Patents by Inventor Brian J. Burkes
Brian J. Burkes 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: 10920591Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The bore includes a fore surface including a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and having a substantially linear portion and a fore base transition portion radially inward of the fore ramp portion. The bore also includes an aft surface including an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and having a substantially linear portion and an aft base transition portion radially inward of the aft ramp portion.Type: GrantFiled: October 3, 2019Date of Patent: February 16, 2021Assignee: Raytheon Technologies CorporationInventors: Jeffrey Leon, William Indoe, Kimberly Caruso, Brian J. Burke, Fabian D. Betancourt, Kurt Leach
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Patent number: 10787921Abstract: A cover plate for a rotor assembly is disclosed. In various embodiments, the cover plate includes an annular member having a radially inner portion and a radially outer portion with respect to a longitudinal axis, the radially inner portion including an aft face and an angled forward face, the angled forward face defining a forward face angle with respect to a cylindrical plane that is coaxial with the longitudinal axis, the face angle having a value that is greater than or equal to fifty degrees; a first tab and a second tab disposed proximate the radially inner portion of the annular member; and a slot disposed between the first tab and the second tab.Type: GrantFiled: September 13, 2018Date of Patent: September 29, 2020Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Derek A Brigham, Jeffrey Leon, David Dwyer Whittle, Amarnath Ramlogan, Brian J Burke, Santiago Orellana, Tania Bhatia Kashyap, Dianbo Li
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Patent number: 10724374Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore disposed about the central axis, a rim and a web disposed radially between the bore and the rim. The bore has a fore surface and an aft surface. The aft surface of the bore may include an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and an aft base transition portion radially inward of the aft ramp portion. The fore surface of the bore may include a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and a fore base transition portion radially inward of the fore ramp portion. The aft ramp portion includes a substantially linear portion and the fore ramp portion includes a substantially linear portion.Type: GrantFiled: September 1, 2017Date of Patent: July 28, 2020Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, William Indoe, Kimberly Caruso, Brian J. Burke, Fabian D. Betancourt, Kurt Leach
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Publication number: 20200149398Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The bore includes a fore surface including a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and having a substantially linear portion and a fore base transition portion radially inward of the fore ramp portion. The bore also includes an aft surface including an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and having a substantially linear portion and an aft base transition portion radially inward of the aft ramp portion.Type: ApplicationFiled: October 3, 2019Publication date: May 14, 2020Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, WILLIAM INDOE, KIMBERLY CARUSO, BRIAN J. BURKE, FABIAN D. BETANCOURT, KURT LEACH
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Patent number: 10641110Abstract: A turbine rotor disk for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a number of blade posts, tabs and slots circumferentially disposed about a rim portion of the disk. The tabs each include a blade post transition portion, a slope portion radially inward of the blade transition portion and a face portion radially inward of the slope portion. The blade posts, tabs and slots are circumferentially oriented about the rim portion such that a tab or slot is positioned radially inward of each blade post.Type: GrantFiled: September 1, 2017Date of Patent: May 5, 2020Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, William Indoe, Brian J. Burke, Kimberly Caruso, Santiago Orellana, Kurt Leach, Fabian D. Betancourt
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Publication number: 20200088052Abstract: A cover plate for a rotor assembly is disclosed. In various embodiments, the cover plate includes an annular member having a radially inner portion and a radially outer portion with respect to a longitudinal axis, the radially inner portion including an aft face and an angled forward face, the angled forward face defining a forward face angle with respect to a cylindrical plane that is coaxial with the longitudinal axis, the face angle having a value that is greater than or equal to fifty degrees; a first tab and a second tab disposed proximate the radially inner portion of the annular member; and a slot disposed between the first tab and the second tab.Type: ApplicationFiled: September 13, 2018Publication date: March 19, 2020Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: Derek A Brigham, Jeffrey Leon, David Dwyer Whittle, Amarnath Ramlogan, Brian J Burke, Santiago Orellana, Tania Bhatia Kashyap, Dianbo Li
