Patents by Inventor Donald R. Senterfitt

Donald R. Senterfitt 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: 4966229
    Abstract: Heat pipe (10) includes an acute angle leading wedge shape form (38) with a radiused leading edge (26). Engine fuel supply (65) cools the trailing wedge shape form (40). The intense heat flux at the leading edge is cleanly dissipated and spread over substantial heat pipe cooling surface (64, 66). A coating (36) on the external surface of the leading edge wedge shape form is formed of a layer of iridium and a layer of oxide.
    Type: Grant
    Filed: December 26, 1989
    Date of Patent: October 30, 1990
    Assignee: United Technologies Corporation
    Inventors: Donald R. Senterfitt, James R. Mullaly, Larry D. Hamner, Abdus S. Khan, John G. Smeggil
  • Patent number: 4743104
    Abstract: A laser ring mirror assembly is disclosed which supports and cools an annular ring mirror of a high powered laser with a cooling manifold which has a coolant flow design which is intended to reduce thermal distortions of the ring mirror by minimizing azimuthal variations in temperature around its circumference. The cooling manifold has complementary pairs of cooling passages each of which conduct coolant in opposite flow directions. The manifold also houses adjusters which vary the depth between the annular ring mirror and each cooling passage, and which vary the flow area of the cooling passage to produce a control over the cooling characteristics of the cooling manifold.
    Type: Grant
    Filed: October 14, 1986
    Date of Patent: May 10, 1988
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Albert Eng, Donald R. Senterfitt
  • Patent number: 4171093
    Abstract: A flap and seal assembly for an exhaust nozzle having a flap liner and seal liner which are in slidable engagement with one another. The seal liner has a facesheet, grid sheet and corrugated supporting sheet while the flap liner has a facesheet and an inner support sheet. The specific inter-relationship between the various elements of the flap and seal liner provides improved support, hot gas aspiration as well as vibratory damping which thereby allows for the use of thinner materials in the construction of the liner assembly.
    Type: Grant
    Filed: August 19, 1977
    Date of Patent: October 16, 1979
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Fred L. Honeycutt, Jr., Donald R. Senterfitt