Patents Assigned to HS MARSTON AEROSPACE LTD.
  • Patent number: 10642291
    Abstract: A valve is provided and includes a bypass block defining a bypass flowpath fluidly communicable with main flowpaths, a member disposable within the bypass block to occupy and move between first and second positions, the member being configured to permit fluid flow through the bypass flowpath when occupying the first position and to block a portion of the bypass flowpath to thereby prevent fluid flow through the bypass flowpath when occupying the second position and an elastic element. The elastic element is coupled to the member and configured to bias the member in a biasing direction toward the second position responsive to a temperature of fluid flowing along the main flowpaths.
    Type: Grant
    Filed: August 22, 2013
    Date of Patent: May 5, 2020
    Assignee: HS MARSTON AEROSPACE LTD
    Inventors: Sean L. Cameron, David Russell Scott, Stuart Anthony Astley, Nigel Philip Clark, Patrick James Jones
  • Patent number: 10544991
    Abstract: A heat exchange plate for a plate heat exchanger includes a plate body having a first side and a second side opposed to the first side. A plurality of pins extends from the first side, and a plurality of recesses is formed in the second side for locating the pins of a similar heat exchange plate arranged adjacent thereto.
    Type: Grant
    Filed: June 30, 2016
    Date of Patent: January 28, 2020
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventors: Mark F. Hill, Robert J. Housely
  • Patent number: 10539378
    Abstract: A heat exchanger comprises a conduit defining an inlet flow path for a fluid; a heat exchanger matrix disposed to receive a flow from the inlet flow path; and a swirler disposed within the conduit and arranged to improve dispersion of a flow from the inlet flow path over the heat exchanger matrix.
    Type: Grant
    Filed: October 12, 2017
    Date of Patent: January 21, 2020
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventors: Jacob Diffey, John Marsh, James Green, Chris McNab
  • Patent number: 10429331
    Abstract: A heat exchanger monitoring system includes a heat exchanger 11 capable of receiving a flow F of a working fluid therethrough. A first sensor 12 is disposed upstream of the heat exchanger 11 for measuring at least one property of fluid relating to an amount of contaminant material carried by a first flow entering the heat exchanger 11 and configured to output a first sensor signal indicative of the measured property of the fluid. A second sensor 14 is disposed downstream of the heat exchanger 11 for measuring the same property of the fluid relating to an amount of contaminant material carried by a second flow exiting the heat exchanger 11 and configured to output a second sensor signal indicative of the measured property of the fluid.
    Type: Grant
    Filed: February 2, 2018
    Date of Patent: October 1, 2019
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventor: Paul Phillips
  • Patent number: 9733028
    Abstract: A valve includes an outer structure. The valve includes a hollow shaft that includes holes formed therein, the shaft disposed within the outer structure and translatable from a first position to a second position. A memory metal alloy (MMA) spring is coupled to the shaft and the outer structure, the MMA spring expanding and moving the shaft from the first position to the second position in response to a temperature of a fluid. A valve head is coupled to the shaft and adapted to be biased within the outer structure, the valve head closing a bypass inlet in the first position and allowing fluid to enter the bypass inlet in the second position, and transferring fluid from the bypass inlet into the hollow shaft so that the fluid can exit the valve via an outlet. A pressure relief mechanism may be included.
    Type: Grant
    Filed: April 17, 2013
    Date of Patent: August 15, 2017
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventors: David Russell Scott, Sean L. Cameron
  • Patent number: 9417016
    Abstract: A laminated heat exchanger includes at least one heat exchange layer that includes a plurality of side members that define a frame having an interior portion. A plurality of heat exchange members extend between at least two of the plurality of side members across the interior portion. The plurality of heat exchange members are linked by a ligament member to form a heat exchange member chain.
    Type: Grant
    Filed: January 5, 2011
    Date of Patent: August 16, 2016
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventor: David Russell Scott
  • Patent number: 9260191
    Abstract: A heat exchanger apparatus is disposed within a first pathway along which a first fluid flows. The heat exchanger apparatus includes a component disposed in the first pathway and the component includes heat transfer surfaces. Each heat transfer surface includes a central body, an outer body surrounding the central body and intermediate bodies extending between the central body and the outer body. The heat transfer surfaces are arranged together such that the central bodies, the outer bodies and the intermediate bodies of each heat transfer surface form at least one or more second pathways along which a second fluid flows and such that the outer bodies of each heat transfer surface form a component surface disposed to contact the first and second fluids.
    Type: Grant
    Filed: August 26, 2011
    Date of Patent: February 16, 2016
    Assignee: HS MARSTON AEROSPACE LTD.
    Inventors: Berwyn Owain Pollard, David Russell Scott
  • Patent number: 8800643
    Abstract: A surface cooler includes a base plate, and at least one fin element extending from the base plate. The at least one fin element includes an outer surface portion that is configured and disposed to be in direct contact with a first fluid and an inner surface portion that is configured and disposed to be in direct contact with a second fluid. The at least one fin element defines a primary heat exchange member that is configured and disposed to facilitate an exchange of heat between the first and second fluids.
    Type: Grant
    Filed: December 27, 2010
    Date of Patent: August 12, 2014
    Assignee: HS Marston Aerospace Ltd.