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Patent number: 10550702Abstract: A turbine rotor disk for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The rim includes a first radially outermost rim portion and a second radially outermost rim portion disposed radially inward of the first radially outermost rim portion. First and second blade posts are disposed proximate the first radially outermost rim portion and spaced circumferentially. First and second tabs are disposed proximate the second radially outermost rim portion and positioned radially inward of the first and second blade posts. A slot is disposed circumferentially between the first tab and the second tab. The first tab and the second tab have an axial profile that includes a blade post transition portion, a slope portion radially inward of the blade transition portion and a face portion radially inward of the slope portion.Type: GrantFiled: September 1, 2017Date of Patent: February 4, 2020Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, William Indoe, Kimberly Caruso, Brian J. Burke, Kurt Leach, Fabian D. Betancourt
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Patent number: 10544677Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes an annular bore portion, an annular rim portion and an annular web portion disposed radially between the bore portion and the rim portion. The annular web portion includes an aft surface. A cylindrical arm is disposed on the aft surface and has a first portion extending axially from the aft surface and a second portion extending radially outward from a distal end of the first portion. The intersection of the first portion and the aft surface defines a fillet, radially inward of the first portion. The fillet is defined by a compound radius.Type: GrantFiled: September 1, 2017Date of Patent: January 28, 2020Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, William Indoe, Kimberly Caruso, Kurt Leach, Fabian D. Betancourt, Brian J. Burke
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Patent number: 10472968Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The bore includes a fore surface including a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and having a substantially linear portion and a fore base transition portion radially inward of the fore ramp portion. The bore also includes an aft surface including an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and having a substantially linear portion and an aft base transition portion radially inward of the aft ramp portion.Type: GrantFiled: September 1, 2017Date of Patent: November 12, 2019Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Jeffrey Leon, William Indoe, Kimberly Caruso, Brian J. Burke, Fabian D. Betancourt, Kurt Leach
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Publication number: 20190071970Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore disposed about the central axis, a rim and a web disposed radially between the bore and the rim. The bore has a fore surface and an aft surface. The aft surface of the bore may include an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and an aft base transition portion radially inward of the aft ramp portion. The fore surface of the bore may include a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and a fore base transition portion radially inward of the fore ramp portion. The aft ramp portion includes a substantially linear portion and the fore ramp portion includes a substantially linear portion.Type: ApplicationFiled: September 1, 2017Publication date: March 7, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: JEFFREY LEON, WILLIAM INDOE, KIMBERLY CARUSO, BRIAN J. BURKE, FABIAN D. BETANCOURT, KURT LEACH
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Publication number: 20190071972Abstract: A turbine rotor disk for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The rim includes a first radially outermost rim portion and a second radially outermost rim portion disposed radially inward of the first radially outermost rim portion. First and second blade posts are disposed proximate the first radially outermost rim portion and spaced circumferentially. First and second tabs are disposed proximate the second radially outermost rim portion and positioned radially inward of the first and second blade posts. A slot is disposed circumferentially between the first tab and the second tab. The first tab and the second tab have an axial profile that includes a blade post transition portion, a slope portion radially inward of the blade transition portion and a face portion radially inward of the slope portion.Type: ApplicationFiled: September 1, 2017Publication date: March 7, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: JEFFREY LEON, WILLIAM INDOE, KIMBERLY CARUSO, BRIAN J. BURKE, KURT LEACH, FABIAN D. BETANCOURT
