Patents by Inventor James H. Mabe
James H. Mabe 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: 11225339Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.Type: GrantFiled: June 26, 2020Date of Patent: January 18, 2022Assignee: THE BOEING COMPANYInventors: Eric S. Mindock, James H. Mabe, Frederick Theodore Calkins, Abraham Naroll Gissen, Miguel A. Estevez
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Publication number: 20200331639Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.Type: ApplicationFiled: June 26, 2020Publication date: October 22, 2020Inventors: Eric S. Mindock, James H. Mabe, Frederick Theodore Calkins, Abraham NaroII Gissen, Miguel A. Estevez
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Patent number: 10730645Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.Type: GrantFiled: April 21, 2017Date of Patent: August 4, 2020Assignee: THE BOEING COMPANYInventors: Eric S. Mindock, James H. Mabe, Frederick Theodore Calkins, Abraham Naroll Gissen, Miguel A. Estevez
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Publication number: 20180305043Abstract: An apparatus includes a thermally conductive interface assembly including a first component associated with a first interface surface and a second component associated with a second interface surface. The apparatus also includes a shape memory alloy component coupled to the thermally conductive interface assembly and configured to move one or more components of the thermally conductive interface assembly between a first state and a second state based on a temperature of the shape memory alloy component. In the first state, the first interface surface is in physical contact with the second interface surface, and in the second state, a gap is defined between the first interface surface and the second interface surface.Type: ApplicationFiled: April 21, 2017Publication date: October 25, 2018Inventors: Eric S. Mindock, James H. Mabe, Frederick Theodore Calkins, Abraham NaroII Gissen, Miguel A. Estevez
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Patent number: 10053239Abstract: In one or more aspects of the present disclosure, an aerospace vehicle includes a frame, an actuable multifunctional cellular structure connected to the frame, the actuable multifunctional cellular structure including a first face member and a second face member, and a shape memory alloy core coupled to the first face member and the second face member, and wherein, at least one of the first face member and the second face member is a graded thermal structure configured so that heat transferred through the graded thermal structure in a predetermined thermal pattern to the shape memory alloy core effects a predetermined change in a shape of the shape memory alloy core and effects a change in shape of the actuable multifunctional cellular structure.Type: GrantFiled: September 9, 2015Date of Patent: August 21, 2018Assignee: The Boeing CompanyInventors: James H. Mabe, Ali Yousefiani
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Patent number: 10054047Abstract: A thermal energy harvesting system employs a hot flow conduit and a cold flow conduit with a flow routing device interruptibly interconnecting the hot flow conduit and cold flow conduit with a flow casing. At least one shape memory actuator (SMA) tube is in fluid contact with the flow casing and fixed at a first end. The flow routing device sequentially supplies hot flow from the hot flow conduit and cold flow from the cold flow conduit inducing rotation of the at least one SMA tube at a second end. A generator or alternator is operably connected to the second end of the at least one SMA tube.Type: GrantFiled: August 10, 2016Date of Patent: August 21, 2018Assignee: The Boeing CompanyInventors: James H. Mabe, Naveed M. Hussain, Edward A. Whalen, Frederick T. Calkins
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Patent number: 10029781Abstract: Shape memory alloy-actuated propeller blades and shape memory alloy-actuated propeller assemblies are disclosed. An example propeller blade includes a propeller body, a plate coupled to the propeller body, a torque transfer member, and a shape memory alloy (SMA) actuator. The torque transfer member has a distal end attached to the plate such that the torque transfer member applies to the plate at least a portion of a torque applied to the torque transfer member at a proximal end of the torque transfer member. The SMA actuator has a distal end and a proximal end. The distal end of the SMA actuator is attached to the torque transfer member. The proximal end of the SMA actuator is coupled to the propeller body such that the distal end is mated to the propeller body. The SMA actuator is configured to apply the torque to the proximal end of the torque transfer member in response to an application of heat to the SMA actuator.Type: GrantFiled: August 3, 2015Date of Patent: July 24, 2018Assignee: The Boeing CompanyInventors: William J. Bigbee-Hansen, Dan J. Clingman, James H. Mabe
