Patents by Inventor Joseph Lippert, Jr.

Joseph Lippert, Jr. 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: 4180372
    Abstract: A spring-loaded pivoting end plate that is hinged such that it is deployed by centrifugal force into the airstream to thereby act as an aerodynamic brake for wind turbines in overspeed conditions. The brake has a stationary portion fixed on the tip of the turbine rotor and a pivoting portion hinged for movement with respect to the fixed portion. The longitudinal centerline of the brake coincides with the chord line of the turbine blade and the pivoting movement is about a hinge axis that is normal to the rotational plane of the turbine. The planform of the brake has a low aspect ratio shape with the ratio of the fore and aft chordwise length to the width being one or greater. The edges of the brake in the normal running condition extend beyond the contour of the turbine blade to serve as an end plate such that the aerodynamic efficiency of the blade is improved thereby.
    Type: Grant
    Filed: March 2, 1977
    Date of Patent: December 25, 1979
    Assignee: Grumman Corporation
    Inventor: Joseph Lippert, Jr.
  • Patent number: 3960345
    Abstract: A strake, or strakes, or faired simulation of same, mounted on a typical engine nacelle or similar wing mounted body to reduce or prevent the formation of vortices usually occurring with nacelle-wing combinations to improve the lift and drag characteristics of the combination and improve the stability of the aircraft since the undesireable variations of downwash changes over the tail surfaces are reduced or eliminated.
    Type: Grant
    Filed: May 16, 1975
    Date of Patent: June 1, 1976
    Assignee: Grumman Aerospace Corporation
    Inventor: Joseph Lippert, Jr.