Patents by Inventor Clifton P. Breay

Clifton P. Breay 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: 20100003840
    Abstract: The present application is directed to dielectric isolators for use in aircraft fuel systems to control lightning induced current and allow dissipation of electrostatic charge. The dielectric isolators are configured to have a high enough impedance to limit lightning currents to low levels, but low enough impedance to allow electrostatic charge to dissipate without allowing buildup. Although the dielectric isolators may develop a potential difference across the dielectric length due to the effects of lightning currents and its inherent impedance, they are configured to withstand these induced voltages without dielectric breakdown or performance degradation. In one embodiment, the dielectric isolator includes a tube constructed of a composition including a thermoplastic organic polymer (e.g., PEEK) and carbon nanotubes, and a pair of couplings attached to opposing ends of the tube.
    Type: Application
    Filed: July 2, 2008
    Publication date: January 7, 2010
    Applicant: Eaton Corporation
    Inventors: Clifton P. Breay, Sara D. Pfannenstiel, Stephen C. Matthews, Edward W.S. Bryant
  • Publication number: 20100003438
    Abstract: A thermoplastic composite material, which includes a thermoplastic, organic polymer; and a plurality of carbon nanotubes, is provided. The thermoplastic composite material exhibits a bulk volume resistivity of about 103 ?-cm (ohm cm) to 1010 ?-cm at 5,000 volts. Such thermoplastic composite materials may find utility in applications that require the thermoplastic to be capable of withstanding high voltage spikes, as would be encountered during a lightning strike.
    Type: Application
    Filed: July 2, 2008
    Publication date: January 7, 2010
    Inventors: Edward W.S. Bryant, Clifton P. Breay
  • Publication number: 20100001512
    Abstract: The present application is directed to dielectric isolators for use in aircraft fuel systems to control lightning induced current and allow dissipation of electrostatic charge. The dielectric isolators are configured to have a high enough impedance to limit lightning currents to low levels, but low enough impedance to allow electrostatic charge to dissipate without allowing buildup. Although the dielectric isolators may develop a potential difference across the dielectric length due to the effects of lightning currents and its inherent impedance, they are configured to withstand these induced voltages without dielectric breakdown or performance degradation. In one embodiment, the dielectric isolator includes a tube constructed of a composition including a thermoplastic organic polymer (e.g., PEEK) and carbon nanotubes, and a pair of fittings attached to opposing ends of the tube.
    Type: Application
    Filed: December 31, 2008
    Publication date: January 7, 2010
    Inventors: Clifton P. Breay, Sara D. Pfannenstiel, Stephen C. Matthews, Edward W.S. Bryant
  • Publication number: 20090322078
    Abstract: A coupling assembly for releasably interconnecting a fluid joint is provided where the fluid joint includes confronting ends of a pair of fluid conveying members, each of which has a ferrule fixedly attached thereto, and a sleeve circumferentially surrounding the ferrules. The coupling assembly includes a pair of coupling members, each of which has a first end and a second end, a hinge assembly configured to hingedly connect the first ends of the coupling members to permit them to rotate relative to each other between an open position and a closed position where the coupling members surround the sleeve, a pair of bonding wires, each of which is coupled to a respective coupling member and configured to electrically bond the respective coupling member to the ferrules of respective fluid conveying members, and a releasable latching assembly configured to releasably secure the second ends of the coupling members together when they are in their closed position.
    Type: Application
    Filed: June 30, 2008
    Publication date: December 31, 2009
    Applicant: Eaton Corporation
    Inventors: David E. Wern, Clifton P. Breay, Richard L. Statler, III
  • Patent number: 7222889
    Abstract: A coupling assembly is provided for releasably interconnecting confronting ends of conduit members. The coupling assembly creates a self-locking, and self-bonding connection wherein locking and unlocking is achieved by a predetermined amount of rotation of a lock nut group with respect to a stationary threaded flange. The overall construction of the coupling assembly creates the rigid connection between the conduit members, yet adequate sealing between the conduit members is provided by a single sealing member.
    Type: Grant
    Filed: August 23, 2005
    Date of Patent: May 29, 2007
    Assignee: Stanley Aviation Corporation
    Inventor: Clifton P. Breay
  • Patent number: 6883836
    Abstract: A positive locking fitting assembly is provided for interconnecting two adjacent structures, such as two modular components of an aircraft. The fitting assembly includes a pair of couplers which attach to the respective modular components, and a transfer tube which interconnects the couplers. Each coupler has a positive locking feature which prevents inadvertent uncoupling during operation. A plurality of redundant seals are incorporated throughout the construction of the fitting assembly which ensures a leak proof relationship not only between the joined pair of modular components, but also through the structure of the elements of the fitting assembly itself.
    Type: Grant
    Filed: January 17, 2003
    Date of Patent: April 26, 2005
    Assignee: Stanley Aviation Corporation
    Inventors: Clifton P. Breay, Thomas B. Darby, Daniel E. Keenan, Anthony W. Vaughan
  • Patent number: 6880859
    Abstract: A conduit coupling assembly is provided for interconnecting a pair of fluid conveying members placed in a confronting relationship within the coupling assembly. The coupling assembly includes a longitudinally split coupler having a pair of coupling halves rotatable about a hinge. A plurality of engagement members are mounted on the respective coupling halves for connecting the coupling halves. Electrical conductivity is maintained across the coupling assembly by a bonding wire on each of the coupling halves. Each bonding wire provides multiple points of contact with the metallic flanges of the fluid carrying members. Optionally, the flanges of the fluid carrying members and the coupling assembly may be coated with a conductive coating thereby providing a redundant means to prevent buildup of an electrostatic charge.
    Type: Grant
    Filed: July 31, 2003
    Date of Patent: April 19, 2005
    Assignee: Stanley Aviation Corporation
    Inventors: Clifton P. Breay, Anthony Vaughan, Sara D. Lopata
  • Publication number: 20040140667
    Abstract: A positive locking fitting assembly is provided for interconnecting two adjacent structures, such as two modular components of an aircraft. The fitting assembly includes a pair of couplers which attach to the respective modular components, and a transfer tube which interconnects the couplers. Each coupler has a positive locking feature which prevents inadvertent uncoupling during operation. A plurality of redundant seals are incorporated throughout the construction of the fitting assembly which ensures a leak proof relationship not only between the joined pair of modular components, but also through the structure of the elements of the fitting assembly-itself.
    Type: Application
    Filed: January 17, 2003
    Publication date: July 22, 2004
    Inventors: Clifton P. Breay, Thomas B. Darby, Daniel E. Keenan, Anthony Vaughan