Patents Assigned to MT Aerospace AG
  • Patent number: 10527230
    Abstract: The invention relates to a container for holding and storing liquids and viscous materials, in particular cryogenic fluids, comprising a jacket (12), which defines the interior (14) of the container (10) having a chamber (16), said container (10) being constituted of at least two container structures (20, 20?, 20?) and each of said at least two container structures (20, 20?, 20?) being formed as one piece from a blank (32) and having a dome portion (22), a branching portion (24), which is contiguous to the dome portion (22), and two cylinder portions (26, 28; 26?, 28?), which are contiguous to the branching portion (24), and the mutually facing container structures (20, 20; 20?, 20?) which are adjacent to each other being joined together.
    Type: Grant
    Filed: August 26, 2015
    Date of Patent: January 7, 2020
    Assignee: MT Aerospace AG
    Inventors: Martin Stachulla, Daniel Zell
  • Patent number: 10247227
    Abstract: A component for the transmission and absorption of mechanical forces and moments includes at least one dimensionally stable component element having at least one hollow-profiled section extending along a longitudinal axis of the dimensionally stable component element, and at least one hollow-profiled component element consisting of fiber-reinforced plastic extending along a longitudinal axis of the hollow-profiled component element. The hollow-profiled component element is partially received by the hollow-profiled section of the dimensionally stable component element in a form-fitting manner. The component is produced by a method that includes the steps of inserting one end of the one hollow-profiled component element into the hollow-profiled section of the dimensionally stable component element and pressing the outer circumference (26) of the hollow-profiled component element (16) against the inner circumference (24) of the hollow-profiled section (14) by an inflatable element.
    Type: Grant
    Filed: January 22, 2018
    Date of Patent: April 2, 2019
    Assignee: MT Aerospace AG
    Inventors: Wolfgang Fiedler, Thomas Lippert, Taylan Toprak
  • Publication number: 20180142727
    Abstract: A component for the transmission and absorption of mechanical forces and moments includes at least one dimensionally stable component element having at least one hollow-profiled section extending along a longitudinal axis of the dimensionally stable component element, and at least one hollow-profiled component element consisting of fibre-reinforced plastic extending along a longitudinal axis of the hollow-profiled component element. The hollow-profiled component element is partially received by the hollow-profiled section of the dimensionally stable component element in a form-fitting manner. The component is produced by a method that includes the steps of inserting one end of the one hollow-profiled component element into the hollow-profiled section of the dimensionally stable component element and pressing the outer circumference (26) of the hollow-profiled component element (16) against the inner circumference (24) of the hollow-profiled section (14) by an inflatable element.
    Type: Application
    Filed: January 22, 2018
    Publication date: May 24, 2018
    Applicant: MT AEROSPACE AG
    Inventors: Wolfgang FIEDLER, Thomas LIPPERT, Taylan TOPRAK
  • Patent number: 9874240
    Abstract: The invention relates to a component for absorbing and/or transmitting mechanical forces and/or moments, comprising at least one dimensionally stable component element (12, 12?, 12?, 2??, 12??), which has at least one hollow-profiled section (14), and at least one hollow-profiled component element (16) consisting of fiber-reinforced plastic, which can be partially received by the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??), and can be arranged in a form-fitting manner in the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??) by means of raised portions (32, 32?) which extend radially inwards and/or depressions (38, 38?), recesses or holes which extend radially outwards, wherein the inner circumference (24) of the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??) and the outer circumference (26) of the hollow-profiled component element (16) consisting
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: January 23, 2018
    Assignee: MT AEROSPACE AG
    Inventors: Wolfgang Fiedler, Thomas Lippert, Taylan Toprak
  • Publication number: 20170299120
    Abstract: The invention relates to a container for holding and storing liquids and viscous materials, in particular cryogenic fluids, comprising a jacket (12), which defines the interior (14) of the container (10) having a chamber (16), said container (10) being constituted of at least two container structures (20, 20?, 20?) and each of said at least two container structures (20, 20?, 20?) being formed as one piece from a blank (32) and having a dome portion (22), a branching portion (24), which is contiguous to the dome portion (22), and two cylinder portions (26, 28; 26?, 28?), which are contiguous to the branching portion (24), and the mutually facing container structures (20, 20; 20?, 20?) which are adjacent to each other being joined together.
