Patents by Inventor Shayan Ahmadian
Shayan Ahmadian 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: 11346239Abstract: A method of measuring a gas turbine engine component of a gas turbine engine according to an example of the present disclosure includes, among other things, providing at least one gas turbine engine component including a coating on a substrate, detecting infrared radiation emitted from at least one localized region of the coating at a first wavelength in a first electromagnetic radiation frequency range, detecting infrared radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength in a second electromagnetic radiation frequency range that differs from the first electromagnetic radiation frequency range, and determining a heat flux relating to the at least one localized region based upon a comparison of the first wavelength and the second wavelength.Type: GrantFiled: September 18, 2020Date of Patent: May 31, 2022Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Shayan Ahmadian, Charles W. Haldeman, Mark F. Zelesky, Christopher T. Bergman, Sebastian Martinez
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Publication number: 20210301676Abstract: A method of measuring a gas turbine engine component of a gas turbine engine according to an example of the present disclosure includes, among other things, providing at least one gas turbine engine component including a coating on a substrate, detecting infrared radiation emitted from at least one localized region of the coating at a first wavelength in a first electromagnetic radiation frequency range, detecting infrared radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength in a second electromagnetic radiation frequency range that differs from the first electromagnetic radiation frequency range, and determining a heat flux relating to the at least one localized region based upon a comparison of the first wavelength and the second wavelength.Type: ApplicationFiled: September 18, 2020Publication date: September 30, 2021Inventors: Shayan Ahmadian, Charles W. Haldeman, Mark F. Zelesky, Christopher T. Bergman, Sebastian Martinez
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Patent number: 10995402Abstract: A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.Type: GrantFiled: May 27, 2020Date of Patent: May 4, 2021Assignee: Raytheon Technologies CorporationInventors: Shayan Ahmadian, Hoyt Y. Chang
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Patent number: 10823417Abstract: A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.Type: GrantFiled: September 19, 2017Date of Patent: November 3, 2020Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Carey Clum, Shayan Ahmadian, Christopher W. Robak
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Patent number: 10815817Abstract: A turbine section according to an example of the present disclosure includes, among other things, a component including a coating on a substrate, and at least one sensor positioned a distance from the component, the at least one sensor configured to detect radiation emitted from at least one localized region of the coating at a first wavelength and configured to detect radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength. The first wavelength and the second wavelength are utilized to determine a heat flux relating to the at least one localized region. A method of measuring a gas turbine engine component is also disclosed.Type: GrantFiled: January 21, 2016Date of Patent: October 27, 2020Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Shayan Ahmadian, Charles W. Haldeman, Mark F. Zelesky, Christopher T. Bergman, Sebastian Martinez
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Publication number: 20200318231Abstract: A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.Type: ApplicationFiled: May 27, 2020Publication date: October 8, 2020Applicant: Raytheon Technologies CorporationInventors: Shayan Ahmadian, Hoyt Y. Chang
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Patent number: 10450960Abstract: A tangential on-board injector (TOBI) for a gas turbine engine is provided. The TOBI includes a body having an entrance and an exit, the body having an outer curved wall and defining an air passageway between the entrance and the exit and a purge cavity configured on an exterior surface of the body with a purge cavity entry fluidly connecting the air passageway to the purge cavity. The purge cavity is configured such that particles in an airflow through the passageway will enter the purge cavity.Type: GrantFiled: September 21, 2015Date of Patent: October 22, 2019Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Mark F. Zelesky, Joel H. Wagner, Shayan Ahmadian
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Publication number: 20190086084Abstract: A combustor may include a combustor shell, a particle collection panel, and a combustor panel. The combustor shell may define a plurality of first impingement holes, the particle collection panel may include a plurality of particle collection chambers and may define a plurality of second impingement holes, and the combustor panel may define a plurality of effusion holes. The particle collection panel may be disposed inward of the combustor shell and the combustor panel may be disposed inward of the particle collection panel. Each particle collection chamber may have a closed inward end and an opening defined in an outward end. The particle collection chambers may be configured to entrap particulates.Type: ApplicationFiled: September 19, 2017Publication date: March 21, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: Carey Clum, Shayan Ahmadian, Christopher W. Robak
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Patent number: 10202903Abstract: A particle separator for removing particles in a flow of air is provided. The particle separator having: a conduit for directing air towards a curved section of the conduit; and a drum in fluid communication with the conduit proximate to the curved section of the conduit, wherein particles in the air travelling towards the curved section will contact a surface of the drum.Type: GrantFiled: September 22, 2015Date of Patent: February 12, 2019Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Shayan Ahmadian, Steven Bruce Gautschi, Mark F. Zelesky
