Patents by Inventor Alan W. Myers

Alan W. Myers 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: 11040771
    Abstract: A rotor hub is presented that uses a low profile and frontal area design that reduces drag and combines the advantages of utilizing a virtual flapping hinge and a soft in-plane rotor hub.
    Type: Grant
    Filed: May 8, 2019
    Date of Patent: June 22, 2021
    Assignee: AVX AIRCRAFT COMPANY
    Inventors: Alan W. Myers, John D. Busch
  • Publication number: 20190344884
    Abstract: A rotor hub is presented that uses a low profile and frontal area design that reduces drag and combines the advantages of utilizing a virtual flapping hinge and a soft in-plane rotor hub.
    Type: Application
    Filed: May 8, 2019
    Publication date: November 14, 2019
    Inventors: Alan W. Myers, John D. Busch
  • Patent number: 4362281
    Abstract: A mounting for a helicopter pylon having a plurality of resilient vertical support links (24-27) between the pylon (12) and the helicopter fuselage (13). The links have a composite spring rate for a given pylon weight which establishes a resilient support for the fuselage from the pylon at the thrust required to support said fuselage in normal flight and in which oscillatory vertical force transmitted to fuselage is minimal for acceptable static deflections of the pylon.Physical stops (24e, 24n, 24p) are operable to limit deflection between the pylon (12) and the fuselage (13) at predetermined rotor thrust above and below said normal thrust.Links (24-27) are mounted at the ends of a pair of rigid beams (20, 21 and 22, 23) which are secured at the centers thereof to opposite sides of transmission portion of the pylon (12).A vertical rigid mounting pin (24b) extends downward at the end of each beam.
    Type: Grant
    Filed: February 26, 1981
    Date of Patent: December 7, 1982
    Assignee: Textron, Inc.
    Inventors: Wesley L. Cresap, Alan W. Myers, Sathy P. Viswanathan
  • Patent number: 4270711
    Abstract: A helicopter landing gear assembly includes a pair of crosstubes (20, 22) having a pair of struts (28, 30) connected at the outboard ends thereof. A first of the crosstubes (22) is connected to the helicopter fuselage (16) at a pair of laterally spaced points (24, 26). The second of the crosstubes (20) is joined by a pivot connection (32) to a structural bridge (10) positioned above the second crosstube. The structural bridge (10) is connected at its outer ends to the fuselage main beams (12, 14). The structural bridge (10) connected to the second crosstube (20) permits the helicopter fuselage (16) to pivot about a fore-aft axis thereof to lower the natural roll frequency of the helicopter airframe and therefore increase the margin of stability to prevent ground resonance.
    Type: Grant
    Filed: January 29, 1979
    Date of Patent: June 2, 1981
    Assignee: Textron, Inc.
    Inventors: Wesley L. Cresap, Alan W. Myers
  • Patent number: D357894
    Type: Grant
    Filed: September 20, 1993
    Date of Patent: May 2, 1995
    Assignee: Bell Helicopter Textron Inc.
    Inventors: George E. Arnold, Dennis E. Gregory, Robert G. Anderson, Alan W. Myers