Patents by Inventor Giridhari Agrawal

Giridhari Agrawal 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).

  • Publication number: 20080012237
    Abstract: An improved and enhanced dynamic seal for use in high-speed turbomachinery includes an inner ring coupled to an outer sleeve. The coupling between the inner ring and the outer sleeve is strengthened by forming an increased surface area, exhibited by recesses, in at least one of the outer surface of the inner ring and the inner surface of the outer sleeve, and by providing an adhesive material in the recesses to bond the inner ring to the outer sleeve. Additionally, the coupling can be further strengthened by providing complementary projections on at least one of the outer surface of the inner ring and the inner surface of the outer sleeve to fit into the recesses.
    Type: Application
    Filed: July 16, 2007
    Publication date: January 17, 2008
    Applicant: R & D Dynamics Corporation
    Inventor: Giridhari Agrawal
  • Publication number: 20050189720
    Abstract: An improved and enhanced dynamic seal for use in high-speed turbomachinery includes an inner ring coupled to an outer sleeve. The coupling between the inner ring and the outer sleeve is strengthened by forming an increased surface area, exhibited by recesses, in at least one of the outer surface of the inner ring and the inner surface of the outer sleeve, and by providing an adhesive material in the recesses to bond the inner ring to the outer sleeve.
    Type: Application
    Filed: February 24, 2005
    Publication date: September 1, 2005
    Applicant: R & D Dynamics Corporation
    Inventor: Giridhari Agrawal
  • Publication number: 20050185865
    Abstract: An improved and enhanced hydrodynamic fluid film bearing for rotatably supporting a shaft journal is provided and includes a stationary retaining member, at least two generally cylindrical foil elements attached to one another and forming an anti-rotation fin, and a generally cylindrical resilient backing member. The retaining member has an inner surface defining a cylindrical opening for receiving a shaft journal. The inner surface also includes a longitudinally extending slot in which the anti-rotation fin formed by the foil elements is mounted so that the foil elements line at least a portion of the cylindrical opening. The resilient member is also disposed within the cylindrical opening generally concentric to and radially outward from the foil elements. The foil elements may be discrete elements attached together to form the anti-rotation fin, or alternatively formed from a single foil with a bend defining the anti-rotation fin.
    Type: Application
    Filed: February 19, 2004
    Publication date: August 25, 2005
    Applicant: R & D Dynamics Corporation
    Inventor: Giridhari Agrawal
  • Publication number: 20050147335
    Abstract: A stacked foil thrust bearing assembly provides a compact, lightweight, high load capacity, high temperature, oil-free foil thrust bearing for use in high speed rotating machinery. A stacked foil thrust bearing assembly comprises a plurality of thrust runners in adjacently spaced and parallel relationship. Each thrust runner includes an annular-shaped portion having generally opposite axial sides, and a thrust bearing positioned on each of the generally opposite axial sides. Each thrust bearing includes a thrust bearing plate and a spring plate operatively engaging the thrust bearing plate. A plurality of foils are circumaxially dispersed about one axial side of the thrust bearing plates. A plurality of springs are circumaxially dispersed about one axial side of the spring bearing plates.
    Type: Application
    Filed: June 27, 2003
    Publication date: July 7, 2005
    Applicant: R & D Dynamics Corporation
    Inventor: Giridhari Agrawal