Patents by Inventor Max L. Blosser

Max L. Blosser 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: 9051063
    Abstract: A heat shield for a space vehicle comprises a plurality of phenolic impregnated carbon ablator (PICA) blocks secured to a surface of the space vehicle and arranged in a pattern with gaps therebetween. The heat shield further comprises a plurality of PICA strips disposed in the gaps between the PICA blocks. The PICA strips are mounted edgewise, such that the structural orientation of the PICA strips is substantially perpendicular to the structural orientation of the PICA blocks.
    Type: Grant
    Filed: January 29, 2013
    Date of Patent: June 9, 2015
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Max L. Blosser, Carl C. Poteet, Stan A. Bouslog
  • Patent number: 8236413
    Abstract: A combination structural support and thermal protection system is provided. A cured preceramic polymer matrix reinforced with carbon fibers can be used alone or in a multiple component system.
    Type: Grant
    Filed: July 2, 2008
    Date of Patent: August 7, 2012
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: H. Kevin Rivers, Stephen J. Scotti, Lynn M. Bowman, Max L. Blosser
  • Publication number: 20100000176
    Abstract: A combination structural support and thermal protection system is provided. A cured preceramic polymer matrix reinforced with carbon fibers can be used alone or in a multiple component system.
    Type: Application
    Filed: July 2, 2008
    Publication date: January 7, 2010
    Applicant: U.S.A. as Represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: H. Kevin Rivers, Stephen J. Scotti, Lynn M. Bowman, Max L. Blosser
  • Patent number: 5238056
    Abstract: Various heat exchange apparatuses are described in which an oscillating flow of primary coolant is used to dissipate an incident heat flux. The oscillating flow may be imparted by a reciprocating piston, a double action twin reciprocating piston, fluidic oscillators or electromagnetic pumps. The oscillating fluid flows through at least one conduit in either an open loop or a closed loop. A secondary flow of coolant may be used to flow over the outer walls of at least one conduit to remove heat transferred from the primary coolant to the walls of the conduit.
    Type: Grant
    Filed: February 24, 1992
    Date of Patent: August 24, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stephen J. Scotti, Max L. Blosser, Charles J. Camarda
  • Patent number: 5107920
    Abstract: Various heat exchange apparatuses are described in which an oscillating flow of primary coolant is used to dissipate an incident heat flux. The oscillating flow may be imparted by a reciprocating piston, a double action twin reciprocating piston, fluidic oscillators or electromagnetic pumps. The oscillating fluid flows through at least one conduit in either an open loop or a closed loop. A second flow of coolant may be used to flow over the outer walls of at least one conduit to remove heat transferred from the primary coolant to the walls of the conduit.
    Type: Grant
    Filed: March 30, 1990
    Date of Patent: April 28, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Stephen J. Scotti, Max L. Blosser, Charles J. Camarda