tool, are provided. The one or more anchors may extend radially from the mechanical service tool and the cutter may move relative to the mechanical service tool. The cutter may include a drilling bit. The communication and control system may obtain remote commands that control the cutter, the one or more anchors, or both. The one or more sensors may detect operational conditions of the mechanical service tool and may be operatively coupled to the communication and control system.Type: GrantFiled: September 21, 2018Date of Patent: December 27, 2022Assignee: SCHLUMBERGER TECHNOLOGY CORPORATIONInventors: Robert Kyle Wiesenborn, Matthew Dresel, Pierre-Olivier Gourmelon, Rex Mennem, Matthew Billingham, Todor Sheiretov, Nathan Landsiedel, Yoann Couble, Wade DuPree
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Patent number: 11521186Abstract: A computerized data transfer system allows data transfers to be initiated over a network between senders and recipients. Individual senders initiate data transfers over the network by selecting a recipient from a list at a sender device. The system includes a data store of sender specific recipients, a data transfer history data store of past transfers; and a master participant data store storing profiles of recipients for which transfers can be initiated. The system includes a computing device that for selected senders, retrieves entries of the data store of sender specific recipients, master participant data store and data transfer history data store; generates a predicted transfer profile for each recipient for the sender, based on past data transfers and the master participant data store to identify deviations therefrom; and updates the data store of sender specific recipients for the selected sender to update entries for recipients associated with identified deviations.Type: GrantFiled: August 21, 2018Date of Patent: December 6, 2022Assignee: The Toronto-Dominion BankInventors: Robert Kyle Miller, Sonja Torbica, Helene Nicole Esposito, Harrison Michael James Reilly, Matta Wakim, Kyryll Odobetskiy, Dexter Lamont Fichuk, Adam Douglas McPhee, Omas Abdullah
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Patent number: 11498663Abstract: A landing gear system includes an axle having an internal cavity and a wheel rotatably coupled to the axle. A drive shaft is mounted within the cavity to be rotatable about an axis. The landing gear system further includes a rod slidably mounted within the drive shaft and a clutch. The clutch has a first portion that is coupled to the rod and rotates with the drive shaft. A second portion of the clutch is fixedly coupled to the wheel. The rod selectively reciprocates along the axis between a first position and a second position to engage and disengage the clutch.Type: GrantFiled: February 18, 2020Date of Patent: November 15, 2022Assignee: SAFRAN LANDING SYSTEMS CANADA INC.Inventors: Robert Kyle Schmidt, Steve Amberg, Jason Brown
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Patent number: 11498664Abstract: A landing gear system includes a wheel rotatably coupled to an axle about an axis. A torque tube is rotatably mounted to the axle about the axis such that the axle extends through a central portion of the torque tube. A rotor is fixed in rotation about the axis relative to the wheel, and a stator is fixed in rotation about the axis relative to the torque tube. The landing gear assembly further includes a clutch assembly selectively reciprocal between an engaged state and a disengaged state. The stator is fixed in rotation about the axis relative to the torque tube when the clutch assembly is in an engaged state. When the clutch assembly is in a disengaged state, the stator is rotatably about the axis relative to the torque tube.Type: GrantFiled: July 10, 2020Date of Patent: November 15, 2022Assignee: SAFRAN LANDING SYSTEMS CANADA INC.Inventor: Robert Kyle Schmidt
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Patent number: 11407502Abstract: A taxi drive system is disclosed that provides motive force to wheels of an aircraft. The motive force is transferred by a motor powered continuous track (e.g., belt, chain, or other flexible transmission element) directly to the wheel(s) of an aircraft. The system is carried by the landing gear of the aircraft, and is placed in engagement with an aircraft wheel with sufficient force to allow for the track to drive the aircraft wheel. The taxi drive system includes a separate motor from the main aircraft engines so that the aircraft may be taxied while the main engines are shutdown or at idle.Type: GrantFiled: February 24, 2020Date of Patent: August 9, 2022Assignee: SAFRAN LANDING SYSTEMS CANADA INC.Inventor: Robert Kyle Schmidt
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Patent number: 11407500Abstract: A landing gear for a vehicle includes a strut configured for reciprocating movement between a stowed position and a deployed position. A shock absorber has a first element slidingly disposed within the strut and a second element slidingly coupled to the first element. A trailing arm is rotatably coupled to the second element. A first linkage is coupled to the first element, wherein the first linkage drives the first element between a raised position when the strut is in the stowed position and a lowered position when the strut is in the deployed position. The landing gear further includes a second linkage coupled to the trailing arm. The second linkage rotates the trailing arm between a first trailing arm position when the strut is in the stowed position and a second trailing arm position when the strut is in the deployed position.Type: GrantFiled: September 15, 2020Date of Patent: August 9, 2022Assignee: SAFRAN LANDING SYSTEMS CANADA, INC.Inventors: Robert Kyle Schmidt, Steve Amberg, Michael Saccoccia