    Type: Application
    Filed: August 26, 2015
    Publication date: October 19, 2017
    Applicant: MT AEROSPACE AG
    Inventors: Martin STACHULLA, Daniel ZELL
  • Patent number: 9468965
    Abstract: The invention relates to a method for shaping an essentially flat-surfaced blank (10) to form a shell body (34), comprising the following steps: forming at least one flat-surfaced, buckling-stable insert (12) which is adapted to form, dimension and deformation properties of the flat-surfaced blank (10); forming a blank (14) to be deformed and at least one buckling-stable insert (16, 16?, 16?) to be deformed from the flat-surfaced blank (10, 10?) and the at least one flat-surfaced buckling-stable insert (12, 12?); placing and clamping the blank (14) to be deformed and the at least one buckling-stable insert (16, 16?, 16?) relative to one another and deforming the blank (14) together with the at least one buckling-stable insert (16, 16?, 16?) to be deformed in order to form the shell body, using at least one forming tool (32) that acts upon the front or inner side (20) of the blank (14) to be deformed or the at least one insert (16) to be deformed which is provided as a support.
    Type: Grant
    Filed: March 28, 2011
    Date of Patent: October 18, 2016
    Assignee: MT Aerospace AG
    Inventor: Wulf Radtke
  • Patent number: 9302437
    Abstract: The present invention relates to a high-pressure tank made from fiber-reinforced plastic for, in particular, gaseous media, wherein, on its inner wall, the tank is equipped completely or partially with a substantially permeation-tight foil made of metal, wherein the metal has a high elastic range and a low thermal expansion coefficient, and the foil has a thickness of ?0.5 mm. The invention also relates to a method for manufacturing tanks of this type.
    Type: Grant
    Filed: December 15, 2014
    Date of Patent: April 5, 2016
    Assignee: MT AEROSPACE AG
    Inventor: Wulf Radtke
  • Patent number: 9011622
    Abstract: The present invention relates to a high-pressure tank made from fiber-reinforced plastic for, in particular, gaseous media, wherein, on its inner wall, the tank is equipped completely or partially with a substantially permeation-tight foil made of metal, wherein the metal has a high elastic range and a low thermal expansion coefficient, and the foil has a thickness of ?0.5 mm. The invention also relates to a method for manufacturing tanks of this type.
    Type: Grant
    Filed: March 30, 2011
    Date of Patent: April 21, 2015
    Assignee: MT Aerospace AG
    Inventor: Wulf Radtke
  • Publication number: 20150096994
    Abstract: The present invention relates to a high-pressure tank made from fiber-reinforced plastic for, in particular, gaseous media, wherein, on its inner wall, the tank is equipped completely or partially with a substantially permeation-tight foil made of metal, wherein the metal has a high elastic range and a low thermal expansion coefficient, and the foil has a thickness of ?0.5 mm. The invention also relates to a method for manufacturing tanks of this type.
    Type: Application
    Filed: December 15, 2014
    Publication date: April 9, 2015
    Applicant: MT AEROSPACE AG
    Inventor: Wulf RADTKE
  • Publication number: 20140137700
    Abstract: The invention relates to a component for absorbing and/or transmitting mechanical forces and/or moments, comprising at least one dimensionally stable component element (12, 12?, 12?, 2??, 12??), which has at least one hollow-profiled section (14), and at least one hollow-profiled component element (16) consisting of fibre-reinforced plastic, which can be partially received by the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??), and can be arranged in a form-fitting manner in the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??) by means of raised portions (32, 32?) which extend radially inwards and/or depressions (38, 38?), recesses or holes which extend radially outwards, wherein the inner circumference (24) of the hollow-profiled section (14) of the dimensionally stable component element (12, 12?, 12?, 12??, 12??) and the outer circumference (26) of the hollow-profiled component element (16) consisting
    Type: Application
    Filed: June 19, 2012
    Publication date: May 22, 2014
    Applicant: MT AEROSPACE AG
    Inventors: Wolfgang Fiedler, Thomas Lippert, Taylan Toprak
  • Patent number: 8613190
    Abstract: The invention relates to a pressure vessel consisting of a housing and an insulating layer lining the inner surface of the housing. The housing is formed from a fiber composite material which has a high mechanical and thermal resistance and the insulating layer is formed from a gas-tight silicone elastomer, with the housing and the insulating layer being bonded to each other. The invention also relates to a method for the manufacture of such pressure vessels.
