Patents by Inventor Adam B. Lubchansky

Adam B. Lubchansky 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: 11230072
    Abstract: An apparatus for fabricating a composite structure includes a tape placement machine including a delivery head configured to dispose a composite tape and a backing plate coupled to the tape placement machine and selectively located relative to the delivery head to react to a placement force applied by the tape placement machine as the composite tape is being disposed.
    Type: Grant
    Filed: July 16, 2018
    Date of Patent: January 25, 2022
    Assignee: The Boeing Company
    Inventors: Keith D. Humfeld, Adam B. Lubchansky
  • Patent number: 10786955
    Abstract: A method for fabricating a composite structure includes steps of: (1) laying up, with a delivery head of a tape placement machine, a continuous segment of a composite tape on a composite panel to form a flange portion of an initial ply of a composite stiffener; (2) locating a backing plate, coupled to the delivery head, relative to the delivery head and the composite panel; and (3) further layup up, with the delivery head, the continuous segment of the composite tape on the backing plate to form a web portion of the initial ply of the composite stiffener.
    Type: Grant
    Filed: July 16, 2018
    Date of Patent: September 29, 2020
    Assignee: The Boeing Company
    Inventors: Keith D. Humfeld, Adam B. Lubchansky
  • Publication number: 20200016849
    Abstract: A method for fabricating a composite structure includes steps of: (1) laying up, with a delivery head of a tape placement machine, a continuous segment of a composite tape on a composite panel to form a flange portion of an initial ply of a composite stiffener; (2) locating a backing plate, coupled to the delivery head, relative to the delivery head and the composite panel; and (3) further layup up, with the delivery head, the continuous segment of the composite tape on the backing plate to form a web portion of the initial ply of the composite stiffener.
    Type: Application
    Filed: July 16, 2018
    Publication date: January 16, 2020
    Applicant: The Boeing Company
    Inventors: Keith D. Humfeld, Adam B. Lubchansky
  • Publication number: 20200016850
    Abstract: An apparatus for fabricating a composite structure includes a tape placement machine including a delivery head configured to dispose a composite tape and a backing plate coupled to the tape placement machine and selectively located relative to the delivery head to react to a placement force applied by the tape placement machine as the composite tape is being disposed.
    Type: Application
    Filed: July 16, 2018
    Publication date: January 16, 2020
    Applicant: The Boeing Company
    Inventors: Keith D. Humfeld, Adam B. Lubchansky
  • Patent number: 9086085
    Abstract: A fastening system includes a fastener having a head portion and a shaft portion, wherein the head portion has a recess (e.g., a removal tool recess), and an insert (e.g., a plastic insert) having an insert shape substantially equal to the recess shape and an insert thickness substantially equal to or less than the recess depth, wherein the insert is configured to removeably seat within the recess of the head portion. In this way, the insert may be later removed from the recess, allowing easy tool access even in applications where an overlying fairing material or other such conformal coating is used.
    Type: Grant
    Filed: July 26, 2006
    Date of Patent: July 21, 2015
    Assignee: The Boeing Company
    Inventors: Adam B. Lubchansky, Mike McCracken
  • Publication number: 20080025815
    Abstract: A fastening system includes a fastener having a head portion and a shaft portion, wherein the head portion has a recess (e.g., a removal tool recess), and an insert (e.g., a plastic insert) having an insert shape substantially equal to the recess shape and an insert thickness substantially equal to or less than the recess depth, wherein the insert is configured to removeably seat within the recess of the head portion. In this way, the insert may be later removed from the recess, allowing easy tool access even in applications where an overlying fairing material or other such conformal coating is used.
    Type: Application
    Filed: July 26, 2006
    Publication date: January 31, 2008
    Inventors: Adam B. Lubchansky, Mike McCracken