Patents by Inventor Amir Rezai

Amir Rezai 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: 20220410469
    Abstract: A method of fabricating an article by fused filament fabrication.
    Type: Application
    Filed: November 26, 2020
    Publication date: December 29, 2022
    Applicant: BAE Systems Plc
    Inventor: Amir Rezai
  • Patent number: 10611930
    Abstract: The invention relates to methods of bonding and a conductively bonded joint, provided by high loadings of conductively coated nano scale particulate fillers in a conductive adhesive in combination with a conductive intermediary structure, more particularly to a lightning strike resilient bonded joint between fibre reinforced polymer composites. A method of joining a first fibre reinforced polymer composite surface and a second fibre reinforced polymer composite surface, comprising the steps of providing a conductive intermediary structure between said first and second surfaces, filling the void between said surfaces and enveloping said intermediary structure with a conductive adhesive, curing the conductive adhesive to form a bonded first and second surface. A conductive adhesive comprising a curable binder and a high aspect ratio nanoscale carbon particulate filler present in the range of from 0.1 to 40% wt, wherein said particulate filler comprises a metal coating.
    Type: Grant
    Filed: January 16, 2014
    Date of Patent: April 7, 2020
    Assignee: BAE Systems PLC
    Inventors: Amir Rezai, Alexander Roy Parfitt, Brett Edward Hemingway
  • Patent number: 10261037
    Abstract: A structure to be monitored for damage and a method of monitoring the structure for damage are provided. The structure has a coating thereon, the coating defining a surface having characteristics which vary in a predetermined manner with damage to the structure. The surface has a series of conductive tracks applied thereto and in intimate contact therewith such that the said predetermined variation of the surface characteristics will vary the resistance of the series of conductive tracks in a predetermined manner in order to determine both location and extent of damage.
    Type: Grant
    Filed: February 2, 2015
    Date of Patent: April 16, 2019
    Assignee: BAE Systems plc
    Inventors: Jagjit Sidhu, Amir Rezai, David Andrew Cocksedge
  • Patent number: 10023702
    Abstract: The invention relates to methods and a novel powdered curable monomer which may be used to manufacture bulk polymers, adhesives and coatings composite materials with high percentage weight inclusions of particulate filler materials, more specifically to fibre reinforced polymer composite materials with high percentage weight inclusions of particulate filler materials. The preferred particulate filler materials are carbon nanotubes. The method according to the invention allows greater than 0.5 wt % of carbon nanotubes, typically greater 10% wt of carbon nanotubes or other high aspect ratio fillers to be readily incorporated in the resin matrix, before being applied to the fibre reinforcing plys.
    Type: Grant
    Filed: August 21, 2012
    Date of Patent: July 17, 2018
    Assignee: BAE Systems plc
    Inventors: David Baker, Amir Rezai
  • Patent number: 9909605
    Abstract: A method for forming a joint between a fiber reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fiber reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.
    Type: Grant
    Filed: October 21, 2013
    Date of Patent: March 6, 2018
    Assignee: BAE SYSTEMS plc
    Inventors: David Baker, Amir Rezai, Andrew David Wescott, Daniel Peter Graham
  • Publication number: 20170363557
    Abstract: A structure to be monitored for damage and a method of monitoring the structure for damage are provided. The structure has a coating thereon, the coating defining a surface having characteristics which vary in a predetermined manner with damage to the structure. The surface has a series of conductive tracks applied thereto and in intimate contact therewith such that the said predetermined variation of the surface characteristics will vary the resistance of the series of conductive tracks in a predetermined manner in order to determine both location and extent of damage.
    Type: Application
    Filed: February 2, 2015
    Publication date: December 21, 2017
    Inventors: Jagjit Sidhu, Amir Rezai, David Andrew Cocksedge
  • Publication number: 20170136694
    Abstract: Apparatus and a method of forming a composite component (8) by additive layer manufacturing are provided. The method includes the steps of providing an elongate tape (2) of carbon nanotubes (CNTs), applying stretching force to the tape (2) whereby to align the carbon nanotubes to the tape and form an aligned tape (27), impregnating the tape (27) with matrix material (40, 48, 50), forming the aligned tape (27) into portions (43) of required size and transferring the portions as required to a component build location whereby to form the component (8), layer by layer.
    Type: Application
    Filed: February 4, 2015
    Publication date: May 18, 2017
    Applicant: BAE Systems plc
    Inventors: Amir Rezai, Jagjit Sidhu, Andrew David Wescott
  • Publication number: 20160221229
    Abstract: A flexible manufacturing tool is provided. The tool includes a multi-layer generally planar sheet of material defining a tool surface thereon, means such as spaced jacks to controllably deform the sheet by applying out-of-plane deforming forces to the sheet and means selectively to increase and decrease interlayer shear or frictional forces whereby to vary the flexural stiffness of the sheet. Such means may comprise applying a vacuum between the layers to increase interlayer friction or the use of softenable polymers between the layers.
