Patents by Inventor Aristidis Sidiropoulos

Aristidis Sidiropoulos 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: 11603963
    Abstract: Disclosed herein is a structure that comprises a tank including an outer cylindrical surface and a domed end. The structure also comprises a tank skirt positioned circumferentially around the tank. A wall of the tank and a wall of the tank skirt form two sides of a y-joint between the tank and the tank skirt. The y-joint includes a wedge structure positioned between the tank and the tank skirt. Additionally, a thickness of at least one of the wall of the tank or the wall of the tank skirt forming the y-joint tapers such that the thickness of the at least one of the wall of the tank or the wall of the tank skirt that tapers has a greater thickness at the y-joint than away from the y-joint.
    Type: Grant
    Filed: January 12, 2021
    Date of Patent: March 14, 2023
    Assignee: The Boeing Company
    Inventors: Aristidis Sidiropoulos, William P. Keith
  • Publication number: 20210148511
    Abstract: Disclosed herein is a structure that comprises a tank including an outer cylindrical surface and a domed end. The structure also comprises a tank skirt positioned circumferentially around the tank. A wall of the tank and a wall of the tank skirt form two sides of a y-joint between the tank and the tank skirt. The y-joint includes a wedge structure positioned between the tank and the tank skirt. Additionally, a thickness of at least one of the wall of the tank or the wall of the tank skirt forming the y-joint tapers such that the thickness of the at least one of the wall of the tank or the wall of the tank skirt that tapers has a greater thickness at the y-joint than away from the y-joint.
    Type: Application
    Filed: January 12, 2021
    Publication date: May 20, 2021
    Inventors: Aristidis Sidiropoulos, William P. Keith
  • Patent number: 10920932
    Abstract: Disclosed herein is a structure that comprises a tank including an outer cylindrical surface and a domed end. The structure also comprises a tank skirt positioned circumferentially around the tank. A wall of the tank and a wall of the tank skirt form two sides of a y-joint between the tank and the tank skirt. The y-joint includes a wedge structure positioned between the tank and the tank skirt. Additionally, a thickness of at least one of the wall of the tank or the wall of the tank skirt forming the y-joint tapers such that the thickness of the at least one of the wall of the tank or the wall of the tank skirt that tapers has a greater thickness at the y-joint than away from the y-joint.
    Type: Grant
    Filed: January 8, 2019
    Date of Patent: February 16, 2021
    Assignee: The Boeing Company
    Inventors: Aristidis Sidiropoulos, William P. Keith
  • Publication number: 20200217454
    Abstract: Disclosed herein is a structure that comprises a tank including an outer cylindrical surface and a domed end. The structure also comprises a tank skirt positioned circumferentially around the tank. A wall of the tank and a wall of the tank skirt form two sides of a y-joint between the tank and the tank skirt. The y-joint includes a wedge structure positioned between the tank and the tank skirt. Additionally, a thickness of at least one of the wall of the tank or the wall of the tank skirt forming the y-joint tapers such that the thickness of the at least one of the wall of the tank or the wall of the tank skirt that tapers has a greater thickness at the y-joint than away from the y-joint.
    Type: Application
    Filed: January 8, 2019
    Publication date: July 9, 2020
    Inventors: Aristidis Sidiropoulos, William P. Keith
  • Patent number: 10480451
    Abstract: Methods and systems for restricting movement in a flow mixer including a plurality of lobes that each includes a trough, using a stiffener mechanism, are provided. The stiffener mechanism includes a first end portion configured to be coupled to a first lobe of the plurality of lobes and a second end portion configured to be coupled to a second lobe of the plurality of lobes. The stiffener mechanism also includes a body portion coupled between the first end portion and the second end portion such that the body portion is configured to restrict movement of the first and second lobes.
