Patents by Inventor Chris Payne

Chris Payne 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: 20250102116
    Abstract: Cryogenic storage turn trays may be provided having a variety of sensors. The storage turn trays can have a sample storage area, a gear assembly, a shaft assembly, and a sensor assembly. The sensor assembly can be configured to measure movement of a sample storage area to determine a position of the sample storage area. Various indicators, displays, and/or annunciators may communicate the position of the sample storage area to a user.
    Type: Application
    Filed: September 24, 2024
    Publication date: March 27, 2025
    Applicant: MVE Biological Solutions US, LLC
    Inventors: Jeff Brooks, Chris Payne, Christina Ellis, Doug Wilcox, Brian Lauman, Jeremy Corkran, Will Stockdell, David Fitzgerald, Jayrrd VAN ROOYEN, Bryan Borgerding
  • Publication number: 20250052453
    Abstract: A cryogenic freezer and a method of controlling temperature within the cryogenic freezer. The cryogenic freezer includes an inner vessel. The inner vessel defines a storage chamber. The cryogenic freezer includes an outer vessel surrounding the inner vessel. The outer vessel may define a vacuum-insulated space in between the outer vessel and the inner vessel. The cryogenic freezer includes a temperature sensor configured to measure a temperature within the storage chamber. The cryogenic freezer includes a controller coupled to the temperature sensor. The controller is configured to pulse an amount of cryogen into the storage container to control the temperature within the storage container.
    Type: Application
    Filed: October 29, 2024
    Publication date: February 13, 2025
    Applicant: MVE Biological Solutions US, LLC
    Inventors: Jeffrey Brooks, Douglas Alan Wilcox, II, Daniel McCall, Chris Payne
  • Patent number: 12158295
    Abstract: A cryogenic freezer and a method of controlling temperature within the cryogenic freezer. The cryogenic freezer includes an inner vessel. The inner vessel defines a storage chamber. The cryogenic freezer includes an outer vessel surrounding the inner vessel. The outer vessel may define a vacuum-insulated space in between the outer vessel and the inner vessel. The cryogenic freezer includes a temperature sensor configured to measure a temperature within the storage chamber. The cryogenic freezer includes a controller coupled to the temperature sensor. The controller is configured to pulse an amount of cryogen into the storage container to control the temperature within the storage container.
    Type: Grant
    Filed: November 11, 2022
    Date of Patent: December 3, 2024
    Assignee: MVE Biological Solutions US, LLC
    Inventors: Jeffrey Brooks, Douglas Alan Wilcox, II, Daniel McCall, Chris Payne
  • Publication number: 20240159433
    Abstract: A cryogenic freezer and a method of controlling temperature within the cryogenic freezer. The cryogenic freezer includes an inner vessel. The inner vessel defines a storage chamber. The cryogenic freezer includes an outer vessel surrounding the inner vessel. The outer vessel may define a vacuum-insulated space in between the outer vessel and the inner vessel. The cryogenic freezer includes a temperature sensor configured to measure a temperature within the storage chamber. The cryogenic freezer includes a controller coupled to the temperature sensor. The controller is configured to pulse an amount of cryogen into the storage container to control the temperature within the storage container.
    Type: Application
    Filed: November 11, 2022
    Publication date: May 16, 2024
    Applicant: MVE Biological Solutions US, LLC
    Inventors: Jeffrey Brooks, Douglas Alan Wilcox, II, Daniel McCall, Chris Payne
  • Patent number: 11629690
    Abstract: A reinforcing structure for a wind turbine blade is in the form of an elongate stack of layers of pultruded fibrous composite strips supported within a U-shaped channel. The length of each layer is slightly different to create a taper at the ends of the stack; the centre of the stack has five layers, and each end has a single layer. The ends of each layer are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip extending the full length of the stack. The reinforcing structure extends along a curved path within the outer shell of the blade. The regions of the outer shell of the blade on either side of the reinforcing structure are filled with structural foam, and the reinforcing structure and the foam are both sandwiched between an inner skin and an outer skin.
    Type: Grant
    Filed: May 31, 2022
    Date of Patent: April 18, 2023
    Assignee: Vestas Wind Systems A/S
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Publication number: 20220290648
    Abstract: A reinforcing structure for a wind turbine blade is in the form of an elongate stack of layers of pultruded fibrous composite strips supported within a U-shaped channel. The length of each layer is slightly different to create a taper at the ends of the stack; the centre of the stack has five layers, and each end has a single layer. The ends of each layer are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip extending the full length of the stack. The reinforcing structure extends along a curved path within the outer shell of the blade. The regions of the outer shell of the blade on either side of the reinforcing structure are filled with structural foam, and the reinforcing structure and the foam are both sandwiched between an inner skin and an outer skin.
