Patents by Inventor Richard M. Cima

Richard M. Cima 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: 4903761
    Abstract: A two-phase closed-loop heat transfer system comprises a capillary-type evaporator 10, a condenser 11 (preferably also of the capillary-type), and a vapor conduit 17 through which heat-laden working fluid in vapor phase is driven adiabatically from the evaporator 10 to the condenser 11. The evaporator 10 comprises a plurality of tubes 12 connected in parallel. A helically threaded capillary channel 39 is formed on the cylindrical interior surface of each tube 12, and a wick assembly 33 is positioned longitudinally within each tube 12. Each wick assembly 33 comprises a high-permeability wick 36 within which are embedded a first tubule 34 and a second tubule 35. The first and second tubules 34 and 35 are of low permeability, and have one closed end and one open end. The open end of the first tubule 34 is connected to a feed line 16 through which liquid-phase working fluid is delivered into the first tubule 34.
    Type: Grant
    Filed: June 3, 1987
    Date of Patent: February 27, 1990
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Richard M. Cima
  • Patent number: 4890668
    Abstract: A two-phase closed-loop heat transfer system comprises a capillary-type evaporator 10, a condenser 11 (preferably also of the capillary type), and a vapor conduit 17 through which heat-laden working fluid in vapor phase is driven adiabatically from the evaporator 10 to the condenser 11. The evaporator 10 comprises a plurality of tubes 12 connected in parallel. A helically threaded capillary channel 39 is formed on the cylindrical interior surface of each tube 12, and a wick assembly 33 is positioned longitudinally within each tube 12. Each wick assembly 33 comprises a high-permeability wick 36 within which are embedded a first tubule 34 and a second tubule 35. The first and second tubules 34 and 35 are of low permeability, and have one closed end and one open end. The open end of the first tubule 34 is connected to a feed line 16 through which liquid-phase working fluid is delivered into the first tubule 34.
    Type: Grant
    Filed: November 7, 1988
    Date of Patent: January 2, 1990
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Richard M. Cima