Patents Represented by Attorney Mellor A. Gill
  • Patent number: 4086913
    Abstract: A solar heat collector having an array of liquid transporting tubes and a plurality of heat absorber panels joined by a tube gripping accommodation on each panel providing structural integrity and good thermal conductivity.
    Type: Grant
    Filed: December 15, 1976
    Date of Patent: May 2, 1978
    Assignee: Grumman Aerospace Corporation
    Inventor: Joseph G. Gavin
  • Patent number: 4085911
    Abstract: A vertical takeoff and landing aircraft having a tail assembly supporting structure which is pivotally connected to the fuselage, and having a shrouded fan driven by an engine submerged in the fuselage, the shrouded fan being connected to and rotatable with the tail supporting structure so as to direct the slipstream of the shrouded fan over the tail assembly at all times.
    Type: Grant
    Filed: May 23, 1977
    Date of Patent: April 25, 1978
    Assignee: Grumman Aerospace Corporation
    Inventor: Richard J. Nahodyl
  • Patent number: 4081023
    Abstract: A heat pipe to remove heat from a light fixture in a room of a building that will transfer the fixture heat to a system in a building that will in turn reject or use the fixture heat in a heating, ventilating, air conditioning system for the building.
    Type: Grant
    Filed: November 26, 1976
    Date of Patent: March 28, 1978
    Assignee: Grumman Aerospace Corporation
    Inventors: Fred Edelstein, Robert A. Haslett, Odd E. Sangesland
  • Patent number: 4075500
    Abstract: A wind powered electrical generating system having a suitable shaped aerodynamic duct or shroud within which a wind turbine having a fixed pitch blade is mounted, as by means of a stator means at the inlet of the duct or shroud with the stator means including mechanism for varying their effective angle of attack with regard to the approaching wind so as to provide the desired swirling approach of the wind to the turbine therebehind in achieving the desired torque and speed of shafting from the turbine to generator driven by the turbine in maintaining constant phase and frequency of the electrical output wherein the duct or shroud is mounted by a tower or shaft that will permit the cocking of the structure into the wind.
    Type: Grant
    Filed: August 13, 1975
    Date of Patent: February 21, 1978
    Assignee: Grumman Aerospace Corporation
    Inventors: Richard A. Oman, Kenneth M. Foreman
  • Patent number: 4066882
    Abstract: A high-speed, real-time automatic test system element that is compatible with most contemporary computers and will interface with units under test via a front-mounted coaxial patch panel and rear exiting cables to mate with common automatic test system interconnection schemes whereby a language driver callable with programming statements enables dynamic digital testing of modern integrated circuit cards and chassis at their normal clock rates and provides a digital reading of GO/NO-GO test evaluations.
    Type: Grant
    Filed: August 16, 1976
    Date of Patent: January 3, 1978
    Assignee: Grumman Aerospace Corporation
    Inventor: Charles M. Esposito
  • Patent number: 4059346
    Abstract: A variable focus mirror comprising a uniform elastic disk having a mirror finish on one face thereof, which is urged against an annular fulcrum concentric with the disk by a uniform force applied at the rim of the disk. This force causes the flat disk to be flexed into a substantially spherical, nearly parabolic shape. The magnitude of the force applied controls the degree of flexure and hence the focal length of the spherical mirror. For laser beam focusing the materials are selected to be able to withstand the laser energy being reflected.
    Type: Grant
    Filed: June 30, 1976
    Date of Patent: November 22, 1977
    Assignee: Grumman Aerospace Corporation
    Inventors: Howard S. Levine, Robert Winter
  • Patent number: 4042835
    Abstract: A very low noise input charge coupled device employing switches to provide a voltage gain in all electrodes prior to or in conjunction with the transfer of the signal(s) into, for example, a shift register so as to insure a signal amplitude well above the noise level associated with the shift register of the charge coupled device.