    Type: Application
    Filed: May 31, 2022
    Publication date: September 15, 2022
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Patent number: 11371482
    Abstract: A reinforcing structure for a wind turbine blade is in the form of an elongate stack of layers of pultruded fibrous composite strips supported within a U-shaped channel. The length of each layer is slightly different to create a taper at the ends of the stack; the centre of the stack has five layers, and each end has a single layer. The ends of each layer are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip extending the full length of the stack. The reinforcing structure extends along a curved path within the outer shell of the blade. The regions of the outer shell of the blade on either side of the reinforcing structure are filled with structural foam, and the reinforcing structure and the foam are both sandwiched between an inner skin and an outer skin.
    Type: Grant
    Filed: October 21, 2019
    Date of Patent: June 28, 2022
    Assignee: Vestas Wind Systems A/S
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Publication number: 20200049128
    Abstract: A reinforcing structure for a wind turbine blade is in the form of an elongate stack of layers of pultruded fibrous composite strips supported within a U-shaped channel. The length of each layer is slightly different to create a taper at the ends of the stack; the centre of the stack has five layers, and each end has a single layer. The ends of each layer are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip extending the full length of the stack. The reinforcing structure extends along a curved path within the outer shell of the blade. The regions of the outer shell of the blade on either side of the reinforcing structure are filled with structural foam, and the reinforcing structure and the foam are both sandwiched between an inner skin and an outer skin.
    Type: Application
    Filed: October 21, 2019
    Publication date: February 13, 2020
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Patent number: 10487797
    Abstract: A reinforcing structure for a wind turbine blade is in the form of an elongate stack of layers of pultruded fibrous composite strips supported within a U-shaped channel. The length of each layer is slightly different to create a taper at the ends of the stack; the centre of the stack has five layers, and each end has a single layer. The ends of each layer are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip extending the full length of the stack. The reinforcing structure extends along a curved path within the outer shell of the blade. The regions of the outer shell of the blade on either side of the reinforcing structure are filled with structural foam, and the reinforcing structure and the foam are both sandwiched between an inner skin and an outer skin.
    Type: Grant
    Filed: December 11, 2012
    Date of Patent: November 26, 2019
    Assignee: Vestas Wind Systems A/S
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Publication number: 20140301859
    Abstract: A reinforcing structure 9 for a wind turbine blade is in the form of an elongate stack 27 of layers 31 of pultruded fibrous composite strips supported within a U-shaped channel 28. The length of each layer 31 is slightly different to create a taper at the ends of the stack; the centre of the stack 27 has five layers 31, and each end has a single layer 31. The ends of each layer 31 are chamfered, and the stack is coated with a thin flexible pultruded fibrous composite strip 33 extending the full length of the stack 27. The reinforcing structure 9 extends along a curved path within the outer shell of the blade. During configuration of the blade components within a mould 37, the reinforcing structure 9 is introduced into the mould 37 by sliding the channel 28 along the surface of an elongate wedge 29 within the mould 37 along the curved path.
    Type: Application
    Filed: December 11, 2012
    Publication date: October 9, 2014
    Applicant: VESTAS WIND SYSTEMS A/S
    Inventors: Mark Hancock, Frank Hoelgaard Hahn, Chris Payne
  • Patent number: 8584991
    Abstract: A wing, having an adjustable flap that can be moved between a retracted and an extended setting is provided, as well as a gap-covering device, with an adjustment lever and a gap-covering flap arranged on the latter with a flow surface. The adjustment lever with the gap-covering flap is pre-loaded by means of a pre-loading device into a first setting, in which the gap-covering flap is located in the interior of the wing. The adjustable flap and the adjustment lever with the gap-covering flap are mechanically coupled such that as the adjustable flap moves into its retracted setting, a movement of the adjustment lever takes place against the pre-load effected by the pre-loading device, into a second setting. The flow surface of the gap-covering flap in the second setting of the adjustment lever runs between the upper side of the retracted adjustable flap and the wing flow surface.
    Type: Grant
    Filed: November 10, 2009
    Date of Patent: November 19, 2013
    Assignee: Airbus Operations GmbH
    Inventors: Bernhard Schlipf, Chris Payne, Markus Gibbert, Tom Dostmann
  • Publication number: 20110297796
    Abstract: A wing, having an adjustable flap that can be moved between a retracted and an extended setting is provided, as well as a gap-covering device, with an adjustment lever and a gap-covering flap arranged on the latter with a flow surface. The adjustment lever with the gap-covering flap is pre-loaded by means of a pre-loading device into a first setting, in which the gap-covering flap is located in the interior of the wing. The adjustable flap and the adjustment lever with the gap-covering flap are mechanically coupled such that as the adjustable flap moves into its retracted setting, a movement of the adjustment lever takes place against the pre-load effected by the pre-loading device, into a second setting. The flow surface of the gap-covering flap in the second setting of the adjustment lever runs between the upper side of the retracted adjustable flap and the wing flow surface.
    Type: Application
    Filed: November 10, 2009
    Publication date: December 8, 2011
    Applicants: AIRBUS OPERATIONS LTD, AIRBUS OPERATIONS GMBH
    Inventors: Bernhard Schlipf, Chris Payne, Markus Gibbert, Tom Dostmann