    Type: Grant
    Filed: November 3, 2009
    Date of Patent: December 24, 2013
    Assignee: MT Aerospace AG
    Inventors: Bernd Murawski, Helmut Maierhofer
  • Publication number: 20130256157
    Abstract: The present invention relates to a high-pressure tank made from fiber-reinforced plastic for, in particular, gaseous media, wherein, on its inner wall, the tank is equipped completely or partially with a substantially permeation-tight foil made of metal, wherein the metal has a high elastic range and a low thermal expansion coefficient, and the foil has a thickness of ?0.5 mm. The invention also relates to a method for manufacturing tanks of this type.
    Type: Application
    Filed: March 20, 2011
    Publication date: October 3, 2013
    Applicant: MT AEROSPACE AG
    Inventor: Wulf Radtke
  • Publication number: 20130219981
    Abstract: The invention relates to a method for shaping an essentially flat-surfaced blank (10) to form a shell body (34), comprising the following steps: forming at least one flat-surfaced, buckling-stable insert (12) which is adapted to form, dimension and deformation properties of the flat-surfaced blank (10); forming a blank (14) to be deformed and at least one buckling-stable insert (16, 16?, 16?) to be deformed from the flat-surfaced blank (10, 10?) and the at least one flat-surfaced buckling-stable insert (12, 12?); placing and clamping the blank (14) to be deformed and the at least one buckling-stable insert (16, 16?, 16?) relative to one another and deforming the blank (14) together with the at least one buckling-stable insert (16, 16?, 16?) to be deformed in order to form the shell body, using at least one forming tool (32) that acts upon the front or inner side (20) of the blank (14) to be deformed or the at least one insert (16) to be deformed which is provided as a support.
    Type: Application
    Filed: March 28, 2011
    Publication date: August 29, 2013
    Applicant: MT AEROSPACE AG
    Inventor: Wulf Radtke
  • Patent number: 7798450
    Abstract: The invention relates to a support structure for a retractable and extendable flap (12) associated with an object (14), surrounded by a flowing fluid, comprising a shell profile (16) that has a fluid/aerodynamic low-drag form on the outer side and on the inner side forms a chamber (18) for at least partially receiving a device (20) for retracting and extending the flap (12).
    Type: Grant
    Filed: August 5, 2004
    Date of Patent: September 21, 2010
    Assignee: MT Aerospace AG
    Inventors: Aicke Patzelt, Michael Reiprich, Gunther Stegmaier, Wietse Wiglema
  • Publication number: 20100196637
    Abstract: The invention relates to a method for producing fibre-reinforced hollow bodies comprising integrally formed elements in a hollow mould. A fibre mat is laminated in two halves of the hollow mould, which respectively form the negative mould for the fibre-reinforced hollow bodies comprising integrally formed elements to be produced, and, once the two halves of the thus lined hollow mould have been connected, the fibre mat is pressed into the hollow mould under pressure in a form-fitting manner. The invention also relates to products produced according to the inventive method.
    Type: Application
    Filed: March 26, 2008
    Publication date: August 5, 2010
    Applicant: MT AEROSPACE AG
    Inventors: Thomas Lippert, Helmut Michel, Ulrich Strasser
  • Publication number: 20100108691
    Abstract: The invention relates to a pressure vessel consisting of a housing and an insulating layer lining the inner surface of the housing. The housing is formed from a fiber composite material which has a high mechanical and thermal resistance and the insulating layer is formed from a gas-tight silicone elastomer, with the housing and the insulating layer being bonded to each other. The invention also relates to a method for the manufacture of such pressure vessels.