    Type: Grant
    Filed: February 24, 1976
    Date of Patent: August 16, 1977
    Assignee: Grumman Aerospace Corporation
    Inventor: James T. Fulton
  • Patent number: 4030102
    Abstract: A supporting structure that deployed resembles a spoked wheel which is retractable into a compact volume by virtue of hinged rim and reelable spokes that is an efficient and stable structure for storing, deploying and supporting surfaces such as radar and communications antennas, shielding, earth sensing, solar cell arrays and solar energy reflectors.
    Type: Grant
    Filed: October 23, 1975
    Date of Patent: June 14, 1977
    Assignee: Grumman Aerospace Corporation
    Inventors: Richard Kaplan, Jack L. Schultz
  • Patent number: 4026628
    Abstract: An electrical connector having a deformable tubular shell between a cable and fitting manufactured by a process of magnetically deforming the shell at one end to the underlying cable and at the other end to the underlying fitting to provide a superior EMI and shielding integrity as well as a good water tight seal without the need of potting the connection or providing special seal elements.
    Type: Grant
    Filed: December 18, 1975
    Date of Patent: May 31, 1977
    Assignee: Grumman Aerospace Corporation
    Inventors: Morris V. Duffner, Alexander Mintz
  • Patent number: 4015586
    Abstract: A closed water/glycol solar heating system for preheating a fluid so as to reduce energy requirements in bringing said fluid up to a desired temperature and holding same, said system including a solar collector having a flexible dome.
    Type: Grant
    Filed: January 12, 1976
    Date of Patent: April 5, 1977
    Assignee: Grumman Aerospace Corporation
    Inventors: Henry J. Vroom, Warren Robert Bolle, Herbert Schneider, Burton Swerdling
  • Patent number: 4007616
    Abstract: A process of manufacture to produce low cost pressure vessels from a length of metal tubing by use of localized heat and/or axial tensile force to shrink the diameter of the tubing at selected locations of a predetermined starting length approximately one diameter long and many diameters apart to permit subsequent separation to form open-ended pressure vessels. Subsequent conventional swaging operations could thicken and reduce the end diameters so they can be threaded.
    Type: Grant
    Filed: November 6, 1975
    Date of Patent: February 15, 1977
    Assignee: Grumman Aerospace Corporation
    Inventor: Benjamin J. Aleck
  • Patent number: 3995168
    Abstract: A device for the outside display of the level and specific density of a liquid contained within a tank, particularly for inflammable liquids, characterized by a plurality of paired light pipes having optical interface means therebetween located at intervals within a support with electrical means operable by light energy from one of the pair of light pipes being conducted thereby due to a mismatch of the index of refraction caused by an absence of fuel at the area of the optical interface to provide a display of the fluid level and/or the density of the fluid within a tank.
    Type: Grant
    Filed: August 4, 1975
    Date of Patent: November 30, 1976
    Assignee: Grumman Aerospace Corporation
    Inventors: Frederick Neuscheler, John J. Connelly
  • Patent number: 3992773
    Abstract: An electrical connector having a deformable tubular shell between a cable and fitting manufactured by a process of magnetically deforming the shell at one end to the underlying cable and at the other end to the underlying fitting to provide a superior EMI and shielding integrity as well as a good water tight seal without the need of potting the connection or providing special seal elements.
    Type: Grant
    Filed: April 21, 1975
    Date of Patent: November 23, 1976
    Assignee: Grumman Aerospace Corporation
    Inventors: Morris V. Duffner, Alexander Mintz
  • Patent number: 3982696
    Abstract: A jet noise suppressor nozzle comprised of a plurality of chute flow dividers through which air passes to mix with the jet gases at the boundaries formed by the downstream ends of the chute and the terminal plane of the nozzle with a plate at the forward area of the chute inlets under which jet gases are exhausted so as to create the aforementioned flow by the Coanda effect on the boundary layer air around the nozzle over the plate.
    Type: Grant
    Filed: July 1, 1975
    Date of Patent: September 28, 1976
    Assignee: Grumman American Aviation Corporation
    Inventor: Walter R. Gordon