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Publication number: 20220241619Abstract: A breathing system hood assembly that fits over a user's head includes an air impermeable hood having an opening dimensioned to fit over the user's head and an elastically deformable neck seal arranged along at least a portion of the opening. The neck seal includes a region wherein the neck seal is arranged in overlapping relation with itself, whereby the neck seal can expand to fit over a user's head and contract to create a seal with the user's neck.Type: ApplicationFiled: April 30, 2020Publication date: August 4, 2022Inventors: Robert Kyle Fullerton, Silvia Geciova-Borovova Guttmann, Robert D. Williams, Scott M. Purrington, Jhansi R. Arikatla
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Publication number: 20220234726Abstract: Wheel acceleration systems are disclosed that provide a motive force to at least one wheel of an aircraft, in order to accelerate the aircraft to takeoff speed with the assistance of main engine thrust. The wheel acceleration system includes a pyrotechnic unit configured to generate expanding gases by combusting a propellant, and a rotary propulsion unit pneumatically coupled to the pyrotechnic unit. The rotary propulsion unit includes an impeller configured to be driven by the expanding gases and to deliver torque to the wheel.Type: ApplicationFiled: January 27, 2021Publication date: July 28, 2022Applicant: SAFRAN LANDING SYSTEMS CANADA INC.Inventor: Robert Kyle Schmidt
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Publication number: 20220219812Abstract: A landing gear system includes a drive shaft extending through an axle. A wheel with a drive surface is rotatably coupled to the axle. A drive assembly, which has disengaged and engaged states, includes a drive element and an idler element. The drive element, which has an engagement feature, is coupled to the drive shaft for rotation about an axis. The engagement feature has first and second diameters when the drive assembly is in the disengaged and engaged states, respectively. The idler element is frictionally engaged with the engagement feature of the drive element to transfer rotation of the drive element to the wheel when the drive assembly is in the engaged state. The idler element is disengaged from at least one of the engagement feature of drive element and the wheel when the drive assembly is in the disengaged state.Type: ApplicationFiled: January 12, 2021Publication date: July 14, 2022Applicant: Safran Landing Systems Canada Inc.Inventor: Robert Kyle Schmidt
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Publication number: 20220219813Abstract: A landing gear system includes wheel rotatably coupled to an axle. A driveshaft extends through a cavity formed in the axle and is rotatable about an axis. A planetary gear includes a sun gear operably coupled to the drive shaft and a planet gear operably engaging the sun gear. The planetary gear further includes a ring gear that surrounds and is operably coupled to the planet gear so that rotation of the drive shaft rotates the ring gear. A clutch assembly is selectively moveable between an engaged state and a disengaged state. The clutch assembly transfers rotation of the ring gear to the wheel when the clutch assembly is in the engaged state, and the clutch assembly does not transfer rotation of the wheel to the ring gear when the clutch assembly is in the disengaged state.Type: ApplicationFiled: January 12, 2021Publication date: July 14, 2022Applicants: Safran Landing Systems, Safran Landing Systems Canada Inc.Inventors: Robert Kyle Schmidt, Steve Amberg, Didier Brun
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Publication number: 20220221021Abstract: A shock absorber includes a housing and an end wall slidably disposed within the housing. The end wall and the housing cooperate to define at least a portion of a cavity within the housing. The cavity is filled with a fluid, and a piston is slidably disposed within the cavity. Movement of the piston within the cavity compresses the fluid to provide a spring force. The shock absorber further includes a compensator coupled to the end wall. The compensator positions the end wall within the housing to change a volume of the cavity in response to a change in a temperature of a first element of the compensator.Type: ApplicationFiled: January 12, 2021Publication date: July 14, 2022Applicant: Safran Landing Systems Canada Inc.Inventor: Robert Kyle Schmidt