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Publication number: 20190033138Abstract: A plasma spray system including a temperature sensor operable to determine a temperature of the workpiece at a measurement zone; a heater operable to selectively heat the workpiece at a heating zone downstream of the measurement zone; a plasma spray subsystem operable to plasma spray a workpiece, the plasma spray defines an application zone on the workpiece downstream of the heating zone and a control in communication with the plasma spray subsystem, the temperature sensor, and the heater, the control operable to control the heater to heat the workpiece in the heating zone to a desired temperature in response to a temperature determined by the temperature sensor.Type: ApplicationFiled: July 28, 2017Publication date: January 31, 2019Applicant: United Technologies CorporationInventors: Shayan Ahmadian, Kevin W. Schlichting
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Patent number: 10012147Abstract: An engine and particle decelerator is provided herein. The engine having: an inlet opening for directing air towards a compressor of the engine; and a particle decelerator located between the inlet opening and the compressor such that air travelling towards the compressor from the inlet opening must travel through the particle decelerator and wherein an area of the particle decelerator is greater than an inlet and an outlet of the particle decelerator.Type: GrantFiled: August 17, 2015Date of Patent: July 3, 2018Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Hoyt Y. Chang, Shayan Ahmadian
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Patent number: 9983147Abstract: A system and method for prognostic health monitoring of thermal barrier coatings is provided. The system may comprise monitoring a thermal barrier coated gas turbine engine component, and measuring the infrared radiation emitting from the component. The measured thermal radiation data may be analyzed and compared to known material thermal radiation data in order to determine the health of the thermal barrier coating. The compiled comparison results may be compared against a historical statistical study to then determine the overall health of the thermal barrier coating. The system may comprise generating a health monitoring alert in response to the health of the thermal barrier coating indicating an imminent failure.Type: GrantFiled: March 1, 2016Date of Patent: May 29, 2018Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Shayan Ahmadian, Thomas J. Martin, Alexander Staroselsky, Charles W. Haldeman
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Publication number: 20170254761Abstract: A system and method for prognostic health monitoring of thermal barrier coatings is provided. The system may comprise monitoring a thermal barrier coated gas turbine engine component, and measuring the infrared radiation emitting from the component. The measured thermal radiation data may be analyzed and compared to known material thermal radiation data in order to determine the health of the thermal barrier coating. The compiled comparison results may be compared against a historical statistical study to then determine the overall health of the thermal barrier coating. The system may comprise generating a health monitoring alert in response to the health of the thermal barrier coating indicating an imminent failure.Type: ApplicationFiled: March 1, 2016Publication date: September 7, 2017Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: Shayan Ahmadian, Thomas J. Martin, Alexander Staroselsky, Charles W. Haldeman
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Publication number: 20170218505Abstract: A coating system including a reflective cool down chamber with at least one arcuate wall; and an infrared lamp directed at the arcuate wall.Type: ApplicationFiled: February 3, 2016Publication date: August 3, 2017Inventors: Shayan Ahmadian, Hoyt Y. Chang
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Publication number: 20170211408Abstract: A turbine section according to an example of the present disclosure includes, among other things, a component including a coating on a substrate, and at least one sensor positioned a distance from the component, the at least one sensor configured to detect radiation emitted from at least one localized region of the coating at a first wavelength and configured to detect radiation emitted from the substrate corresponding to the at least one localized region at a second, different wavelength. The first wavelength and the second wavelength are utilized to determine a heat flux relating to the at least one localized region. A method of measuring a gas turbine engine component is also disclosed.Type: ApplicationFiled: January 21, 2016Publication date: July 27, 2017Inventors: Shayan Ahmadian, Charles W. Haldeman, Mark F. Zelesky, Christopher T. Bergman, Sebastian Martinez
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Publication number: 20170082027Abstract: A tangential on-board injector (TOBI) for a gas turbine engine is provided. The TOBI includes a body having an entrance and an exit, the body having an outer curved wall and defining an air passageway between the entrance and the exit and a purge cavity configured on an exterior surface of the body with a purge cavity entry fluidly connecting the air passageway to the purge cavity. The purge cavity is configured such that particles in an airflow through the passageway will enter the purge cavity.Type: ApplicationFiled: September 21, 2015Publication date: March 23, 2017Inventors: Mark F. Zelesky, Joel H. Wagner, Shayan Ahmadian
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Publication number: 20170082025Abstract: A particle separator for removing particles in a flow of air is provided. The particle separator having: a conduit for directing air towards a curved section of the conduit; and a drum in fluid communication with the conduit proximate to the curved section of the conduit, wherein particles in the air travelling towards the curved section will contact a surface of the drum.Type: ApplicationFiled: September 22, 2015Publication date: March 23, 2017Inventors: Shayan Ahmadian, Steven Bruce Gautschi, Mark F. Zelesky
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Publication number: 20170051669Abstract: An engine and particle decelerator is provided herein. The engine having: an inlet opening for directing air towards a compressor of the engine; and a particle decelerator located between the inlet opening and the compressor such that air travelling towards the compressor from the inlet opening must travel through the particle decelerator and wherein an area of the particle decelerator is greater than an inlet and an outlet of the particle decelerator.Type: ApplicationFiled: August 17, 2015Publication date: February 23, 2017Inventors: Hoyt Y. Chang, Shayan Ahmadian