Patents by Inventor Philip I Robinson

Philip I Robinson 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: 7004432
    Abstract: An aircraft mechanism including a flap positioning mechanism comprising a carriage and track system suitable for use with variable radius or multiple curvature tracks.
    Type: Grant
    Filed: November 13, 2001
    Date of Patent: February 28, 2006
    Assignee: Airbus UK Limited
    Inventor: Philip I Robinson
  • Publication number: 20040065783
    Abstract: An aircraft mechanism including a flap positioning mechanism comprising a carriage and track system suitable for use with variable radius or multiple curvature tracks.
    Type: Application
    Filed: June 23, 2003
    Publication date: April 8, 2004
    Inventor: Philip I Robinson
  • Patent number: 5591388
    Abstract: Staple fibres of solvent-spun cellulose are made by a method in which:i) cellulose is dissolved in an amine oxide solvent to form a hot cellulose solution,ii) the hot cellulose solution is extruded through a die assembly to form a tow of continuous filaments,iii) the tow is passed through a water bath to leach out the amine oxide,iv) the tow is crimped by passing through a stuffer box in which it is compressed to apply crimp,v) dry steam being injected into the stuffer box during the crimping process, andvi) the crimped tow is passed to a cutter and cut to the desired fibre length. An apparatus is also provided in which the staple fibres can be made.
    Type: Grant
    Filed: April 25, 1995
    Date of Patent: January 7, 1997
    Assignee: Courtaulds Fibres (Holdings) Limited
    Inventors: Alan Sellars, Patrick A. White, Philip I. Robinson
  • Patent number: 5363767
    Abstract: A guided missile for air to ground deployment having a modular construction which can be readily configured to suit varying deployment roles. The missile comprises a common central fuselage 1, 2, 3 carrying a fuel tank and mounting points for an engine, wings and nose-cone 7. Bolted onto either side of the fuselage are panniers 6a, 6b of variable length and payload capacity. In one embodiment the panniers 6a, 6b carry munitions for lateral ejection through frangile panels. In an alternative embodiment, munitions are mounted in the fuselage and the panniers carry fuel.
    Type: Grant
    Filed: December 12, 1990
    Date of Patent: November 15, 1994
    Assignee: British Aerospace Public Limited Company
    Inventor: Philip I. Robinson
  • Patent number: 4528978
    Abstract: A solar rocket absorber of rhenium tubes is used to provide heated liquid hydrogen to a thruster. The rhenium tubes are wrapped in a closed shape having an opening for receiving solar radiation for heating the liquid propellant. The vessel of rhenium tubes is held by a carbon shell which is further encased in a reradiation shield to prevent heat loss.
    Type: Grant
    Filed: December 8, 1983
    Date of Patent: July 16, 1985
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Philip I. Robinson
  • Patent number: 4509749
    Abstract: A dual purpose tennis net tie down and height setting device 14 comprises a top hook 16 for attaching to the upper edge 18 of tennis net 12. Depending from the top hook 16 is tie down chain 20 which connects in parallel with bottom hook 26 and a height refinement turnbuckle 32. By joining bottom hook 26 and chain 20 in parallel, the bottom hook 26 may be adjusted to correct for deviations in the depth of tie down fitting 24 without altering the distance between top hook interior 22 and the bottom of the last chain link 30.
    Type: Grant
    Filed: December 10, 1979
    Date of Patent: April 9, 1985
    Inventor: Philip I. Robinson
  • Patent number: 4377072
    Abstract: There is provided a ceramic heat exchange module 10 having fluid inlet and outlet conduits (12,20) extending from one side of horizontal manifolds (14,18). Serpentine tubes 16 extend from the opposed sides and connect the manifolds. In use, in a fluidized bed combustor 22, the manifolds are positioned between the base 30 and air inlets 32. Serpentine tubes extend into the fluidized bed 36, the fluid inlet and outlet conduits extend through the base for coupling to a working fluid supply.
    Type: Grant
    Filed: October 27, 1980
    Date of Patent: March 22, 1983
    Assignee: Rockwell International Corporation
    Inventors: John Campbell, Jr., Larry H. Russell, Philip I. Robinson
  • Patent number: 4357907
    Abstract: There is provided a fluidized bed combustor comprising an economizer contained in an upper interior portion and indirect heat exchange conduits suspended in the lower interior portion of the fluidized bed combustor in spaced relation to the interior surfaces of the fluidized bed combustor.
    Type: Grant
    Filed: October 27, 1980
    Date of Patent: November 9, 1982
    Assignee: Rockwell International Corporation
    Inventors: John Campbell, Jr., Larry H. Russell, Philip I. Robinson