Patents by Inventor Neil J. Dubois

Neil J. Dubois 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: 5821418
    Abstract: The present invention relates to a cooled fixture for high temperature acerometer measurement. The fixture includes a collar mounted to a pipe and a block mounted to the collar to which one or more accelerometers may be connected. The block is provided with a cooling system for controlling the temperature of the accelerometer(s) mounted to the block and maintaining the temperature at a level at which the accelerometers will survive.
    Type: Grant
    Filed: April 28, 1996
    Date of Patent: October 13, 1998
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Neil J. Dubois
  • Patent number: 5632218
    Abstract: A debris deflector protects an underwater vehicle's control. surface while ntroducing little or no flow disturbance around the control surface. The deflector extends outward from the vehicle to peninsulate the control surface. The deflector's cross-section is defined by a wedge shape subtended by an arc with the apex of the wedge shape always pointing towards the control surface.
    Type: Grant
    Filed: August 5, 1996
    Date of Patent: May 27, 1997
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: John J. Vaillancourt, Neil J. Dubois, Stacy J. Hills
  • Patent number: 5396855
    Abstract: There is presented an underwater vehicle tailcone assembly including a ford flange, a first tubular sheath extending rearwardly from the forward flange, and elastomer material bonded to inner and outer surfaces of the first sheath to form a forward chamber wall. The assembly further includes an aft flange, a second tubular sheath extending forwardly from the aft flange, and elastomer material bonded to inner and outer surfaces of the second sheath to form an aft chamber wall. The assembly still further includes a rigid housing wall disposed between a rearward end of the forward chamber wall and a forward end of the aft chamber wall. The forward chamber wall, the housing wall, and the aft chamber wall form a continuous tailcone wall from a forward edge of the forward flange to a rearward edge of the aft flange.
    Type: Grant
    Filed: June 30, 1994
    Date of Patent: March 14, 1995
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Neil J. DuBois
  • Patent number: 5333570
    Abstract: The present invention relates to a damped actuator linkage for use on an erwater vehicle. The linkage includes a first linkage member connected to an actuator for providing a torsional force, a second linkage member connected to a utility device, and a layer of non-metallic material interposed between the first and second linkage members to reduce the transmission of noise and the attenuation of vibrations. The non-metallic material layer may be a layer of polyurethane material or a layer of silicone compound. This layer is preferably cast in concentric arrangement between the two linkage members.
    Type: Grant
    Filed: May 18, 1992
    Date of Patent: August 2, 1994
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Neil J. DuBois, Stanley J. Polhemus
  • Patent number: 5158030
    Abstract: A damped flexible seal assembly for a torpedo isolates the tailcone thereof rom vibrational energy present in the drive shaft assembly. A pair of outside flanges, each of which include an inwardly facing groove and an O-ring constrained therein, provide a watertight seal against the outer non-rotating surface of the drive shaft assembly. An inside flange includes an outwardly-facing groove and an O-ring constrained therein, and provides a watertight seal against the inner surface of the tail cone. Two cast-in-place elastomeric seals provide a watertight seal between the flanges and further provide a damping barrier between the outside flanges and the inside flanges for damping vibrational energy present in the drive shaft assembly before the energy can reach the tailcone through the seal assembly.
    Type: Grant
    Filed: March 22, 1992
    Date of Patent: October 27, 1992
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Neil J. DuBois, Antonio M. Amaral
  • Patent number: 5154788
    Abstract: A continuous filament is selected from among a group of appropriate types of filaments, and selection of the filament length and the filament thickness is made as well. A matrix material is selected from a group of appropriate types of matrix materials. Filaments of the selected type, length and thickness are undirectionally imbedded in the selected matrix to provide a uniaxial continuously reinforced composite. The Young's modulus, E.sub.c, and the shear modulus G.sub.c, are calculated for the composite. Mathematical formulas are provided for calculation of upper and lower bounds of transverse stiffness, B. A mathematical formula is provided for calculation of critical comprehensive stress, P.sub.c. Transverse stiffness, B, is involved as one of the factors in this formula. Either one or the other of the upper bound of B or the lower bound of B are alternatively applied in calculating P.sub.
    Type: Grant
    Filed: July 3, 1991
    Date of Patent: October 13, 1992
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventors: Francis C. Spicola, Neil J. Dubois
  • Patent number: 5040764
    Abstract: A mounting assembly for absorbing low frequency vibrational energy as proed by a source and isolating a base member therefrom, the mounting assembly including a central metallic ring, non-metallic foam rings located on both sides of the central metallic ring in concentric relation with respect thereto, and inner and outer metallic ring members engaging said foam rings in concentric relation, the foam rings defining a spongy mass that effectively absorbs the low frequency vibrational energy emanating from the source.
    Type: Grant
    Filed: September 28, 1990
    Date of Patent: August 20, 1991
    Assignee: The United States of America as represented by the Secretary of the Navy
    Inventor: Neil J. Dubois