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Publication number: 20180094622Abstract: A shape memory alloy (SMA) actuated aerostructure operable to dynamically change shape according to flight conditions is disclosed. Deformable structures are actuated by SMA actuators that are coupled to face sheets of the deformable structures. Actuating the SMA actuators produces complex shape changes of the deformable structures by activating shape changes of the SMA actuators. The SMA actuators are actuated via an active or passive temperature change based on operating conditions. The SMA actuated aerostructure can be used for morphable nozzles such as a variable area fan nozzle and/or a variable geometry chevron of a jet engine to reduce engine noise during takeoff without degrading fuel burn during cruise.Type: ApplicationFiled: April 3, 2013Publication date: April 5, 2018Inventors: Richard D. Widdle, JR., Matthew T. Grimshaw, Kava S. CROSSON-ELTURAN, James H. Mabe, Frederick T. Calkins, Lynn M. Gravatt, Moushumi Shome
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Patent number: 9885345Abstract: A scalable multi-element shape memory alloy (SMA) rotary motor employs a plurality of SMA tubes. A ratcheting gear transmission couples the plurality of SMA tubes in parallel to a common output. A controller provides power to a plurality of heaters associated with each of the plurality of SMA tubes, sequentially heating selected heaters to provide continuous rotational motion of the common output.Type: GrantFiled: December 10, 2014Date of Patent: February 6, 2018Assignee: The Boeing CompanyInventors: Frederick T. Calkins, James H. Mabe, Jonathan K. Brown
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Patent number: 9638176Abstract: In one embodiment, the disclosed vortex generator may include a flap, a bearing configured to be mounted on a surface, an axle retained in the bearing, the flap attached to the axle such that the flap rotates relative to the bearing about the axle, and an actuator made of a shape memory alloy attached to the flap and to a support, the actuator shaped to receive the axle therethrough, such that a change in temperature of the actuator causes the actuator to rotate the flap relative to the bearing.Type: GrantFiled: May 10, 2013Date of Patent: May 2, 2017Assignee: The Boeing CompanyInventors: Belur N. Shivashankara, James H. Mabe, Dan J. Clingman
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Publication number: 20170066519Abstract: In one or more aspects of the present disclosure, an aerospace vehicle includes a frame, an actuable multifunctional cellular structure connected to the frame, the actuable multifunctional cellular structure including a first face member and a second face member, and a shape memory alloy core coupled to the first face member and the second face member, and wherein, at least one of the first face member and the second face member is a graded thermal structure configured so that heat transferred through the graded thermal structure in a predetermined thermal pattern to the shape memory alloy core effects a predetermined change in a shape of the shape memory alloy core and effects a change in shape of the actuable multifunctional cellular structure.Type: ApplicationFiled: September 9, 2015Publication date: March 9, 2017Inventors: James H. Mabe, Ali Yousefiani
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Publication number: 20170036752Abstract: Shape memory alloy-actuated propeller blades and shape memory alloy-actuated propeller assemblies are disclosed. An example propeller blade includes a propeller body, a plate coupled to the propeller body, a torque transfer member, and a shape memory alloy (SMA) actuator. The torque transfer member has a distal end attached to the plate such that the torque transfer member applies to the plate at least a portion of a torque applied to the torque transfer member at a proximal end of the torque transfer member. The SMA actuator has a distal end and a proximal end. The distal end of the SMA actuator is attached to the torque transfer member. The proximal end of the SMA actuator is coupled to the propeller body such that the distal end is mated to the propeller body. The SMA actuator is configured to apply the torque to the proximal end of the torque transfer member in response to an application of heat to the SMA actuator.Type: ApplicationFiled: August 3, 2015Publication date: February 9, 2017Inventors: William J. Bigbee-Hansen, Dan J. Clingman, James H. Mabe
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Publication number: 20160348580Abstract: A thermal energy harvesting system employs a hot flow conduit and a cold flow conduit with a flow routing device interruptibly interconnecting the hot flow conduit and cold flow conduit with a flow casing. At least one shape memory actuator (SMA) tube is in fluid contact with the flow casing and fixed at a first end. The flow routing device sequentially supplies hot flow from the hot flow conduit and cold flow from the cold flow conduit inducing rotation of the at least one SMA tube at a second end. A generator or alternator is operably connected to the second end of the at least one SMA tube.Type: ApplicationFiled: August 10, 2016Publication date: December 1, 2016Inventors: James H. Mabe, Naveed M. Hussain, Edward A. Whalen, Frederick T. Calkins
