Patents by Inventor Loren L. Alderson

Loren L. Alderson 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: 4373869
    Abstract: A warm-up valve in a load responsive hydraulic system which connects the pump discharge pressure with the pump compensator while bypassing to reservoir a partial capacity of the pump. When proper reservoir temperature is reached, a thermostatically controlled solenoid closes the warm-up valve causing the pump to return to low pressure standby.
    Type: Grant
    Filed: August 22, 1980
    Date of Patent: February 15, 1983
    Assignee: The Cessna Aircraft Company
    Inventors: Robert J. Martin, Loren L. Alderson, Jerry F. Carlin
  • Patent number: 4280403
    Abstract: Hydraulic "squeeze cylinders" control the size of the discharge orifice on an extrusion baler and are operated by a control circuit that relieves pressure in the cylinders in response to the build-up of a certain predetermined pressure level in the circuit. Pressurized fluid for the squeeze cylinders is supplied by a single-acting pump cylinder that is connected between the plunger head and its pitman rod in such a way as to deliver a charge of pressurized fluid into the circuit on each compression stroke of the plunger. A pilot-operated relief valve is operated by circuit pressure when the latter reaches a predetermined pressure level to block flow from the pump cylinder and open a relief path for fluid in the squeeze cylinders.
    Type: Grant
    Filed: August 13, 1979
    Date of Patent: July 28, 1981
    Assignee: The Cessna Aircraft Company
    Inventor: Loren L. Alderson
  • Patent number: 4192337
    Abstract: An improvement to a priority valve which provides priority flow to a priority function, not only directly from a fluid power source, but also from an accumulator when the priority demand exceeds the output of the fluid power source. This priority flow valve also provides flow to one or more secondary functions when the priority flow requirements are satisfied or when the priority flow path is blocked.
    Type: Grant
    Filed: August 7, 1978
    Date of Patent: March 11, 1980
    Assignee: The Cessna Aircraft Company
    Inventors: Loren L. Alderson, Delbert E. Truesdell
  • Patent number: 4168659
    Abstract: Hydraulic "squeeze cylinders" control the size of the discharge orifice on an extrusion baler and are operated by a control circuit that relieves pressure in the cylinders in response to the buildup of a certain predetermined pressure level in the circuit. Pressurized fluid for the squeeze cylinders is supplied by a single-acting pump cylinder that is connected between the reciprocal plunger head and its push rod in such a way as to deliver a slug of pressurized fluid into the circuit on each compression stroke of the plunger, the pump drawing in a fresh slug from a reservoir during each retraction stroke of the plunger.
    Type: Grant
    Filed: February 28, 1978
    Date of Patent: September 25, 1979
    Assignee: Hesston Corporation
    Inventors: George Yatcilla, Garold L. Fleming, Kurt Graber, Loren L. Alderson
  • Patent number: 3984978
    Abstract: An auxiliary hydraulic front wheel drive including a pair of variable displacement pressure and flow compensated motors each connected to individual wheels; the auxiliary drive utilizes a pressure compensated pump source of the existing hydraulic system on the vehicle. The primary accessories run by said pump maintain a priority flow over the auxiliary drive motors since the pressure compensating level of the motors is set slightly below that of the pump.
    Type: Grant
    Filed: November 22, 1974
    Date of Patent: October 12, 1976
    Assignee: The Cessna Aircraft Company
    Inventor: Loren L. Alderson
  • Patent number: 3979908
    Abstract: A priority valve utilized in a pressure and flow compensated variable displacement system which supplies priority flow to a priority motor and secondary flow to a secondary motor as long as the priority flow requirements are satisfied or the priority flow path is blocked. The priority valve utilizes the same flow control signal as the system pump including a fixed restriction in the signal line and a relief valve downstream of said restriction, set at a level below the maximum pressure level of the system so that when the priority motor is stopped, flow continues to the secondary motor.
    Type: Grant
    Filed: September 29, 1975
    Date of Patent: September 14, 1976
    Assignee: The Cessna Aircraft Company
    Inventor: Loren L. Alderson