Patents by Inventor Christian A. Rogg

Christian A. Rogg 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: 20120199292
    Abstract: A tool for forming a panel including a core area, at which plies sandwich a core, and a trim area surrounding the core, at which the plies are bonded together, is provided and includes a body having a surface on which the panel is formable, the surface including core and trim portions for respective correspondence with locations of the core and trim areas of the panel, a border between the core and trim portions defining a surface feature displaced from a plane of the core portion, a lock disposable proximate to the surface feature to increase a pre-bonding friction between the plies at the surface feature and an assembly to apply bonding pressure to the plies and the lock at least at the core and trim areas.
    Type: Application
    Filed: February 3, 2011
    Publication date: August 9, 2012
    Applicant: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Jonathan Bremmer, Neil W. Cawthra, Christian A. Rogg, Paul H. Denavit, William E. Hovan, III, Robert A. Lacko, Jeffrey G. Sauer
  • Publication number: 20110011518
    Abstract: A thermoplastic matrix airframe structure section includes a multitude of thermoplastic matrix frame members and a multitude of thermoplastic matrix beam members which form a substructure, which receives a thermoplastic matrix inner cap grid structure, a thermoplastic matrix outer cap grid structure, and a thermoplastic matrix skin which are in-situ co-bonded to the substructure to significantly strengthen and unify the substructure.
    Type: Application
    Filed: July 26, 2006
    Publication date: January 20, 2011
    Inventors: Thomas Carstensen, William V. Forster, Christian A. Rogg
  • Patent number: 6739861
    Abstract: The composite molding apparatus includes a rigid base member and a complementary semi-rigid mold member or “black bag” caul plate having a sieve member formed therein. The sieve member layer of the semi-rigid mold member engages pins which extend from the sandwich core to limit penetration into the semi-rigid mold member to a predetermined depth. The semi-rigid mold member is supported relative to the rigid mold member by the pins to provide uniform pressure transfer to the composite article during a high pressure co-cure molding process without crushing the sandwich core.
    Type: Grant
    Filed: November 26, 2001
    Date of Patent: May 25, 2004
    Assignee: Sikorsky Aircraft Corporation
    Inventors: David M. Cournoyer, Neil W. Cawthra, Thomas A. Carstensen, Christian A. Rogg, Michael G. Osiecki
  • Publication number: 20030098520
    Abstract: The composite molding apparatus includes a rigid base member and a complementary semi-rigid mold member or “black bag” caul plate having a sieve member formed therein. The sieve member layer of the semi-rigid mold member engages pins which extend from the sandwich core to limit penetration into the semi-rigid mold member to a predetermined depth. The semi-rigid mold member is supported relative to the rigid mold member by the pins to provide uniform pressure transfer to the composite article during a high pressure co-cure molding process without crushing the sandwich core.
    Type: Application
    Filed: November 26, 2001
    Publication date: May 29, 2003
    Inventors: David M. Cournoyer, Neil W. Cawthra, Thomas A. Carstensen, Christian A. Rogg, Michael G. Osiecki