Patents by Inventor Frederick Tischhauser

Frederick Tischhauser 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: 20220247006
    Abstract: Methods and apparatus for thermal management of batteries are disclosed herein. An example battery disclosed herein includes a housing defining a cavity and a battery cell disposed in the cavity of the housing. The battery cell has a terminal. The battery further includes a bus bar disposed in the cavity of the housing. The bus bar is coupled to the terminal. A fluid channel formed in the bus bar. The fluid channel is to receive a cooling fluid to cool the bus bar and reduce a temperature of the battery.
    Type: Application
    Filed: December 16, 2021
    Publication date: August 4, 2022
    Inventors: Tim Moser, Frederick Tischhauser
  • Patent number: 11332238
    Abstract: There is provided an energy absorbing landing gear system for attachment to a vertical landing apparatus. The energy absorbing landing gear system includes a linear damper assembly, and a load limiter assembly coupled to the linear damper assembly, the load limiter assembly having at least one deformable element to enhance an energy absorption capability. When the energy absorbing landing gear system is attached to the vertical landing apparatus, during a landing phase, the linear damper assembly contacts a landing surface, and a piston assembly of the linear damper assembly moves a first compression distance toward the load limiter assembly, and when the linear damper assembly reaches a maximum compression, the linear damper assembly moves a second compression distance into the load limiter assembly, and the at least one deformable element deforms.
    Type: Grant
    Filed: March 22, 2020
    Date of Patent: May 17, 2022
    Assignee: Aurora Flight Sciences Corporation
    Inventor: Frederick Tischhauser
  • Publication number: 20210291968
    Abstract: There is provided an energy absorbing landing gear system for attachment to a vertical landing apparatus. The energy absorbing landing gear system includes a linear damper assembly, and a load limiter assembly coupled to the linear damper assembly, the load limiter assembly having at least one deformable element to enhance an energy absorption capability. When the energy absorbing landing gear system is attached to the vertical landing apparatus, during a landing phase, the linear damper assembly contacts a landing surface, and a piston assembly of the linear damper assembly moves a first compression distance toward the load limiter assembly, and when the linear damper assembly reaches a maximum compression, the linear damper assembly moves a second compression distance into the load limiter assembly, and the at least one deformable element deforms.
    Type: Application
    Filed: March 22, 2020
    Publication date: September 23, 2021
    Applicant: Aurora Flight Sciences Corporation, a subsidiary of The Boeing Company
    Inventor: Frederick Tischhauser