Patents by Inventor William P. Fallon

William P. Fallon 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: 20260109086
    Abstract: A method of forming a bonded structure is disclosed herein. In some embodiments, a method includes curing a first part on a first tool to a first degree of cure, the first degree of cure (DOC) being a partially cured state, removing the partially cured first part from the first tool, assembling the partially cured first part and a second part into a structure, and curing the structure to form a bonded structure, where the partially cured first part is cured to a second degree of cure (DOC) that is greater than the first DOC.
    Type: Application
    Filed: October 21, 2024
    Publication date: April 23, 2026
    Inventors: Felix Nhanchau Nguyen, Yin-Farn Chen, William P. Fallon, Robert Warner Koon
  • Patent number: 9903034
    Abstract: A method of depositing aluminum onto a substrate is disclosed. In this method, the substrate is disposed as cathode in an electrochemical cell with an anode and a liquid electrodeposition composition comprising an ionic liquid and a source of aluminum, and aluminum is electroplated onto the substrate. Residual water content in the electroplating bath is controlled by exposure to light in the presence of a photo-oxidation catalyst to decompose the water or species associated with water.
    Type: Grant
    Filed: November 22, 2013
    Date of Patent: February 27, 2018
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Lei Chen, Xiaomei Yu, William P. Fallon
  • Publication number: 20150144495
    Abstract: A method of depositing aluminum onto a substrate is disclosed. In this method, the substrate is disposed as cathode in an electrochemical cell with an anode and a liquid electrodeposition composition comprising an ionic liquid and a source of aluminum, and aluminum is electroplated onto the substrate. Residual water content in the electroplating bath is controlled by exposure to light in the presence of a photo-oxidation catalyst to decompose the water or species associated with water.
    Type: Application
    Filed: November 22, 2013
    Publication date: May 28, 2015
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Lei Chen, Xiaomei Yu, William P. Fallon
  • Patent number: 6578793
    Abstract: A variable diameter rotor blade assembly includes a rotor hub with multiple rotor blades each having an outboard blade section telescopically mounted to an inboard blade section. A reeling assembly includes a strap drum that extends and retracts a strap attached to each of the outboard blade sections to selectively change the diameter of the rotor blade assembly. The strap includes a body portion extending toward the drum and a termination portion attached to each of the outboard blade sections. The termination portion is made from a rigid fiber reinforced composite that has a higher rigidity than the body portion. A transition region is formed between the body portion and the termination portion and is made from a flexible matrix-fiber composite that has a higher rigidity than the body portion and a lower rigidity than the rigid fiber reinforced composite.
    Type: Grant
    Filed: February 13, 2001
    Date of Patent: June 17, 2003
    Assignee: Sikorsky Aircraft Corporation
    Inventors: Francis E. Byrnes, William P. Fallon
  • Publication number: 20020109042
    Abstract: A variable diameter rotor blade assembly includes a rotor hub with multiple rotor blades each having an outboard blade section telescopically mounted to an inboard blade section. A reeling assembly includes a strap drum that extends and retracts a strap attached to each of the outboard blade sections to selectively change the diameter of the rotor blade assembly. The strap includes a body portion extending toward the drum and a termination portion attached to each of the outboard blade sections. The termination portion is made from a rigid fiber reinforced composite that has a higher rigidity than the body portion. A transition region is formed between the body portion and the termination portion and is made from a flexible matrix-fiber composite that has a higher rigidity than the body portion and a lower rigidity than the rigid fiber reinforced composite.
    Type: Application
    Filed: February 13, 2001
    Publication date: August 15, 2002
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Francis E. Byrnes, William P. Fallon