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Patent number: 11378150Abstract: A shock absorber includes a housing and an end wall slidably disposed within the housing. The end wall and the housing cooperate to define at least a portion of a cavity within the housing. The cavity is filled with a fluid, and a piston is slidably disposed within the cavity. Movement of the piston within the cavity compresses the fluid to provide a spring force. The shock absorber further includes a compensator coupled to the end wall. The compensator positions the end wall within the housing to change a volume of the cavity in response to a change in a temperature of a first element of the compensator.Type: GrantFiled: January 12, 2021Date of Patent: July 5, 2022Assignee: SAFRAN LANDING SYSTEMS CANADA INC.Inventor: Robert Kyle Schmidt
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Publication number: 20220127016Abstract: Techniques and methodologies for servicing a shock strut are provided that account for the variability in gas solubility of the shock strut while in-service. These examples incorporates knowledge of the shock strut's stoke history in order to estimate/predict the amount of gas in solution, its percentage saturation, etc. This may permit a more refined knowledge of the true servicing state of the shock strut.Type: ApplicationFiled: October 27, 2020Publication date: April 28, 2022Applicants: SAFRAN LANDING SYSTEMS CANADA INC, SAFRAN LANDING SYSTEMS UK LTDInventors: Robert Kyle Schmidt, Jon Smith
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Publication number: 20220122053Abstract: A server comprises a communications module; a processor coupled with the communications module; and a memory coupled to the processor and storing processor-executable instructions which, when executed by the processor, configure the processor to receive, via the communications module and from a computing device, a signal representing a request to perform an operation from a user; determine that the user does not have a persistent account; and when it is determined that the user does not have a persistent account: obtain, via the communications module and from a digital identity network, a signal including verified identity data of the user; generate a temporary data record and associate the temporary data record with the verified identity data of the user; receive a value transfer based on the requested operation and store the received value in the temporary data record; and perform the operation using the stored value in the temporary data record.Type: ApplicationFiled: October 15, 2020Publication date: April 21, 2022Applicant: The Toronto-Dominion BankInventors: Robert Kyle MILLER, Kevin Wayne FARAGHER, Malcolm Dinyar JUSSAWALLA, Tomasz PAWELKIEWICZ, Karandeep PURI
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Publication number: 20220097868Abstract: A remote towing interface is used to couple a towbar to an aircraft having a fuselage and a steerable landing gear. The remote towing interface includes a towbar coupler mounted to the aircraft and configured to releasably couple a towbar to the aircraft. The remote towing interface further includes a sensor and a controller. The sensor is configured to sense a position of the towbar relative to the aircraft when the towbar is coupled to the towbar coupler, and the controller controls the steerable landing gear according to the sensed position of the towbar relative to the aircraft.Type: ApplicationFiled: September 29, 2020Publication date: March 31, 2022Applicant: Safran Landing Systems Canada Inc.Inventor: Robert Kyle Schmidt
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Publication number: 20220081105Abstract: A landing gear for a vehicle includes a strut configured for reciprocating movement between a stowed position and a deployed position. A shock absorber has a first element slidingly disposed within the strut and a second element slidingly coupled to the first element. A trailing arm is rotatably coupled to the second element. A first linkage is coupled to the first element, wherein the first linkage drives the first element between a raised position when the strut is in the stowed position and a lowered position when the strut is in the deployed position. The landing gear further includes a second linkage coupled to the trailing arm. The second linkage rotates the trailing arm between a first trailing arm position when the strut is in the stowed position and a second trailing arm position when the strut is in the deployed position.Type: ApplicationFiled: September 15, 2020Publication date: March 17, 2022Applicant: Safran Landing Systems Canada Inc.Inventors: Robert Kyle Schmidt, Steve Amberg, Michael Saccoccia
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Publication number: 20220009622Abstract: A landing gear system includes a wheel rotatably coupled to an axle about an axis. A torque tube is rotatably mounted to the axle about the axis such that the axle extends through a central portion of the torque tube. A rotor is fixed in rotation about the axis relative to the wheel, and a stator is fixed in rotation about the axis relative to the torque tube. The landing gear assembly further includes a clutch assembly selectively reciprocal between an engaged state and a disengaged state. The stator is fixed in rotation about the axis relative to the torque tube when the clutch assembly is in an engaged state. When the clutch assembly is in a disengaged state, the stator is rotatably about the axis relative to the torque tube.Type: ApplicationFiled: July 10, 2020Publication date: January 13, 2022Applicant: Safran Landing Systems Canada Inc.Inventor: Robert Kyle Schmidt