Patents by Inventor Frank E. HASHBERGER

Frank E. HASHBERGER 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: 20140152162
    Abstract: An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the movable stowage bin portion in a closed position and unlatches the movable stowage bin portion to an open position. An electrically operated stowage bin activation switch operates the stowage bin latch mechanism, allowing the aircraft stowage bins to be locked by independently controlling the overhead stowage bins through the aircraft cabin management system, or by control of the latch by the stowage bin activation switch.
    Type: Application
    Filed: February 7, 2014
    Publication date: June 5, 2014
    Applicant: BE Intellectual Property, Inc.
    Inventors: Frank E. Hashberger, Clarence Ivester
  • Publication number: 20140091178
    Abstract: An aircraft lavatory comprising an enclosure having a door, a first side wall, a rear wall, a ceiling, and a second side wall, wherein the second side wall includes a sink, the second side wall defining a plane and wherein the sink is inwardly disposed from said plane. To create space for a stowage compartment, an additional side wall parallel to, and adjacent to, said second side wall is formed. This space houses a stowage compartment accessible from outside said lavatory, the stowage compartment formed between said second side wall and said additional wall.
    Type: Application
    Filed: September 25, 2013
    Publication date: April 3, 2014
    Applicant: B/E Aerospace, Inc.
    Inventors: James C. Grieve, William J. Banfield, Frank E. Hashberger
  • Patent number: 8665119
    Abstract: An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the movable stowage bin portion in a closed position and unlatches the movable stowage bin portion to an open position. An electrically operated stowage bin activation switch operates the stowage bin latch mechanism, allowing the aircraft stowage bins to be locked by independently controlling the overhead stowage bins through the aircraft cabin management system, or by control of the latch by the stowage bin activation switch.
    Type: Grant
    Filed: April 18, 2011
    Date of Patent: March 4, 2014
    Assignee: BE Intellectual Property, Inc.
    Inventors: Frank E. Hashberger, Clarence Ivester
  • Publication number: 20110254705
    Abstract: An electrically activated latch for aircraft stowage bins includes an overhead stowage bin module having a stationary support structure and a movable stowage bin portion. An electrically operated stowage bin latch mechanism latches the movable stowage bin portion in a closed position and unlatches the movable stowage bin portion to an open position. An electrically operated stowage bin activation switch operates the stowage bin latch mechanism, allowing the aircraft stowage bins to be locked by independently controlling the overhead stowage bins through the aircraft cabin management system, or by control of the latch by the stowage bin activation switch.
    Type: Application
    Filed: April 18, 2011
    Publication date: October 20, 2011
    Applicant: BE INTELLECTUAL PROPERTY, INC.
    Inventors: Frank E. HASHBERGER, Clarence IVESTER
  • Publication number: 20110253836
    Abstract: An aircraft overhead luggage bin module includes a stowage bin assembly, an integral light assembly providing structural stiffness to an upper portion of the stowage bin assembly. The stowage bin assembly includes an air distribution plenum that also transmits loads to mounting structures, an upper air diffuser connected to the air distribution plenum, and an optional lower sidewall diffuser connected to the air distribution plenum.
    Type: Application
    Filed: April 18, 2011
    Publication date: October 20, 2011
    Applicant: BE INTELLECTUAL PROPERTY, INC.
    Inventor: Frank E. HASHBERGER
  • Publication number: 20110255296
    Abstract: An aircraft ceiling module includes a ceiling panel with integrated lighting, valences and wiring. LED lighting units are mounted directly to the ceiling panel, and one or more valence panels are connected to the ceiling panel to shield the LED lighting units. The valence panels are integral to the ceiling panel, and provide structural stiffness to overall construction of the ceiling module. Wiring connected to the LED lighting units is integrated into the ceiling panel.
    Type: Application
    Filed: April 18, 2011
    Publication date: October 20, 2011
    Applicant: BE INTELLECTUAL PROPERTY, INC.
    Inventors: Frank E. HASHBERGER, Sylvio A. C. BRAVETTI
  • Publication number: 20110256821
    Abstract: An interior ceiling panel system includes a ceiling panel mounted in a ceiling area, a first airflow directing panel in a first side of the ceiling area defining an airflow passage, and a second airflow directing panel in a second side of the ceiling area, defining an eddy space. An airflow supply source introduces airflow into the ceiling area, and the second airflow directing panel provides an obstruction that creates an eddy in the eddy space that incoming airflow with air in the cabin. One or more speakers project sound energy upward toward the ceiling panel, which deflects sound energy to provide more uniform sound levels in the cabin.
    Type: Application
    Filed: April 18, 2011
    Publication date: October 20, 2011
    Applicant: BE INTELLECTUAL PROPERTY, INC.
    Inventors: Frank E. HASHBERGER, Sylvio A.C. BRAVETTI