Patents by Inventor Daniel John Clingman

Daniel John 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).

  • Patent number: 11871673
    Abstract: Actuator assemblies, mechanical assemblies including the actuator assemblies, and methods of fabricating the same are disclosed herein. The actuator assemblies include a piezoelectric element having a first side and a second side, a first electrode in electrical communication with the first side, and a second electrode in electrical communication with the second side. The first electrode includes a flexible, electrically conductive membrane. The mechanical assemblies include a first structure, which includes a first interface surface, a second structure, which includes a second interface surface, and the actuator assembly. The actuator assembly is configured to provide a motive force for relative motion between the first structure and the second structure. The methods include defining a first electrode on a first side of a piezoelectric element and defining a second electrode on a second side of the piezoelectric element. The first electrode includes a flexible, electrically conductive membrane.
    Type: Grant
    Filed: April 9, 2020
    Date of Patent: January 9, 2024
    Assignee: The Boeing Company
    Inventor: Daniel John Clingman
  • Publication number: 20200243747
    Abstract: Actuator assemblies, mechanical assemblies including the actuator assemblies, and methods of fabricating the same are disclosed herein. The actuator assemblies include a piezoelectric element having a first side and a second side, a first electrode in electrical communication with the first side, and a second electrode in electrical communication with the second side. The first electrode includes a flexible, electrically conductive membrane. The mechanical assemblies include a first structure, which includes a first interface surface, a second structure, which includes a second interface surface, and the actuator assembly. The actuator assembly is configured to provide a motive force for relative motion between the first structure and the second structure. The methods include defining a first electrode on a first side of a piezoelectric element and defining a second electrode on a second side of the piezoelectric element. The first electrode includes a flexible, electrically conductive membrane.
    Type: Application
    Filed: April 9, 2020
    Publication date: July 30, 2020
    Inventor: Daniel John Clingman
  • Patent number: 10658565
    Abstract: Actuator assemblies, mechanical assemblies including the actuator assemblies, and methods of fabricating the same are disclosed herein. The actuator assemblies include a piezoelectric element having a first side and a second side, a first electrode in electrical communication with the first side, and a second electrode in electrical communication with the second side. The first electrode includes a flexible, electrically conductive membrane. The mechanical assemblies include a first structure, which includes a first interface surface, a second structure, which includes a second interface surface, and the actuator assembly. The actuator assembly is configured to provide a motive force for relative motion between the first structure and the second structure. The methods include defining a first electrode on a first side of a piezoelectric element and defining a second electrode on a second side of the piezoelectric element. The first electrode includes a flexible, electrically conductive membrane.
    Type: Grant
    Filed: August 29, 2016
    Date of Patent: May 19, 2020
    Assignee: The Boeing Company
    Inventor: Daniel John Clingman
  • Publication number: 20180062066
    Abstract: Actuator assemblies, mechanical assemblies including the actuator assemblies, and methods of fabricating the same are disclosed herein. The actuator assemblies include a piezoelectric element having a first side and a second side, a first electrode in electrical communication with the first side, and a second electrode in electrical communication with the second side. The first electrode includes a flexible, electrically conductive membrane. The mechanical assemblies include a first structure, which includes a first interface surface, a second structure, which includes a second interface surface, and the actuator assembly. The actuator assembly is configured to provide a motive force for relative motion between the first structure and the second structure. The methods include defining a first electrode on a first side of a piezoelectric element and defining a second electrode on a second side of the piezoelectric element. The first electrode includes a flexible, electrically conductive membrane.
    Type: Application
    Filed: August 29, 2016
    Publication date: March 1, 2018
    Inventor: Daniel John Clingman
  • Patent number: 8584987
    Abstract: 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: Grant
    Filed: May 6, 2011
    Date of Patent: November 19, 2013
    Assignee: The Boeing Company
    Inventors: Casey Lyn Madsen, Daniel John Clingman, James H. Mabe, Frederick Theodore Calkins
  • Publication number: 20120282474
    Abstract: 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: Application
    Filed: May 6, 2011
    Publication date: November 8, 2012
    Inventors: Casey Lyn Madsen, Daniel John Clingman, James H. Mabe, Frederick Theodore Calkins