Patents by Inventor Robert S. Michaels

Robert S. Michaels 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: 8505577
    Abstract: Regulated pneumatic gas is supplied through a gas supply tube (14) which is welded to a pilot valve housing (18) which accommodates a solenoid valve (16). When the solenoid valve is electrically activated and opened, the pneumatic gas flows through a bifurcated channel (22) which is welded to the pilot valve housing and to a fuel valve mechanism (24A) and to an oxidizer valve mechanism (24B). The force of the pneumatic gas causes pistons (38A, 38B) to actuate respective poppets (36A, 36B). Movement of the poppets results in the dispensing of fuel propellant from a fuel outlet chamber (44A) and the dispensing of oxidizer from an oxidizer outlet chamber (44B). The fuel valve mechanism and oxidizer valve mechanism are positioned and oriented such that the exiting fuel and oxidizer are mixed in a vortex rocket engine.
    Type: Grant
    Filed: November 30, 2010
    Date of Patent: August 13, 2013
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventors: Daryoush M. Salehi, Roger P. Berry, Nathan P. Mathis, Robert S. Michaels
  • Patent number: 7284487
    Abstract: Stereolithography is used to fabricate directly a single-piece, missile-usable, accurate, flightweight igniter without the use of intermediate, non-operational molds or prototypes in the fabrication process. The same prototype-less, direct stereolithography can be used to produce other missile-usable parts by designing each such part to be of a single-piece configuration and by using material that is suitable for both stereolithography and functional missile application.
    Type: Grant
    Filed: July 6, 2004
    Date of Patent: October 23, 2007
    Assignee: United States of America as represented by the Secretary of the Army
    Inventors: Robert W. Milton, Mark W. Kirkham, Robert S. Michaels, Jon A. Freeman, Bryce D. Brubaker
  • Patent number: 7257939
    Abstract: Sliding-Action Magneto-Mechanical Injector Throttling Device (SLAMMIT) provides on-demand, yet accurate, throttling of the mass flow of the fuel and/or oxidizer into the combustion chamber of a vortex injector. At least two SLAMMIT sub-assemblies comprise the SLAMMIT Device and each sub-assembly is integrated into a manifold and is driven to slide in a given direction by a drive block that is internal to the sub-assembly. The drive block is, in turn, actuated by an electromagnet that is external to the SLAMMIT sub-assembly. As the SLAMMIT sub-assemblies slide, flappers inside the sub-assemblies achieve the effective opening size of the injection orifices anywhere between fully open and fully closed.
    Type: Grant
    Filed: August 15, 2003
    Date of Patent: August 21, 2007
    Assignee: United States of America as represented by the Secretary of the Army
    Inventors: Robert S. Michaels, Jerrold H. Arszman
  • Patent number: 6086853
    Abstract: This invention is a composition of matter and method of preparing the same. More specifically the present invention is a medicated vapor candle consisting of a homogenous mixture having approximately three parts petroleum jelly containing the active ingredients of camphor, menthol and eucalyptus, melted and mixed with four parts candle wax. The active ingredients, by volume, of approximately 5% camphor, 2.5% menthol and 1.2% eucalyptus oil.
    Type: Grant
    Filed: January 25, 1999
    Date of Patent: July 11, 2000
    Inventor: Robert S. Michaels
  • Patent number: 5622046
    Abstract: Current state-of-the art injection methodologies for bipropellant engines ly on either impingement or turbulence to mix the fuel and oxidizer streams. The multiple impinging stream vortex injector combines both mixing schemes into a single injector. Both first stage mixing at point of impingement and second stage mixing or turbulent vortex mixing is accomplished by impinging momentum balanced, tangentially injected propellant streams onto one another. The impingement angles are calculated to yield a resultant stream vector that consists of only a tangential velocity component. The two stages of mixing results in increased engine performance and combustion efficiency.
    Type: Grant
    Filed: August 28, 1995
    Date of Patent: April 22, 1997
    Assignee: The United States of America as represented by the Secretary of the Army
    Inventors: Robert S. Michaels, Ben F. Wilson
  • Patent number: 5613734
    Abstract: The present invention entails a chair having a back movable between an upper operative position and a lower or retracted stowed position. The chair includes a base frame having a seat and a catch rail disposed below the seat. A retainer is spaced above the catch rail and there is defined a throughway between the catch rail and the retainer. A back is provided and is movable relative to the base frame. In the upper operative position the back engages and is supported by the catch rail while the retainer prevents the back from rotating past a predetermined position. In the lower retracted position, the back is disengaged from the catch rail and extends below the catch rail.
    Type: Grant
    Filed: February 8, 1996
    Date of Patent: March 25, 1997
    Assignee: Bassett Furniture Ind. Inc.
    Inventors: Robert S. Michael, Joe E. Miller, David P. Zagaroli