Patents by Inventor Vladimir Alekseevich Golovkin

Vladimir Alekseevich Golovkin 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).

  • Patent number: 6901814
    Abstract: Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.
    Type: Grant
    Filed: May 30, 2003
    Date of Patent: June 7, 2005
    Assignees: Nord-Micro Elektronik Feinmechanik
    Inventors: Yevgeny Semenovich Vozhdaev, Heinz-Gerhard Kohler, Mikhail Alekseevich Golovkin, Vladimir Alekseevich Golovkin, Aleksandr Aleksandrovich Nikolsky, Andrei Aleksandrovich Efremov, Valentin Ivanovich Guskov
  • Patent number: 6813942
    Abstract: A Pitot-Static tube including three groups of orifices for determining the total pressure, static pressure and angle of attack, an axially symmetric body and a strut for fastening to pneumatic paths arranged between them and to electric heating elements. In order to reduce the aerodynamic drag of the Pitot-Static tube and the power required for heating the anti-icing system, the orifices for measuring the static pressure are arranged on a plate upstream of the strut.
    Type: Grant
    Filed: May 2, 2002
    Date of Patent: November 9, 2004
    Assignees: Professor N.E. Zhukovsky Central Aerohydrodynamic Institute, Aeropribor Voskhod, Nord-Micro Elektronik Feinmechanick AG
    Inventors: Yevgeny Semenovich Vozhdaev, Heinz-Gerhard Kohler, Mikhail Alekseevich Golovkin, Vladimir Alekseevich Golovkin, Anatoli Kuzmich Pankratov, Andrei Aleksandrovich Efenov
  • Publication number: 20040007080
    Abstract: Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.
    Type: Application
    Filed: May 30, 2003
    Publication date: January 15, 2004
    Applicants: Aeropribor Voskhod, Nord-Micro Elektronick, Professor N.E. Zhukovsky
    Inventors: Yevgeny Semenovich Vozhdaev, Heinz-Gerhard Kohler, Mikhail Alekseevich Golovkin, Vladimir Alekseevich Golovkin, Aleksandr Aleksandrovich Nikolsky, Andrei Aleksandrovich Efremov, Valentin Ivanovich Guskov
  • Patent number: 6588285
    Abstract: The invention relates to a fuselage Pitot-static tube comprising three groups of orifices for determining the total pressure (2), static pressure (3) and angle of attack (6, 7), and an axisymmetric body (1) and strut (5) for mounting an anti-icing system having, arranged between them, airways (10) and electric heating elements (8). The orifices for determining the angle of attack are arranged on the strut, whose cross section is constructed in the form of a subsonic aerodynamic profile with a rounded-off nose or a tapered nose, and are arranged between the nose of the profile and the position of its maximum thickness.
    Type: Grant
    Filed: September 24, 1999
    Date of Patent: July 8, 2003
    Assignees: Nord-Micro Elektronik Feinmechanik AG, Voskhod, Aeropribor
    Inventors: Yevgeny Semenovich Vozhdaev, Heinz-Gerhard Kohler, Mikhail Alekseevich Golovkin, Vladimir Alekseevich Golovkin, Aleksandr Aleksandrovich Nikolsky, Andrei Aleksandrovich Efremov, Valentin Ivanovich Guskov