    Type: Grant
    Filed: April 17, 2015
    Date of Patent: November 19, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Thomas Richardson Pinney, Michael Best, Jonathan D. Embler, William P. Keith, Aristidis Sidiropoulos, Edward T. Tong
  • Patent number: 10119449
    Abstract: Methods and systems for restricting movement in a flow mixer of an exhaust duct, the flow mixer having a first row of flutes and a second row of flutes generally opposite to the first row of flutes, each flute being elongated and defining an elongated axis. At least two flute ties connect, or couple, together at least two flutes from the first row of flutes and at least two flutes from the second row of flutes. A retainer is coupled to the flute ties and extends generally perpendicularly to the elongated axis of each of the flutes from the first and second rows of flutes. The combination of the retainer and flute ties is configured to generally restrain relative movement between the flutes from the first row and the flutes from the second row.
    Type: Grant
    Filed: August 2, 2016
    Date of Patent: November 6, 2018
    Assignee: THE BOEING COMPANY
    Inventors: Eric Matthews Boekeloo, William Preston Keith, Michael Best, Aristidis Sidiropoulos, Thomas Richardson Pinney
  • Publication number: 20180038261
    Abstract: Methods and systems for restricting movement in a flow mixer of an exhaust duct, the flow mixer having a first row of flutes and a second row of flutes generally opposite to the first row of flutes, each flute being elongated and defining an elongated axis. At least two flute ties connect, or couple, together at least two flutes from the first row of flutes and at least two flutes from the second row of flutes. A retainer is coupled to the flute ties and extends generally perpendicularly to the elongated axis of each of the flutes from the first and second rows of flutes. The combination of the retainer and flute ties is configured to generally restrain relative movement between the flutes from the first row and the flutes from the second row.
    Type: Application
    Filed: August 2, 2016
    Publication date: February 8, 2018
    Inventors: Eric Matthews Boekeloo, William Preston Keith, Michael Best, Aristidis Sidiropoulos, Thomas Richardson Pinney
  • Publication number: 20160305369
    Abstract: Methods and systems for restricting movement in a flow mixer including a plurality of lobes that each includes a trough, using a stiffener mechanism, are provided. The stiffener mechanism includes a first end portion configured to be coupled to a first lobe of the plurality of lobes and a second end portion configured to be coupled to a second lobe of the plurality of lobes. The stiffener mechanism also includes a body portion coupled between the first end portion and the second end portion such that the body portion is configured to restrict movement of the first and second lobes.
    Type: Application
    Filed: April 17, 2015
    Publication date: October 20, 2016
    Inventors: Thomas Richardson Pinney, Michael Best, Jonathan D. Embler, William P. Keith, Aristidis Sidiropoulos, Edward T. Tong
  • Patent number: 8581736
    Abstract: A strain measurement device to assess the integrity of a structural repair to a surface comprises a detector, a processor, and a memory module coupled to the processor. The memory module comprises logic instructions stored in a computer readable medium which, when executed by the processor, configure the processor to use the detector to obtain a first strain measurement from an external strain indicator, use the detector to obtain a second strain measurement from the measurement sensor after at least one stress test is applied to the structural repair, and generate a signal when a difference between the first strain measurement and the second strain measurement exceeds a threshold.
    Type: Grant
    Filed: June 24, 2010
    Date of Patent: November 12, 2013
    Assignee: The Boeing Company
    Inventors: Keith L. McIver, Aristidis Sidiropoulos, Russell L. Keller, Cong N. Duong
  • Publication number: 20110316712
    Abstract: A strain measurement device to assess the integrity of a structural repair to a surface comprises a detector, a processor, and a memory module coupled to the processor. The memory module comprises logic instructions stored in a computer readable medium which, when executed by the processor, configure the processor to use the detector to obtain a first strain measurement from an external strain indicator, use the detector to obtain a second strain measurement from the measurement sensor after at least one stress test is applied to the structural repair, and generate a signal when a difference between the first strain measurement and the second strain measurement exceeds a threshold.
    Type: Application
    Filed: June 24, 2010
    Publication date: December 29, 2011
    Inventors: KEITH L. MCIVER, Aristidis Sidiropoulos, Russell L. Keller, Cong N. Duong