Patents by Inventor Malcolm H. Knapp

Malcolm H. Knapp 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: 4872767
    Abstract: The invention comprises a compact support for a bearing associated with a rotating member such as a shaft of a gas turbine engine. The bearing support has one or more circumferential leaf spring elements which provide radially resilient support for the shaft while being axially stiff to reduce axial thrust movement of the shaft. The spring rate of the support is designed to shift engine vibratory resonances so that they occur outside the normal speed range of the engine; and the support may include internal damping to minimize resonant vibratory peaks. Various bearing support embodiments are also disclosed.
    Type: Grant
    Filed: April 3, 1985
    Date of Patent: October 10, 1989
    Assignee: General Electric Company
    Inventor: Malcolm H. Knapp
  • Patent number: 4796721
    Abstract: A system used in a vehicle having a ground-engaging attitude to effect the displacement from a compartment in the vehicle of a power pack adapted for driving the vehicle. The system elevates the power pack from a vehicle driving position within the compartment toward another position disposed exteriorly of the compartment and maintains the power pack at the same attitude as the ground-engaging attitude of the vehicle upon the elevation of the power pack. The system senses attitude variations of the power pack upon its displacement, and is actuated in response to the attitude variation for controlling operation of the displacement and maintaining functions.
    Type: Grant
    Filed: July 6, 1987
    Date of Patent: January 10, 1989
    Assignee: General Electric Company
    Inventors: Malcolm H. Knapp, Gerhard Sonder
  • Patent number: 4329114
    Abstract: An axial compressor is provided with a cooling air manifold surrounding a portion of the shroud, and means for bleeding air from the compressor to the manifold for selectively flowing it in a modulating manner axially along the outer side of the stator/shroud to cool and shrink it during steady-state operating conditions so as to obtain minimum shroud/rotor clearance conditions. Provision is also made to selectively divert the flow of cooling air from the manifold during transient periods of operation so as to alter the thermal growth or shrink rate of the stator/shroud and result in adequate clearance with the compressor rotor.
    Type: Grant
    Filed: July 25, 1979
    Date of Patent: May 11, 1982
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Richard P. Johnston, Malcolm H. Knapp, Charles E. Coulson
  • Patent number: 4111821
    Abstract: Lubricant compositions for use in the cylinder and drive train lubrication of reciprocating compressors for oxygen-free gases comprise 97% to 99% by weight of a base fluid that is a phthalate ester of an aliphatic alcohol having 10 to 15 carbon atoms and 1% to 3% by weight of an additive system that contains a viscosity index modifying component, an antioxidant component, and optionally a corrosion inhibitor and/or a load bearing additive.
    Type: Grant
    Filed: July 8, 1975
    Date of Patent: September 5, 1978
    Assignee: Tenneco Chemicals, Inc.
    Inventors: Allan K. Lazarus, Malcolm H. Knapp