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Publication number: 20160169213Abstract: A scalable multi-element shape memory alloy (SMA) rotary motor employs a plurality of SMA tubes. A ratcheting gear transmission couples the plurality of SMA tubes in parallel to a common output. A controller provides power to a plurality of heaters associated with each of the plurality of SMA tubes, sequentially heating selected heaters to provide continuous rotational motion of the common output.Type: ApplicationFiled: December 10, 2014Publication date: June 16, 2016Inventors: Frederick T. Calkins, James H. Mabe, Jonathan K. Brown
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Patent number: 8876046Abstract: A rotational actuator assembly employs a first torsion actuator having a shape memory alloy (SMA) tube with a first trained twist direction and a second torsion actuator having a SMA tube with an opposite trained twist direction collinear with the first torsion actuator with abutting proximal ends. A central fitting joins the proximal ends. A control system for temperature control of the first torsion actuator and second torsion actuator about an average temperature provides combined antagonistic rotation of the central fitting.Type: GrantFiled: September 10, 2010Date of Patent: November 4, 2014Assignee: The Boeing CompanyInventors: Ian Gunter, Robert T. Ruggeri, James H. Mabe, Darin Arbogast, Ordie D. Butterfield, Daniel Morgenroth
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Patent number: 8584987Abstract: Concepts and technologies are disclosed herein for shape memory alloy weapon fairings. The shape memory alloy weapon fairings are formed from a shape memory alloy and are configured to change shape in response to temperature changes. At a first temperature, the shape memory alloy weapon fairing has a first shape and at a second temperature, the shape memory alloy has a second shape. Upon deployment of a weapon including the shape memory alloy weapon fairing, the shape memory alloy weapon fairing is heated by the weapon and/or air friction. The shape memory alloy weapon fairing changes shape in response to the temperature change and provides a fairing for one or more structures of the weapon. In some implementations, the fairing covers a protuberance or other connection mechanism of the weapon.Type: GrantFiled: May 6, 2011Date of Patent: November 19, 2013Assignee: The Boeing CompanyInventors: Casey Lyn Madsen, Daniel John Clingman, James H. Mabe, Frederick Theodore Calkins
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Patent number: 8434293Abstract: A shape memory alloy (SMA) actuated aerostructure operable to dynamically change shape according to flight conditions is disclosed. Deformable structures are actuated by SMA actuators that are coupled to face sheets of the deformable structures. Actuating the SMA actuators produces complex shape changes of the deformable structures by activating shape changes of the SMA actuators. The SMA actuators are actuated via an active or passive temperature change based on operating conditions. The SMA actuated aerostructure can be used for morphable nozzles such as a variable area fan nozzle and/or a variable geometry chevron of a jet engine to reduce engine noise during takeoff without degrading fuel burn during cruise.Type: GrantFiled: August 6, 2009Date of Patent: May 7, 2013Assignee: The Boeing CompanyInventors: Richard D. Widdle, Jr., Matthew T. Grimshaw, Kava S. Crosson-Elturan, James H. Mabe, Frederick T. Calkins, Lynn M. Gravatt, Moushumi Shome
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Patent number: 8343298Abstract: First and second aircraft structures are bonded together with an adhesive including strain-sensitive magnetostrictive material.Type: GrantFiled: December 13, 2007Date of Patent: January 1, 2013Assignee: The Boeing CompanyInventors: Diane C. Rawlings, Robert J. Miller, Kenneth A. Krienke, James H. Mabe, Robert T. Ruggeri, Dan J. Clingman
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Publication number: 20120305167Abstract: First and second aircraft structures are bonded together with an adhesive including strain-sensitive magnetostrictive material.Type: ApplicationFiled: December 13, 2007Publication date: December 6, 2012Applicant: THE BOEING COMPANYInventors: Diane C. Rawlings, Robert J. Miller, Kenneth A. Krienke, James H. Mabe, Robert T. Ruggeri, Dan J. Clingman
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Publication number: 20120282474Abstract: Concepts and technologies are disclosed herein for shape memory alloy weapon fairings. The shape memory alloy weapon fairings are formed from a shape memory alloy and are configured to change shape in response to temperature changes. At a first temperature, the shape memory alloy weapon fairing has a first shape and at a second temperature, the shape memory alloy has a second shape. Upon deployment of a weapon including the shape memory alloy weapon fairing, the shape memory alloy weapon fairing is heated by the weapon and/or air friction. The shape memory alloy weapon fairing changes shape in response to the temperature change and provides a fairing for one or more structures of the weapon. In some implementations, the fairing covers a protuberance or other connection mechanism of the weapon.Type: ApplicationFiled: May 6, 2011Publication date: November 8, 2012Inventors: Casey Lyn Madsen, Daniel John Clingman, James H. Mabe, Frederick Theodore Calkins