Patents by Inventor Manfred Kornrumpf

Manfred Kornrumpf 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: 20070181537
    Abstract: A device for connecting two elements by shrinking a shrink tube includes a heating element and a control unit. The heating element is adapted for providing thermal or inductive energy and is further adapted such that with it a shrink tube, which can be pulled onto a connection region of two elements to be connected, can be encased along at least part of the circumference of the shrink tube. The control unit is adapted for supplying electrical energy to the heating element and furthermore is adapted such that with it the temperature of the heating element is controllable such that, by shrinking the shrink tube, the two elements are connectable.
    Type: Application
    Filed: August 9, 2005
    Publication date: August 9, 2007
    Applicant: Airbus Deutschland GmbH
    Inventor: Manfred Kornrumpf
  • Publication number: 20060027536
    Abstract: A device for connecting two elements by shrinking a shrink tube includes a heating element and a control unit. The heating element is adapted for providing thermal or inductive energy and is further adapted such that with it a shrink tube, which can be pulled onto a connection region of two elements to be connected, can be encased along at least part of the circumference of the shrink tube. The control unit is adapted for supplying electrical energy to the heating element and furthermore is adapted such that with it the temperature of the heating element is controllable such that, by shrinking the shrink tube, the two elements are connectable.
    Type: Application
    Filed: August 9, 2005
    Publication date: February 9, 2006
    Applicant: Airbus Deutschland GmbH
    Inventor: Manfred Kornrumpf
  • Patent number: 6843515
    Abstract: A cooling system in an aircraft has fluid flow pipe sections that are mounted to the aircraft structure. The pipe sections have pipe ends that form part of pipe junctions. The two pipe ends of a pipe junction are facing each other and are surrounded by a shrunk hose member of a shrinkable material which overlaps both pipe ends in a fluid- and pressure-tight manner.
    Type: Grant
    Filed: September 6, 2002
    Date of Patent: January 18, 2005
    Assignee: Airbus Deutschland GmbH
    Inventor: Manfred Kornrumpf
  • Publication number: 20030057290
    Abstract: A cooling system in an aircraft has fluid flow pipe sections that are mounted to the aircraft structure. The pipe sections have pipe ends that form part of pipe junctions. The two pipe ends of a pipe junction are facing each other and are surrounded by a shrunk hose member of a shrinkable material which overlaps both pipe ends in a fluid- and pressure-tight manner.
    Type: Application
    Filed: September 6, 2002
    Publication date: March 27, 2003
    Inventor: Manfred Kornrumpf