Patents by Inventor Martin Corney

Martin Corney 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: 5485788
    Abstract: A system (10) for detonating an electro-explosive device (EED) (46) includes a primer (40, 70) connected to an expansion chamber (36) by a shaped vent passage (38). A releasably retained element (60) within the expansion chamber (36) is propelled by expanding gas from the detonated primer to impact a piezoelectric crystal (48) in circuit with the EED (46). Particular safety arrangements are disclosed which prevent the application of voltage from the crystal to the EED until the system is intentionally activated. Some of these arrangements also prevent electromagnetic interference and stray field voltages from reaching the EED.
    Type: Grant
    Filed: September 27, 1994
    Date of Patent: January 23, 1996
    Assignee: Hughes Missile Systems Company
    Inventor: Martin Corney
  • Patent number: 5329840
    Abstract: A system for controlling the application of firing signals to electrically fired ammunition rounds which are chambered in the gun or the like. A plurality of insulated contacts are installed in the firing chamber wall so as to connect electrically to mating insulated contacts which are built into the case of the chambered round. Various configurations of annular contact rings are provided for both the inner surface of a gun firing chamber and for the mating exterior surface of a cartridge to be positioned therein. Timing control circuitry for such systems is also disclosed, suitable for use in a single barrel gun or a multiple barrel gun of the Gatling type or a revolving chamber gun with one or more fixed barrels.
    Type: Grant
    Filed: June 22, 1993
    Date of Patent: July 19, 1994
    Assignee: Hughes Missile Systems Company
    Inventor: Martin Corney
  • Patent number: 5247867
    Abstract: A velocity tailoring system for a defensive automatic gun having controllable muzzle velocity capability. The system includes velocity determination and control apparatus for determining the projectile discharge velocity necessary to achieve an effective target impact velocity that is less than a predetermined projectile shatter velocity. The projectile discharge velocity control signal is provided to the defensive automatic gun system.
    Type: Grant
    Filed: January 16, 1992
    Date of Patent: September 28, 1993
    Assignee: Hughes Missile Systems Company
    Inventor: Martin Corney
  • Patent number: 5235129
    Abstract: A system for controlling the application of firing signals to electrically fired ammunition rounds which are chambered in the gun or the like. A plurality of insulated contacts are installed in the firing chamber wall so as to connect electrically to mating insulated contacts which are built into the case of the chambered round. Various configurations of annular contact rings are provided for both the inner surface of a gun firing chamber and for the mating exterior surface of a cartridge to be positioned therein. Timing control circuitry for such systems is also disclosed, suitable for use in a single barrel gun or a multiple barrel gun of the Gatling type or a revolving chamber gun with one or more fixed barrels.
    Type: Grant
    Filed: November 1, 1991
    Date of Patent: August 10, 1993
    Assignee: Hughes Aircraft Company
    Inventor: Martin Corney
  • Patent number: 4000698
    Abstract: A unique sabot for a sub-caliber or otherwise unusually configured projectile, the sabot being designed to have regions which, under the pressures automatically applied to one or more surfaces of the sabot during the launching of the projectile, fail, causing fracturing of the sabot and separation of the sabot pieces from the projectile within a short distance from the end of the launching device. Particular structure including a frangible sabot body with separation slots shaped to concentrate stresses in the body, and external pressure elements aligned with the slots are provided to achieve the desired end. Immediate break-up of the sabot at the end of the launching means, such as a gun barrel, assures a short area of danger from the sabot fragments in the launching area.
    Type: Grant
    Filed: October 29, 1974
    Date of Patent: January 4, 1977
    Assignee: General Dynamics Corporation Pomona Division
    Inventor: Martin Corney