Patents by Inventor Dan J. Clingman
Dan J. Clingman 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: 20080092354Abstract: A method of manufacturing a piezoelectric beam is provided. The method includes inserting a piezoelectric body and a pair of roller pins into an injection molding form. Once the piezoelectric body and roller pins are enclosed within the injection mold form a liquefied substance is injected into the injection molding form. The liquefied substance solidifies to substantially permanently affix the roller pins to opposing distal ends of the body.Type: ApplicationFiled: October 20, 2006Publication date: April 24, 2008Inventors: Dan J. Clingman, Jack Thiesen
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Patent number: 7307585Abstract: An aircraft aeroelasticity measurement system according to the invention can be used to perform in-flight wing twist measurements of an aircraft or any moving vehicle or structure on which its sensors can be mounted. The system includes a centralized processing unit, a reference navigation unit mounted in the aircraft body, a plurality of measurement navigation units mounted in the aircraft wings, and a global positioning system (“GPS”) receiver that generates GPS data for enhancing the accuracy of the navigation data. The system collects navigation data from the reference navigation unit and the measurement navigation units, generates navigation solutions from the navigation data, and performs a stochastic alignment and flexure estimation procedure to generate a corrected measurement solution that indicates the aeroelasticity of the aircraft. Wing twist and wing deflection information can be derived from the corrected measurement solution.Type: GrantFiled: November 1, 2005Date of Patent: December 11, 2007Assignee: The Boeing CompanyInventors: Harris O. Hinnant, Jr., Darin W. Brekke, Dan J. Clingman
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Patent number: 7202591Abstract: The present invention presents a system for a compound actuator. The system includes first and second electrode layers each including two electrode sections, an intermediate electrode layer between the first and second electrode layers, and first and second electrostrictive materials that change length in an applied electrical field. The first electrostrictive material is positioned between the first and intermediate electrode layers. The second electrostrictive material is positioned between the intermediate and second electrode layers. The first electrostrictive material has a first length adjoining the first electrode section and a second length adjoining the second electrode section. The second electrostrictive material has a third length adjoining the fourth electrode section and a fourth length adjoining the fifth electrode section.Type: GrantFiled: July 7, 2005Date of Patent: April 10, 2007Assignee: The Boeing CompanyInventors: Darin J. Arbogast, Frederick T. Calkins, Dan J. Clingman
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Patent number: 7037076Abstract: A preferred rotary actuator includes an actuator assembly having a torque tube formed of a shape memory alloy (SMA), a superelastic NiTinol return spring associated with the torque tube and adapted to bias the torque tube toward an initial position, and a torque tube heating element, especially a thermoelectric device, for switching the SMA to cause rotation to an object connected to the actuator or to generate a torque upon that object. The torque tube (24) includes a proximal end (32) and a distal end (34). The return spring and torque tube are connected at their ends, with the torque tube being pretwisted while in a martensitic state relative to the spring. Activation of the heating element causes the torque tube to enter an austenitic state in which it returns to its previous untwisted configuration. Removal of heat allows the torque tube to return to a martensitic state, when the return spring retwists the torque tube. A unique locking assembly 22 is used with the preferred actuator assembly.Type: GrantFiled: August 10, 2002Date of Patent: May 2, 2006Assignee: The Boeing CompanyInventors: A. Dean Jacot, Robert T. Ruggeri, Dan J. Clingman
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Patent number: 6994762Abstract: A single crystal piezo (SCP) apparatus and method of forming same. The apparatus is ideally suited for actuator and energy harvesting applications. The apparatus includes an SCP layer bonded to a surface of a flexible metal layer while the metal layer is held flattened within a press or other tool. Once the bonding process is complete, the metal layer imparts a compressive strain to the SCP layer bonded thereto. A layer of uniaxial graphite may also be bonded to the SCP layer to eliminate the poison's ratio tension that would otherwise be created in the SCP layer.Type: GrantFiled: February 10, 2003Date of Patent: February 7, 2006Assignee: The Boeing CompanyInventors: Dan J. Clingman, A. Dean Jacot
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Patent number: 6933662Abstract: The present invention presents a system for a compound actuator. The system includes first and second electrode layers each including two electrode sections, an intermediate electrode layer between the first and second electrode layers, and first and second electrostrictive materials that change length in an applied electrical field. The first electrostrictive material is positioned between the first and intermediate electrode layers. The second electrostrictive material is positioned between the intermediate and second electrode layers. The first electrostrictive material has a first length adjoining the first electrode section and a second length adjoining the second electrode section. The second electrostrictive material has a third length adjoining the fourth electrode section and a fourth length adjoining the fifth electrode section.Type: GrantFiled: February 27, 2003Date of Patent: August 23, 2005Assignee: The Boeing CompanyInventors: Darin J. Arbogast, Frederick T. Calkins, Dan J. Clingman
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Patent number: 6894460Abstract: A circuit passively discharges energy from a piezoelectric device and stores the energy in a power storage element. The circuit has two parallel flow paths each including a diode set and an inductor electrically connected to opposite sides of a piezoelectric device. A power storage element is connected to both inductors. The diode sets are alternately forward biased, and energy from the piezoelectric device discharges through the inductor(s). A portion of the energy is stored in the inductor(s) and the remaining portion is stored in the power storage element. The benefits achieved include passive switching between the parallel circuit paths through diodes in place of traditional switches, and the additional energy stored by the inductors which is also transferred to the power storage element. Passive switching conserves additional energy.Type: GrantFiled: January 9, 2003Date of Patent: May 17, 2005Assignee: The Boeing CompanyInventor: Dan J. Clingman
