Patents by Inventor Jack D. Wright

Jack D. Wright 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: 5313788
    Abstract: A thrust reverser for a long duct mixed flow fan jet engine having a nacelle formed by a fixed forward structure surrounding the fan, a rear fixed structure and a translatable inner and outer cowl therebetween, the nacelle surrounds the engine and forms a long by-pass duct therewith, a common actuator fixed to the translatable cowls to simultaneously displace them over the rear structure, blocker doors coupled to the inner translating cowls for deployment during thrust reversal into the by-pass duct into a blocking position to divert the airflow through the cascades placed into an opening uncovered when the translatable cowls are axially displaced.
    Type: Grant
    Filed: March 26, 1993
    Date of Patent: May 24, 1994
    Assignee: General Electric Company
    Inventors: Jack D. Wright, Joe E. Ellis
  • Patent number: 5000399
    Abstract: An annular nacelle for a turbine engine of an aircraft has a variable contour annular air inlet. The variable contour annular inlet includes annular outer and inner surface-defining radially-spaced structures on the forward portion of the nacelle, an annular member disposed between the annular outer and inner structures and coupled to the annular outer structure for sliding movement along the interiors of the annular outer and inner structures, and a plurality of actuating mechanisms coupled between the nacelle body and the annular member. The actuating mechanisms are operable for moving the annular member between forward and rearward positions.
    Type: Grant
    Filed: February 23, 1990
    Date of Patent: March 19, 1991
    Assignee: General Electric Company
    Inventors: Jack L. Readnour, Jack D. Wright
  • Patent number: 4335573
    Abstract: An afterburning turbofan engine includes amixer for mixing the engine generated hot gas and fan streams prior to discharge through the engine nozzle. The mixer includes a fixed upstream portion and a movable downstream portion which may be indexed to selectively interchange flow communication between the chutes of the two portions to effect a temperature reduction in the downstream mixer portion and, hence, a reduction in infrared radiation.
    Type: Grant
    Filed: September 2, 1970
    Date of Patent: June 22, 1982
    Assignee: General Electric Company
    Inventor: Jack D. Wright
  • Patent number: 4275560
    Abstract: The angle of the variable blocker door vanes in the bypass duct of a turbofan engine is varied in response to the angle of the variable compressor vanes of the engine. A cam and linkage assembly interconnect the blocker doors with the actuation system of the variable stator vanes such that as the angle of the stator vanes is modulated through a first predetermined range, the angle of the blocker doors is modulated through a second predetermined range.
    Type: Grant
    Filed: December 27, 1978
    Date of Patent: June 30, 1981
    Assignee: General Electric Company
    Inventors: Jack D. Wright, Barton H. Snow
  • Patent number: D286880
    Type: Grant
    Filed: March 5, 1984
    Date of Patent: November 25, 1986
    Assignee: General Electric Company
    Inventors: Leroy H. Smith, Jr., Ambrose A. Hauser, William C. Ruehr, Alan R. Stuart, Jack D. Wright