    Type: Application
    Filed: October 1, 2014
    Publication date: August 4, 2016
    Inventors: David BAKER, Amir REZAI
  • Publication number: 20150361308
    Abstract: The invention relates to methods of bonding and a conductively bonded joint, provided by high loadings of conductively coated nano scale particulate fillers in a conductive adhesive in combination with a conductive intermediary structure, more particularly to a lightning strike resilient bonded joint between fibre reinforced polymer composites. A method of joining a first fibre reinforced polymer composite surface and a second fibre reinforced polymer composite surface, comprising the steps of providing a conductive intermediary structure between said first and second surfaces, filling the void between said surfaces and enveloping said intermediary structure with a conductive adhesive, curing the conductive adhesive to form a bonded first and second surface. A conductive adhesive comprising a curable binder and a high aspect ratio nanoscale carbon particulate filler present in the range of from 0.1 to 40% wt, wherein said particulate filler comprises a metal coating.
    Type: Application
    Filed: January 16, 2014
    Publication date: December 17, 2015
    Applicant: BAE SYSTEMS plc
    Inventors: AMIR REZAI, ALEXANDER ROY PARFITT, BRETT EDWARD HEMINGWAY
  • Publication number: 20150298241
    Abstract: The invention relates to the manufacture of hybrid joints more particularly to the manufacture of joints between parts made of differing materials and most particularly to the manufacture of a metallic component comprising a plurality of preformed projections which penetrate composite fabric within a composite part. Particularly there is a method of forming an array of projections on a surface of a metallic component, the method including the steps of bringing at least one preformed projection into at least close proximity to the surface of the component and causing a portion of the projection and a portion of the component in the region of an intersection thereof to at least partially melt, and causing them to be joined together.
    Type: Application
    Filed: November 19, 2013
    Publication date: October 22, 2015
    Inventors: Daniel Peter Graham, David Baker, Amir Rezai, Andrew David Wescott
  • Publication number: 20150260208
    Abstract: A method for forming a joint between a fibre reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fibre reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.
    Type: Application
    Filed: October 21, 2013
    Publication date: September 17, 2015
    Applicant: BAE SYSTEMS plc
    Inventors: David Baker, Amir Rezai, Andrew David Wescott, Daniel Peter Graham
  • Patent number: 9010229
    Abstract: There is disclosed armor having an outer metallic layer, an inner fiber composite layer, and a supporting framework between the inner and outer layers. The supporting framework can include projections from the outer layer arranged to mechanically interlock with the fibers of the fiber composite, and can be arranged to provide an open region between the inner and outer layers that can be filled with a functional filler material.
    Type: Grant
    Filed: October 29, 2010
    Date of Patent: April 21, 2015
    Assignee: BAE Systems PLC
    Inventors: Jennifer Laura McDonald, David Baker, Amir Rezai
  • Publication number: 20140235759
    Abstract: The invention relates to methods and a novel powdered curable monomer which may be used to manufacture bulk polymers, adhesives and coatings composite materials with high percentage weight inclusions of particulate filler materials, more specifically to fibre reinforced polymer composite materials with high percentage weight inclusions of particulate filler materials. The preferred particulate filler materials are carbon nanotubes. The method according to the invention allows greater than 0.5 wt % of carbon nanotubes, typically greater 10% wt of carbon nanotubes or other high aspect ratio fillers to be readily incorporated in the resin matrix, before being applied to the fibre reinforcing plys.
    Type: Application
    Filed: August 21, 2012
    Publication date: August 21, 2014
    Inventors: David Baker, Amir Rezai
  • Patent number: 8578769
    Abstract: A flow sensor and fastener assembly, is disclosed which includes at least the following modules: a sensor housing and a fastener element; wherein: the sensor housing is adapted to receive a flow-based sensor, e.g. a MEMS airflow sensor; the sensor housing includes a connection for transmitting sensing signals from a fitted flow-based sensor; the fastener element includes a head and a shank, at least part of the shank being externally threaded; the fastener element includes a bore extending through the whole length of the fastener element; and the bore is shaped at the head end of the fastener element to provide a sensor housing receiving part.
    Type: Grant
    Filed: November 12, 2009
    Date of Patent: November 12, 2013
    Assignee: Bae Systems PLC.
    Inventors: Martyn John Hucker, Graham Andrew Johnson, David Baker, Amir Rezai
  • Publication number: 20120216670
    Abstract: There is disclosed armour having an outer metallic layer, an inner fibre composite layer, and a supporting framework between the inner and outer layers. The supporting framework can include projections from the outer layer arranged to mechanically interlock with the fibres of the fibre composite, and can be arranged to provide an open region between the inner and outer layers that can be filled with a functional filler material.
    Type: Application
    Filed: October 29, 2010
    Publication date: August 30, 2012
    Applicant: BAE Systems plc
    Inventors: Jennifer Laura McDonald, David Baker, Amir Rezai
  • Publication number: 20110209542
    Abstract: A flow sensor and fastener assembly, is disclosed which includes at least the following modules: a sensor housing and a fastener element; wherein: the sensor housing is adapted to receive a flow-based sensor, e.g. a MEMS airflow sensor; the sensor housing includes a connection for transmitting sensing signals from a fitted flow-based sensor; the fastener element includes a head and a shank, at least part of the shank being externally threaded; the fastener element includes a bore extending through the whole length of the fastener element; and the bore is shaped at the head end of the fastener element to provide a sensor housing receiving part.
    Type: Application
    Filed: November 12, 2009
    Publication date: September 1, 2011
    Applicant: BAE SYSTEMS plc
    Inventors: Martyn John Hucker, Graham Andrew Johnson, David Baker, Amir Rezai