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Publication number: 20040154730Abstract: A single crystal piezo (SCP) apparatus and method of forming same. The apparatus is ideally suited for actuator and energy harvesting applications. The apparatus includes an SCP layer bonded to a surface of a flexible metal layer while the metal layer is held flattened within a press or other tool. Once the bonding process is complete, the metal layer, it imparts a compressive strain to the SCP layer bonded thereto. A layer of uniaxial graphite may also be bonded to the SCP layer to eliminate the poison's ratio tension that would otherwise be created in the SCP layer.Type: ApplicationFiled: February 10, 2003Publication date: August 12, 2004Inventors: Dan J. Clingman, A. Dean Jacot
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Publication number: 20040135554Abstract: A circuit passively discharges energy from a piezoelectric device and stores the energy in a power storage element. The circuit has two parallel flow paths each including a diode set and an inductor electrically connected to opposite sides of a piezoelectric device. A power storage element is connected to both inductors. The diode sets are alternately forward biased, and energy from the piezoelectric device discharges through the inductor(s). A portion of the energy is stored in the inductor(s) and the remaining portion is stored in the power storage element. The benefits achieved include passive switching between the parallel circuit paths through diodes in place of traditional switches, and the additional energy stored by the inductors which is also transferred to the power storage element. Passive switching conserves additional energy.Type: ApplicationFiled: January 9, 2003Publication date: July 15, 2004Inventor: Dan J. Clingman
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Publication number: 20040084986Abstract: The present invention presents a system for a compound actuator. The system includes first and second electrode layers each including two electrode sections, an intermediate electrode layer between the first and second electrode layers, and first and second electrostrictive materials that change length in an applied electrical field. The first electrostrictive material is positioned between the first and intermediate electrode layers. The second electrostrictive material is positioned between the intermediate and second electrode layers. The first electrostrictive material has a first length adjoining the first electrode section and a second length adjoining the second electrode section. The second electrostrictive material has a third length adjoining the fourth electrode section and a fourth length adjoining the fifth electrode section.Type: ApplicationFiled: February 27, 2003Publication date: May 6, 2004Inventors: Darin J. Arbogast, Frederick T. Calkins, Dan J. Clingman
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Publication number: 20030053912Abstract: A preferred rotary actuator includes an actuator assembly having a torque tube formed of a shape memory alloy (SMA), a superelastic NiTinol return spring associated with the torque tube and adapted to bias the torque tube toward an initial position, and a torque tube heating element, especially a thermoelectric device, for switching the SMA to cause rotation to an object connected to the actuator or to generate a torque upon that object. The torque tube (24) includes a proximal end (32) and a distal end (34). The return spring and torque tube are connected at their ends, with the torque tube being pretwisted while in a martensitic state relative to the spring. Activation of the heating element causes the torque tube to enter an austenitic state in which it returns to its previous untwisted configuration. Removal of heat allows the torque tube to return to a martensitic state, when the return spring retwists the torque tube. A unique locking assembly 22 is used with the preferred actuator assembly.Type: ApplicationFiled: August 10, 2002Publication date: March 20, 2003Applicant: The Boeing CompanyInventors: A. Dean Jacot, Robert T. Ruggeri, Dan J. Clingman
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Patent number: 6499952Abstract: A preferred rotary actuator includes an actuator assembly having a torque tube formed of a shape memory alloy (SMA), a superelastic NiTinol return spring associated with the torque tube and adapted to bias the torque tube toward an initial position, and a torque tube heating element, especially a thermoelectric device, for switching the SMA to cause rotation to an object connected to the actuator or to generate a torque upon that object. The torque tube (24) includes a proximal end (32) and a distal end (34). The return spring and torque tube are connected at their ends, with the torque tube being pretwisted while in a martensitic state relative to the spring. Activation of the heating element causes the torque tube to enter an austenitic state in which it returns to its previous untwisted configuration. Removal of heat allows the torque tube to return to a martensitic state, when the return spring retwists the torque tube. A unique locking assembly 22 is used with the preferred actuator assembly.Type: GrantFiled: February 28, 2000Date of Patent: December 31, 2002Assignee: The Boeing CompanyInventors: A. Dean Jacot, Robert T. Ruggeri, Dan J. Clingman
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Patent number: 6065934Abstract: A rotary actuator (18) is provided, including an actuator assembly (20). The actuator assembly includes a torque tube (24) formed of a shape memory alloy, a super elastic NiTinol return spring (26) having a proximal end (46) and a distal end (44), and a torque tube heating element (30) positioned near the torque tube. The torque tube (24) includes a proximal end (32) and a distal end (34). The return spring and torque tube are connected at their ends, with the torque tube being pretwisted while in a martensitic state relative to the spring. Activation of the heating element causes the torque tube to enter an austenitic state in which it returns to its previous untwisted configuration. Removal of heat allows the torque tube to return to a martensitic state, further allowing the return spring to retwist the torque tube. Further provided is a unique locking assembly (22) for use with the actuator assembly.Type: GrantFiled: February 27, 1998Date of Patent: May 23, 2000Assignee: The Boeing CompanyInventors: Arthur Dean Jacot, Gerald J. Julien, Dan J. Clingman