Patents by Inventor Rhona Whitlock

Rhona Whitlock 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: 9701392
    Abstract: A joint including first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.
    Type: Grant
    Filed: July 22, 2016
    Date of Patent: July 11, 2017
    Assignees: Airbus Operations Limited, Airbus Operations (S.A.S.)
    Inventors: Rhona Whitlock, Massimo Del Tin, Peter Dalton, George Ford, Michael John Hill, Adrian Huntbatch, Laurence Breeze, Alain Depeige
  • Patent number: 9557204
    Abstract: A metering apparatus for determining a characteristic of a fluid, such as the volumetric flow rate, flowing through a non-linear section of a pipe is disclosed having a first strain gauge mountable to the non-linear section of the pipe offset from the bending neutral axis of the non-linear section of the pipe, to detect a bending force on the non-linear section of the pipe induced by the inertia of the fluid flowing through the pipe. A second strain gauge is mountable to the pipe disposed on the bending neutral axis of the non-linear section of the pipe, to detect at least one of the hoop strains, longitudinal strains and radial strains imparted on the pipe by the pressure of the fluid flowing through the pipe. A controller is configured to determine the mass flow rate of fluid flowing through the pipe based on the bending force determined by the first strain gauge and the at least one of the hoop strains, longitudinal strains and radial strains determined by the second strain gauge.
    Type: Grant
    Filed: May 25, 2016
    Date of Patent: January 31, 2017
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: George Edmond, Rhona Whitlock, Robert Case
  • Publication number: 20160349092
    Abstract: A metering apparatus for determining a characteristic of a fluid, such as the volumetric flow rate, flowing through a non-linear section of a pipe is disclosed having a first strain gauge mountable to the non-linear section of the pipe offset from the bending neutral axis of the non-linear section of the pipe, to detect a bending force on the non-linear section of the pipe induced by the inertia of the fluid flowing through the pipe. A second strain gauge is mountable to the pipe disposed on the bending neutral axis of the non-linear section of the pipe, to detect at least one of the hoop strains, longitudinal strains and radial strains imparted on the pipe by the pressure of the fluid flowing through the pipe. A controller is configured to determine the mass flow rate of fluid flowing through the pipe based on the bending force determined by the first strain gauge and the at least one of the hoop strains, longitudinal strains and radial strains determined by the second strain gauge.
    Type: Application
    Filed: May 25, 2016
    Publication date: December 1, 2016
    Inventors: George EDMOND, Rhona WHITLOCK, Robert CASE
  • Publication number: 20160332720
    Abstract: A joint including first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.
    Type: Application
    Filed: July 22, 2016
    Publication date: November 17, 2016
    Inventors: Rhona WHITLOCK, Massimo Del TIN, Peter DALTON, George FORD, Michael John HILL, Adrian HUNTBATCH, Laurence BREEZE, Alain DEPEIGE
  • Patent number: 9422049
    Abstract: A joint comprising first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.
    Type: Grant
    Filed: March 22, 2012
    Date of Patent: August 23, 2016
    Assignees: Airbus Operations Limited, Airbus Operations (S.A.S.)
    Inventors: Rhona Whitlock, Massimo Del Tin, Peter Dalton, George Ford, Michael John Hill, Adrian Huntbatch, Laurence Breze, Alain Depeige
  • Publication number: 20140008493
    Abstract: A joint comprising first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.
    Type: Application
    Filed: March 22, 2012
    Publication date: January 9, 2014
    Applicant: AIRBUS OPERATIONS LIMMITED
    Inventors: Rhona Whitlock, Massimo Deltin, Peter Dalton, George Ford, Michael John Hill, Adrian Huntbatch, Laurence Breeze