Patents by Inventor Antti Aho-Mantila

Antti Aho-Mantila 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).

  • Aircraft wing, fastening arrangement, and intermediate support
    Patent number: 7708224
    Abstract: The invention relates to an aircraft wing, a fastening arrangement, and an intermediate support. A support structure of a wing (1) comprises transverse wing ribs (7a, 7b), between which an intermediate support (10) is arranged for providing a fastening point for a motor (9). The intermediate support comprises a vertical first side part (15a) and a vertical second side part (15b) which are at a distance from one another and connected to one another at their lower part by means of a horizontal bottom part (16) at least at a fastening lug (11). The lug is supported on the bottom part of the intermediate support.
    Type: Grant
    Filed: February 7, 2007
    Date of Patent: May 4, 2010
    Assignee: Patria Aerostructures Oy
    Inventors: Antti Aho-Mantila, Pentti Ahtonen, Juha Halme, Lauri Halme, Mikko Hoffrén, Outi Tervala
  • Pivoting panel for aircraft, and composite support piece
    Patent number: 7631840
    Abstract: A pivoting panel for an aircraft and to a composite support piece for this kind panel. The support piece (17) is arranged as a part of the frame structure of the panel (3). The support piece has an extension portion (23) to which an actuator connection fitting (7) of an actuator (4) can be fastened. The extension portion (23) distributes the forces to the structures of the panel (3).
    Type: Grant
    Filed: June 5, 2006
    Date of Patent: December 15, 2009
    Assignee: Patria Aerostructures Oy
    Inventors: Risto Kallinen, Jani Korpimäki, Jussi Linjama, Antti Aho-Mantila, Pentti Ahtonen
  • Aircraft wing, fastening arrangement, and intermediate support
    Publication number: 20090212154
    Abstract: The invention relates to an aircraft wing, a fastening arrangement, and an intermediate support. A support structure of a wing (1) comprises transverse wing ribs (7a, 7b), between which an intermediate support (10) is arranged for providing a fastening point for a motor (9). The intermediate support comprises a vertical first side part (15a) and a vertical second side part (15b) which are at a distance from one another and connected to one another at their lower part by means of a horizontal bottom part (16) at least at a fastening lug (11). The lug is supported on the bottom part of the intermediate support.
    Type: Application
    Filed: February 7, 2007
    Publication date: August 27, 2009
    Inventors: Antti Aho-Mantila, Pentti Ahtonen, Juha Halme, Lauri Halme, Mikko Hoffren, Outi Tervala
  • Pivoting panel for aircraft, and composite support piece
    Publication number: 20090072090
    Abstract: A pivoting panel for an aircraft and to a composite support piece for this kind panel. The support piece (17) is arranged as a part of the frame structure of the panel (3). The support piece has an extension portion (23) to which an actuator connection fitting (7) of an actuator (4) can be fastened. The extension portion (23) distributes the forces to the structures of the panel (3).
    Type: Application
    Filed: June 5, 2006
    Publication date: March 19, 2009
    Inventors: Risto Kallinen, Jani Korpimaki, Jussi Linjama, Antti Aho-Mantila, Pentti Ahtonen