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Publication number: 20190071969Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes an annular bore portion, an annular rim portion and an annular web portion disposed radially between the bore portion and the rim portion. The annular web portion includes an aft surface. A cylindrical arm is disposed on the aft surface and has a first portion extending axially from the aft surface and a second portion extending radially outward from a distal end of the first portion. The intersection of the first portion and the aft surface defines a fillet, radially inward of the first portion. The fillet is defined by a compound radius.Type: ApplicationFiled: September 1, 2017Publication date: March 7, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: JEFFREY LEON, WILLIAM INDOE, KIMBERLY CARUSO, KURT LEACH, FABIAN D. BETANCOURT, BRIAN J. BURKE
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Publication number: 20190071984Abstract: A turbine rotor disk for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a number of blade posts, tabs and slots circumferentially disposed about a rim portion of the disk. The tabs each include a blade post transition portion, a slope portion radially inward of the blade transition portion and a face portion radially inward of the slope portion. The blade posts, tabs and slots are circumferentially oriented about the rim portion such that a tab or slot is positioned radially inward of each blade post.Type: ApplicationFiled: September 1, 2017Publication date: March 7, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: JEFFREY LEON, WILLIAM INDOE, BRIAN J. BURKE, KIMBERLY CARUSO, SANTIAGO ORELLANA, KURT LEACH, FABIAN D. BETANCOURT
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Publication number: 20190071971Abstract: A turbine rotor for a gas turbine engine includes a disk rotationally disposed about a central axis. The disk includes a bore, a rim and a web disposed radially between the bore and the rim. The bore includes a fore surface including a fore web transition portion, a fore ramp portion radially inward of the fore web transition portion and having a substantially linear portion and a fore base transition portion radially inward of the fore ramp portion. The bore also includes an aft surface including an aft web transition portion, an aft ramp portion radially inward of the aft web transition portion and having a substantially linear portion and an aft base transition portion radially inward of the aft ramp portion.Type: ApplicationFiled: September 1, 2017Publication date: March 7, 2019Applicant: UNITED TECHNOLOGIES CORPORATIONInventors: JEFFREY LEON, WILLIAM INDOE, KIMBERLY CARUSO, BRIAN J. BURKE, FABIAN D. BETANCOURT, KURT LEACH
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Publication number: 20130291860Abstract: The present invention is directed to a method for treating cystic fibrosis. The method comprises the steps of: identifying a patient suffering from cystic fibrosis, applying about 0.8-3 mL of a solution comprising about 18-65 mg/mL of denufosol into a medication reservoir of an nebulizer to achieve a target loading dose of denufosol of about 25-52 mg denufosol per dosing regimen, nebulizing the solution by passing through holes of an vibrating mesh device equipped with an oscillating membrane in the nebulizer, and delivering an inhaled respiratory dose of 20-33 mg to the lungs of the patient by inhalation within 3-9 minutes.Type: ApplicationFiled: October 6, 2011Publication date: November 7, 2013Inventors: Ramesh Krishnamoorthy, Carole Evans, Brian J. Burke, Amy E. Schaberg, Thomas G. Coady
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Patent number: 6971486Abstract: A disc brake assembly for a motor vehicle includes a rotor, a bracket, a pair of brake pads slidably supported by the bracket for movement along a reference axis, and a caliper, also slidably supported by the bracket for movement along the reference axis, bridging the rotor periphery and operative to urge each brake pad into engagement with a respective friction surface of the rotor. A spring clip on the caliper includes a first pair of arms, each resiliently engaging a respective radially-disposed surface on the bracket to thereby releasably secure the spring clip to the caliper. The spring clip also includes a second pair of arms, each resiliently engaging a respective axially-disposed surface on the bracket to urge the outboard portion of the caliper along the reference axis away from the outboard friction surface of the rotor.Type: GrantFiled: March 4, 2004Date of Patent: December 6, 2005Assignee: Continental Teves, Inc.Inventors: Scott M. Stickney, Brian J. Burke, Dirk F. Remde, Stefan M. Wirth
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Patent number: D1014792Type: GrantFiled: September 7, 2021Date of Patent: February 13, 2024Assignee: VKR HOLDING A/SInventors: Brian J. Burkes, James Eric Brinton, Steve Roy Kastner, Shaynus Dawn Spoone, Michael James Waters
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Patent number: D1033678Type: GrantFiled: September 7, 2021Date of Patent: July 2, 2024Inventors: Brian J Burkes, James Eric Brinton, Steve Roy Kastner, Shayndus Dawn Spoone, Michael James Waters