Patents by Inventor Stephen L. Rodgers

Stephen L. Rodgers 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: 7217683
    Abstract: Nanoscale chemicals based on polyhedral oligomeric silsesquioxanes (POSS) and polyhedral oligomeric silicates (POS) are taught as lubricants, mold release agents, and as additives to control the viscosity, lubrication, wear, and thermal properties of conventional lubricous materials. The precisely defined nanoscopic dimensions of POSS materials enable viscosity, miscibility, and thermal properties to be (increased) or reduced (decreased) as desired. A key feature to the successful tailoring of properties is the inherent thermal and chemical stability of the POSS/POS nanostructure and the ability to control its topology and chemical potential to match that of surfaces and other materials.
    Type: Grant
    Filed: September 5, 2002
    Date of Patent: May 15, 2007
    Inventors: Rusty L. Blanski, Shawn H. Phillips, Stephen L. Rodgers, Joseph D. Lichtenhan, Joseph J. Schwab
  • Patent number: 6180799
    Abstract: Provided are novel methods for preparing pentaerythritol disulfite employing reduced amounts of thionyl chloride and 1,2-dichloroethane as reaction media. Also disclosed is the first synthesis of pentaerythritol disulfate by oxydation of the above pentaerythritol disulfite. Both the disulfite (2) and the disulfate (3) are obtained in high yields.
    Type: Grant
    Filed: May 1, 2000
    Date of Patent: January 30, 2001
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Suresh C. Suri, Stephen L. Rodgers
  • Patent number: 5616882
    Abstract: A rocket propellant of improved Isp and thrust is provided by modifying a rocket fuel of RP-1 (a kerosene fraction). Such fuel is combined with an oxidizer (e.g. liquid oxygen, LOX) which defines a rocket propellant of the prior art. Such propellant is modified per the invention by addition to or replacement of, the RP-1 with quadricyclane. In another embodiment, quadricyclane is added to n-Hexane as a fuel composition which is then combined with an oxidizer to define a rocket propellant per the invention. The invention thus provides a number of rocket fuels which upon combination with an oxidizer, provides a high energy density propellant, which can permit increases of over 10 wt % in additional payload for rocket launch vehicles.
    Type: Grant
    Filed: March 29, 1996
    Date of Patent: April 1, 1997
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Robert Nichols, Timothy A. McKelvey, Stephen L. Rodgers