    Inventors: Berwyn Owain Pollard, David Russell Scott
  • Patent number: 8770269
    Abstract: A surface cooler is provided and includes an oil layer, through which oil flows, a separating plate disposed in heat transfer communication with the oil and fins extending into an air flow pathway and being disposed in heat transfer communication with the separating plate, the fins being arranged with varied configurations at each of two or more sections sequentially defined along a predominant direction of air flow along the air flow pathway.
    Type: Grant
    Filed: June 11, 2010
    Date of Patent: July 8, 2014
    Assignee: HS Marston Aerospace Ltd.
    Inventor: David Russell Scott
  • Patent number: 8708243
    Abstract: A valve includes a housing and a valve seat and a structure fixedly disposed remote from the valve seat, a valve head to open and close the valve seat, fluid being permitted to flow when the valve seat is open and an elastic system anchored on the structure and coupled to the valve head, the elastic system including a biasing element and an elastic element formed of memory metal alloy disposed to contact fluid permitted to flow, the biasing element and the elastic element being configured to cooperatively move the valve head toward a valve seat open position when a fluid temperature is below a lower limit, and the biasing element and the elastic element being further configured to cooperatively move the valve head toward a valve seat closed position in opposition to the biasing element when the fluid temperature is above an upper limit.
    Type: Grant
    Filed: October 19, 2010
    Date of Patent: April 29, 2014
    Assignee: HS Marston Aerospace Ltd.
    Inventors: Sean L. Cameron, Carl D. Burton
  • Publication number: 20140054387
    Abstract: A valve is provided and includes a bypass block defining a bypass flowpath fluidly communicable with main flowpaths, a member disposable within the bypass block to occupy and move between first and second positions, the member being configured to permit fluid flow through the bypass flowpath when occupying the first position and to block a portion of the bypass flowpath to thereby prevent fluid flow through the bypass flowpath when occupying the second position and an elastic element. The elastic element is coupled to the member and configured to bias the member in a biasing direction toward the second position responsive to a temperature of fluid flowing along the main flowpaths.
    Type: Application
    Filed: August 22, 2013
    Publication date: February 27, 2014
    Applicant: HS MARSTON AEROSPACE LTD
    Inventors: Sean L. Cameron, David Russell Scott, Stuart Anthony Astley, Nigel Philip Clark, Patrick James Jones
  • Publication number: 20130277039
    Abstract: A valve may include an outer structure. The valve may include a hollow shaft that includes holes formed therein, the shaft disposed within the outer structure and translatable from a first position to a second position. A memory metal alloy (MMA) spring may be coupled to the shaft and the outer structure, the MMA spring expanding and moving the shaft from the first position to the second position in response to a temperature of a fluid. A valve head may be coupled to the shaft and adapted to be biased within the outer structure, the valve head closing a bypass inlet in the first position and allowing fluid to enter the bypass inlet in the second position, and transferring fluid from the bypass inlet into the hollow shaft so that the fluid can exit the valve via an outlet. A pressure relief mechanism may be included.
    Type: Application
    Filed: April 17, 2013
    Publication date: October 24, 2013
    Applicant: HS Marston Aerospace Ltd.
    Inventors: David Russell Scott, Sean L. Cameron
  • Patent number: 8544531
    Abstract: A surface cooler is provided and includes an oil layer through which oil flows, fins extending into an air flow pathway and being disposed at a first side of the oil layer in heat transfer communication with the oil, an acoustic lining to reduce noise present in or transmitted by the air flow pathway, which is disposed at a second side of the oil layer opposite the first side and noise transfer tubes extending through the oil layer to transfer the noise present in or transmitted by the air flow pathway to the acoustic lining.
    Type: Grant
    Filed: June 11, 2010
    Date of Patent: October 1, 2013
    Assignee: HS Marston Aerospace Ltd.
    Inventors: David Russell Scott, Berwyn Owain Pollard
  • Publication number: 20130048261
    Abstract: A heat exchanger is provided through which first and second fluids flow in a heat transfer arrangement. The heat exchanger includes a plurality of laminates. Each laminate includes a plurality of primary heat transfer surfaces disposed to contact the first and second fluids and a plurality of secondary heat transfer surfaces disposed to contact the first and/or second fluid. The respective pluralities of the primary and secondary heat transfer surfaces are configured to form respective pluralities of first and second flow pathways along which the first and second fluids flow, respectively, in the heat transfer arrangement. At least one of the plurality of the primary heat transfer surfaces is corrugated along a length of at least one of the plurality of the first flow pathways.
    Type: Application
    Filed: August 26, 2011
    Publication date: February 28, 2013
    Applicant: HS MARSTON AEROSPACE LTD.
    Inventors: David Russell Scott, Berwyn Owain Pollard
  • Publication number: 20130048243
    Abstract: A heat exchanger apparatus is provided and is configured to be disposed within a first pathway along which a first fluid flows. The heat exchanger apparatus includes a component disposed in the first pathway and including heat transfer surfaces configured to define at least one or more second pathways along which a second fluid flows. The heat transfer surfaces are configured to form an exterior surface of the component and are disposed to contact the first and/or second fluids.
    Type: Application
    Filed: August 26, 2011
    Publication date: February 28, 2013
    Applicant: HS MARSTON AEROSPACE LTD.
    Inventors: Berwyn Owain Pollard, David Russell Scott