Patents by Inventor Jendrick Westphal
Jendrick Westphal 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: 11430344Abstract: An air turbulence analysis system and method includes an air turbulence control unit that is configured to receive a position signal from an aircraft within an air space. The air turbulence control unit determines a location of air turbulence within the air space based on the position signal. In at least one embodiment, the position signal is an automatic dependent surveillance-broadcast (ADS-B) signal.Type: GrantFiled: July 9, 2018Date of Patent: August 30, 2022Assignee: THE BOEING COMPANYInventors: Katie M. Reid, Jendrick Westphal, Karol Rydzewski
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Patent number: 11335205Abstract: An apparatus is provided. The apparatus determines a plurality of runway exits reachable by the aircraft, and applied braking force of the aircraft to land at respective ones of the plurality of runway exits and predicts taxi-in times of the aircraft to land at respective ones of the plurality of runway exits. The apparatus also predicts maintenance costs of the aircraft to land at respective ones of the plurality of runway exits based on the applied braking force and predicts overall costs of the aircraft to land at respective ones of the plurality of runway exits based on the taxi-in times and the maintenance costs. The apparatus further determines the runway exit among the plurality of runway exits, the runway exit having a minimal overall cost among the overall costs and presents a recommendation of the runway exit for landing the aircraft to a user.Type: GrantFiled: August 7, 2019Date of Patent: May 17, 2022Assignee: The Boeing CompanyInventors: Marco Gaertner, Jendrick Westphal
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Publication number: 20210043097Abstract: An apparatus is provided. The apparatus determines a plurality of runway exits reachable by the aircraft, and applied braking force of the aircraft to land at respective ones of the plurality of runway exits and predicts taxi-in times of the aircraft to land at respective ones of the plurality of runway exits. The apparatus also predicts maintenance costs of the aircraft to land at respective ones of the plurality of runway exits based on the applied braking force and predicts overall costs of the aircraft to land at respective ones of the plurality of runway exits based on the taxi-in times and the maintenance costs. The apparatus further determines the runway exit among the plurality of runway exits, the runway exit having a minimal overall cost among the overall costs and presents a recommendation of the runway exit for landing the aircraft to a user.Type: ApplicationFiled: August 7, 2019Publication date: February 11, 2021Inventors: Marco Gaertner, Jendrick Westphal
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Patent number: 10831198Abstract: Embodiments are disclosed for a machine and process that include a computer code specially programmed for creating a runway extension speed for an aircraft taking off. The process may include sensing current location, current acceleration, and current speed, for the aircraft during takeoff roll; receiving, in a ROTTOWIRE, the current speed and the current acceleration for the aircraft; creating in the ROTTOWIRE an actual speed profile; creating, using a specially coded program in the ROTTOWIRE and the current acceleration, the runway extension speed via determining, for a current location of the aircraft, a distance from a departure end of the runway and a terminating distance required to terminate the takeoff to a stop of the aircraft on the runway, a distance until the aircraft reaches a designated height; and when the terminating distance equals the distance from the departure end of the runway; and presenting the runway extension speed.Type: GrantFiled: August 18, 2017Date of Patent: November 10, 2020Assignee: The Boeing CompanyInventors: Jendrick Westphal, Jonas Schulze
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Publication number: 20200013300Abstract: An air turbulence analysis system and method includes an air turbulence control unit that is configured to receive a position signal from an aircraft within an air space. The air turbulence control unit determines a location of air turbulence within the air space based on the position signal. In at least one embodiment, the position signal is an automatic dependent surveillance-broadcast (ADS-B) signal.Type: ApplicationFiled: July 9, 2018Publication date: January 9, 2020Applicant: THE BOEING COMPANYInventors: Katie M. Reid, Jendrick Westphal, Karol Rydzewski
