Patents by Inventor James R. French

James R. French 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: 11963717
    Abstract: An energy delivery system includes an RF synthesizer circuit configured to generate an RF electric signal and a preamplification stage operably coupled to the RF synthesizer circuit. The preamplification stage has at least one attenuator. A board controller is operably coupled to the attenuator of the preamplification stage that is configured to modify a gain setting of the attenuator. An output connection is configured to provide a low-power signal or a high-power signal based on at least the RF electric signal and the gain setting. The low-power signal or high-power signal is provided to an RF applicator configured to couple an alternating RF electric field to animal tissue.
    Type: Grant
    Filed: June 7, 2019
    Date of Patent: April 23, 2024
    Assignee: Nova-Tech Engineering, LLC
    Inventors: Marc S. Gorans, James J. Kleven, Wade D. Werder, Jacob R. French, Derek Worcester
  • Patent number: 11933249
    Abstract: Systems and methods for a fully reusable upper stage for a multi-stage launch vehicle are provided. The reusable upper stage uses an aerospike engine for main propulsion and for vertical landing. A heat shield can include a plurality of scarfed nozzles embedded radially around a semi-spherical surface of the heat shield, wherein inboard surfaces of the plurality of scarfed nozzles collectively define an aerospike contour. The heat shield can be actively cooled to dissipate heat encountered during reentry of the upper stage.
    Type: Grant
    Filed: July 8, 2022
    Date of Patent: March 19, 2024
    Assignee: Blue Origin, LLC
    Inventors: James R. French, Roger Eugene Ramsey, Adam Wuerl
  • Publication number: 20230211900
    Abstract: Systems and methods for a fully reusable upper stage for a multi-stage launch vehicle are provided. The reusable upper stage uses an aerospike engine for main propulsion and for vertical landing. A heat shield can include a plurality of scarfed nozzles embedded radially around a semi-spherical surface of the heat shield, wherein inboard surfaces of the plurality of scarfed nozzles collectively define an aerospike contour. The heat shield can be actively cooled to dissipate heat encountered during reentry of the upper stage.
    Type: Application
    Filed: July 8, 2022
    Publication date: July 6, 2023
    Inventors: James R. French, Roger Eugene Ramsey, Adam Wuerl
  • Patent number: 5873549
    Abstract: A nose assembly and method for controlling the rotation and stabilizing the orientation of a vehicle during landing maneuvers. The vehicle includes a nose assembly that is coupled to an airframe thereof and that has a frame and flap assembly. The flap assembly includes an actuating means and a flap coupled to the frame such that the actuating means moves the flap from and between a fully retracted position and a fully extended position in response to a guidance signal received from a flight control computer. In a preferred embodiment of the present invention, the flap assembly includes a plurality of flaps each coupled to the nose assembly frame and an actuating means that selectively positions the plurality of flaps in response to a signal.
    Type: Grant
    Filed: September 25, 1996
    Date of Patent: February 23, 1999
    Assignee: McDonnell Douglas Corporation
    Inventors: Jeffery G. Lane, James R. French
  • Patent number: 4699754
    Abstract: The invention does away with the necessity of moving parts such as a check valve in a nuclear reactor cooling system. Instead, a jet pump, in combination with a TEMP, is employed to assure safe cooling of a nuclear reactor after shutdown. A main flow exists for a reactor coolant. A point of withdrawal is provided for a secondary flow. A TEMP, responsive to the heat from said coolant in the secondary flow path, automatically pumps said withdrawn coolant to a higher pressure and thus higher velocity compared to the main flow. The high velocity coolant is applied as a driver flow for the jet pump which has a main flow chamber located in the main flow circulation pump. Upon nuclear shutdown and loss of power for the main reactor pumping system, the TEMP/jet pump combination continues to boost the coolant flow in the direction it is already circulating.
    Type: Grant
    Filed: May 31, 1985
    Date of Patent: October 13, 1987
    Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space Administration
    Inventor: James R. French
  • Patent number: 4418437
    Abstract: Apparatus for cleaning the bore of a pipe comprising a cleaning tool motor having a housing and a drive shaft which extends from the housing and which is adapted to receive a pipe cleaning tool rotatable with the drive shaft, three guide wheels, which are supported by arms connected to the housing and which are disposed around the housing in spaced apart relationship towards the drive shaft end of the housing so as to use to bear against the bore of a pipe to be cleaned thereby to position the drive shaft coaxially of the pipe, a drive wheel, a drive motor operatively associated with the drive wheel for driving the apparatus through a pipe to be cleaned, a jacking arm for the drive wheel which extends away from the end of the housing remote from the drive shaft, and a jacking arm actuator operative for jacking the drive wheel into driving contact with the walls of a pipe to be cleaned.
    Type: Grant
    Filed: March 5, 1982
    Date of Patent: December 6, 1983
    Inventor: James R. French