Patents by Inventor Bret D. Pica

Bret D. Pica 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: 20230415919
    Abstract: An improved passenger boarding bridge comprises a proximal section such as a rotunda which is connectable to a doored exit of an airport concourse, a distal section such as a cab adapted to dock with a parked aircraft, and at least one tunnel section interposed therebetween. A plurality seals are associated with the various sections and their junctures to extend an environmental envelope of the airport concourse to the parked aircraft. For example, a first plurality of seals may be provided for sealing a juncture of the rotunda section and the tunnel section, and a second plurality of seals may be provided for sealing a juncture of the cab section and the tunnel section. Seals are also associated with each of the rotunda and cab sections.
    Type: Application
    Filed: June 23, 2023
    Publication date: December 28, 2023
    Inventor: Bret D. Pica
  • Patent number: 6845941
    Abstract: A rotor system that allows an aircraft to operate as a helicopter and as an airplane is disclosed. The invention incorporates an annular airfoil attached at the tips of the rotor blades. The rotor system stops and is secured from rotation for operation at high forward speeds. The annulus acts as the primary lifting surface in airplane mode at high speed. The rotor blades incorporate leading and trailing edge flaps for control in transitional and fixed wing flight modes.
    Type: Grant
    Filed: June 4, 2003
    Date of Patent: January 25, 2005
    Inventor: Bret D. Pica
  • Publication number: 20040113013
    Abstract: A rotor system that allows an aircraft to operate as a helicopter and as an airplane is disclosed. The invention incorporates an annular airfoil attached at the tips of the rotor blades. The rotor system stops and is secured from rotation for operation at high forward speeds. The annulus acts as the primary lifting surface in airplane mode at high speed. The rotor blades incorporate leading and trailing edge flaps for control in transitional and fixed wing flight modes.
    Type: Application
    Filed: June 4, 2003
    Publication date: June 17, 2004
    Inventor: Bret D. Pica