Patents by Inventor Paul B. Philipp

Paul B. Philipp 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: 11117004
    Abstract: A fire seal end cap including a cap portion and a plug portion, wherein the plug portion protrudes from the cap portion, and wherein the cap portion and the plug portion are formed from a fire-resistant material.
    Type: Grant
    Filed: January 3, 2018
    Date of Patent: September 14, 2021
    Assignee: The Boeing Company
    Inventors: Scott M. Livingston, Jack W. Mauldin, Robert P. Lotter, Paul B. Philipp, Khalid S. Alshobber, John N. Harris
  • Publication number: 20180140878
    Abstract: A fire seal end cap including a cap portion and a plug portion, wherein the plug portion protrudes from the cap portion, and wherein the cap portion and the plug portion are formed from a fire-resistant material.
    Type: Application
    Filed: January 3, 2018
    Publication date: May 24, 2018
    Applicant: The Boeing Company
    Inventors: Scott M. Livingston, Jack W. Mauldin, Robert P. Lotter, Paul B. Philipp, Khalid S. Alshobber, John N. Harris
  • Patent number: 9889323
    Abstract: A multi-member assembly including a first structural member, a second structural member opposed from the first structural member, a crossover seal positioned between the first and second structural members, wherein the crossover seal defines a bore, and an end cap including a cap portion and a plug portion protruding from the cap portion, wherein the plug portion is at least partially received in the bore such that the cap portion bridges the first and second structural members.
    Type: Grant
    Filed: August 26, 2013
    Date of Patent: February 13, 2018
    Assignee: The Boeing Company
    Inventors: Scott M. Livingston, Jack W. Mauldin, Robert P. Lotter, Paul B. Philipp, Khalid S. Alshobber, John N. Harris
  • Patent number: 9517830
    Abstract: Provided is a captured seal assembly that can be positioned between a first surface and a second surface of a structure or vehicle, such as an aircraft. The captured seal assembly includes a geometric-shaped seal such as a bulb-shaped seal that can be secured to an outer perimeter of the first surface and a receiving land capture that can be secured to an outer perimeter of the second surface. The geometric-shaped seal is designed to engage with the receiving land capture, and join the first surface and second surface when the geometric-shaped seal is engaged with the receiving land capture. In addition, the seal assembly can maintain a differential in pressure between a first region adjacent to the first surface and a second region adjacent to the second surface.
    Type: Grant
    Filed: March 18, 2014
    Date of Patent: December 13, 2016
    Assignee: The Boeing Company
    Inventors: Sham S. Hariram, Paul B. Philipp
  • Publication number: 20150266561
    Abstract: Provided is a captured seal assembly that can be positioned between a first surface and a second surface of a structure or vehicle, such as an aircraft. The captured seal assembly includes a geometric-shaped seal such as a bulb-shaped seal that can be secured to an outer perimeter of the first surface and a receiving land capture that can be secured to an outer perimeter of the second surface. The geometric-shaped seal is designed to engage with the receiving land capture, and join the first surface and second surface when the geometric-shaped seal is engaged with the receiving land capture. In addition, the seal assembly can maintain a differential in pressure between a first region adjacent to the first surface and a second region adjacent to the second surface.
    Type: Application
    Filed: March 18, 2014
    Publication date: September 24, 2015
    Applicant: The Boeing Company
    Inventors: Sham S. Hariram, Paul B. Philipp
  • Publication number: 20140262358
    Abstract: A multi-member assembly including a first structural member, a second structural member opposed from the first structural member, a crossover seal positioned between the first and second structural members, wherein the crossover seal defines a bore, and an end cap including a cap portion and a plug portion protruding from the cap portion, wherein the plug portion is at least partially received in the bore such that the cap portion bridges the first and second structural members.
    Type: Application
    Filed: August 26, 2013
    Publication date: September 18, 2014
    Applicant: The Boeing Company
    Inventors: Scott M. Livingston, Jack W. Mauldin, Robert P. Lotter, Paul B. Philipp, Khalid S. Alshobber, John N. Harris