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Publication number: 20190056740Abstract: Embodiments are disclosed for a machine and process that include a computer code specially programmed for creating a runway extension speed for an aircraft taking off. The process may include sensing current location, current acceleration, and current speed, for the aircraft during takeoff roll; receiving, in a ROTTOWIRE, the current speed and the current acceleration for the aircraft; creating in the ROTTOWIRE an actual speed profile; creating, using a specially coded program in the ROTTOWIRE and the current acceleration, the runway extension speed via determining, for a current location of the aircraft, a distance from a departure end of the runway and a terminating distance required to terminate the takeoff to a stop of the aircraft on the runway, a distance until the aircraft reaches a designated height; and when the terminating distance equals the distance from the departure end of the runway; and presenting the runway extension speed.Type: ApplicationFiled: August 18, 2017Publication date: February 21, 2019Inventors: Jendrick Westphal, Jonas Schulze
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Patent number: 9643737Abstract: Method, apparatus, and computer program product for providing a cause of a scent and/or sound detected during operation of a vehicle are provided. In the event a vehicle operator hears a sound or smells a scent while operating a vehicle, a microphone can sample the sound and/or an electronic nose can sample the scent. A sound and/or scent profile is generated from the sampled sound and/or sampled scent. The generated sound and/or scent profile are compared to known sound and/or scent profiles stored in a data structure. In the event the generated sound and/or scent profile matches a known sound and/or scent profile, the data structure is checked for correspondences between the matched, known sound and/or scent profile and a cause of the sound and/or scent. In the event a correspondence to a cause exists, then the cause is output to a user to identify the cause of the sound and/or scent.Type: GrantFiled: August 19, 2015Date of Patent: May 9, 2017Assignee: THE BOEING COMPANYInventors: Nima Barraci, Jendrick Westphal, Niels-Holger Stark, Merian Kindermann
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Publication number: 20170050750Abstract: Method, apparatus, and computer program product for providing a cause of a scent and/or sound detected during operation of a vehicle are provided. In the event a vehicle operator hears a sound or smells a scent while operating a vehicle, a microphone can sample the sound and/or an electronic nose can sample the scent. A sound and/or scent profile is generated from the sampled sound and/or sampled scent. The generated sound and/or scent profile are compared to known sound and/or scent profiles stored in a data structure. In the event the generated sound and/or scent profile matches a known sound and/or scent profile, the data structure is checked for correspondences between the matched, known sound and/or scent profile and a cause of the sound and/or scent. In the event a correspondence to a cause exists, then the cause is output to a user to identify the cause of the sound and/or scent.Type: ApplicationFiled: August 19, 2015Publication date: February 23, 2017Inventors: Nima BARRACI, Jendrick WESTPHAL, Niels-Holger STARK, Merian KINDERMANN
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Patent number: 8290639Abstract: A method and apparatus for managing a number of control surfaces for an aircraft. A current configuration for the number of control surfaces for the aircraft is identified during flight of the aircraft. A selected point in time at which the current configuration for the number of control surfaces is to be changed to a new configuration for the number of control surfaces is identified. A portion of time relative to the selected point in time during which the current configuration for the number of control surfaces is to be changed to the new configuration is identified based on a difference between a current amount of energy for the aircraft and an expected amount of energy for the aircraft.Type: GrantFiled: November 4, 2010Date of Patent: October 16, 2012Assignee: The Boeing CompanyInventors: Jendrick Westphal, Nico Zimmer
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Publication number: 20120116611Abstract: A method and apparatus for managing a number of control surfaces for an aircraft. A current configuration for the number of control surfaces for the aircraft is identified during flight of the aircraft. A selected point in time at which the current configuration for the number of control surfaces is to be changed to a new configuration for the number of control surfaces is identified. A portion of time relative to the selected point in time during which the current configuration for the number of control surfaces is to be changed to the new configuration is identified based on a difference between a current amount of energy for the aircraft and an expected amount of energy for the aircraft.Type: ApplicationFiled: November 4, 2010Publication date: May 10, 2012Applicant: THE BOEING COMPANYInventors: Jendrick Westphal, Nico Zimmer