Patents Represented by Attorney, Agent or Law Firm Marguerite O. Dineen, Esq.
  • Patent number: 6817299
    Abstract: A fragmenting projectile includes a multi-wall projectile casing with each wall thereof formed by a sleeve. Each pair of adjacent sleeves is defined by inner and outer sleeves that mate in a threaded engagement. Explosive material is disposed in an innermost sleeve.
    Type: Grant
    Filed: December 10, 2003
    Date of Patent: November 16, 2004
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: David P. Cooke
  • Patent number: 6811587
    Abstract: A biological hazard mitigation apparatus permitting a material handling operation in the vicinity of a work area includes a plenum pneumatically coupled and proximate to one side of the work area, a filter sized to trap biological hazards and including an exhaust port, a blower including an inlet port and an exhaust port, and ducting pneumatically coupling the exhaust port of the filter to the inlet port of the blower, wherein the filter is disposed in the plenum, and adjacent surfaces of the filter and the plenum are substantially equal in surface area. If desired, the ducting includes first and second ducts, permitting a silencer to be disposed between the first and second ducts. Methods for operating the apparatus are also described.
    Type: Grant
    Filed: November 18, 2002
    Date of Patent: November 2, 2004
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Richard A Lorey, Michael A Pompeii, Dale W Sisson, William E. Blakley, II
  • Patent number: 6776369
    Abstract: Guidance of a gliding vehicle is disclosed. A method of the invention allows the range of the glide phase of a gliding vehicle to be maximized, while satisfying final flight path angle and aimpoint requirements. The method controls the time-of-flight of the gliding value to a desired value. The time-of-flight control can correct for winds, off-nominal launch conditions, and rocket motor variations, among other factors. Both time-of-flight control and range and cross-range maximization can be achieved by the inventive method, utilizing a compact closed-loop approach.
    Type: Grant
    Filed: November 14, 2003
    Date of Patent: August 17, 2004
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Craig A. Phillips, David S. Malyevac