    Type: Application
    Filed: November 3, 2009
    Publication date: May 6, 2010
    Applicant: MT AEROSPACE AG
    Inventors: Bernd Murawski, Helmut Maierhofer
  • Patent number: 7644600
    Abstract: The invention relates to a vacuum-assisted method and a device for forming an essentially flat blank (12) of metal into a thin-walled, shell-type body (14), especially for performing the method in accordance with one of the preceding claims, that has a supporting structure (16) forming a mold chamber (18) that holds the blank (12) during increasing deformation into the thin-walled, shell-body (14), a device (20) allocated to the supporting structure (16) for clamping the blank (12) about its circumference (22) to the supporting structure (16), that seals the reverse face (24) of the blank (12) facing towards the mold chamber (18) against the front face (26) of the blank (12) facing away from the mold chamber (18), and a device (28) allocated to the mold chamber (18) that also communicates with the mold chamber (18) for applying a vacuum and evacuating the mold chamber (18), and at least one forming tool (50) applied to the front face (26) of the blank (12) is/are allocated to the supporting structure (16), an
    Type: Grant
    Filed: October 15, 2008
    Date of Patent: January 12, 2010
    Assignee: MT Aerospace AG
    Inventors: Helmut Michel, Wulf Radtke, Johannes Hegels
  • Publication number: 20100000279
    Abstract: The invention relates to a vacuum-assisted method and a device for forming an essentially flat blank (12) of metal into a thin-walled, shell-type body (14), especially for performing the method in accordance with one of the preceding claims, that has a supporting structure (16) forming a mold chamber (18) that holds the blank (12) during increasing deformation into the thin-walled, shell-body (14), a device (20) allocated to the supporting structure (16) for clamping the blank (12) about its circumference (22) to the supporting structure (16), that seals the reverse face (24) of the blank (12) facing towards the mold chamber (18) against the front face (26) of the blank (12) facing away from the mold chamber (18), and a device (28) allocated to the mold chamber (18) that also communicates with the mold chamber (18) for applying a vacuum and evacuating the mold chamber (18), and at least one forming tool (50) applied to the front face (26) of the blank (12) is/are allocated to the supporting structure (16), an
    Type: Application
    Filed: October 15, 2008
    Publication date: January 7, 2010
    Applicant: MT AEROSPACE AG
    Inventors: Helmut MICHEL, Wulf RADTKE, Johannes HEGELS
  • Patent number: 7454936
    Abstract: The invention relates to a vacuum-assisted method and a device for forming an essentially flat blank (12) of metal into a thin-walled, shell-type body (14), especially for performing the method in accordance with one of the preceding claims, that has a supporting structure (16) forming a mold chamber (18) that holds the blank (12) during increasing deformation into the thin-walled, shell-body (14), a device (20) allocated to the supporting structure (16) for clamping the blank (12) about its circumference (22) to the supporting structure (16), that seals the reverse face (24) of the blank (12) facing towards the mold chamber (18) against the front face (26) of the blank (12) facing away from the mold chamber (18), and a device (28) allocated to the mold chamber (18) that also communicates with the mold chamber (18) for applying a vacuum and evacuating the mold chamber (18), and at least one forming tool (50) applied to the front face (26) of the blank (12) is/are allocated to the supporting structure (16), an
    Type: Grant
    Filed: May 22, 2006
    Date of Patent: November 25, 2008
    Assignee: MT Aerospace AG
    Inventors: Helmut Michel, Wulf Radtke, Johannes Hegels
  • Publication number: 20080169383
    Abstract: The invention relates to a support structure for a retractable and extendable flap (12) associated with an object (14), surrounded by a flowing fluid, comprising a shell profile (16) that has a fluid/aerodynamic low-drag form on the outer side and on the inner side forms a chamber (18) for at least partially receiving a device (20) for retracting and extending the flap (12).
    Type: Application
    Filed: August 5, 2004
    Publication date: July 17, 2008
    Applicant: MT Aerospace AG
    Inventors: Aicke Patzelt, Michael Reiprich, Gunther Stegmaier, Wietse Wiglema