Patents by Inventor Aleksandr Aleksandrovich Nikolsky

Aleksandr Aleksandrovich Nikolsky 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).

  • Fuselage pitot-static tube
    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
  • Fuselage pitot-static tube
    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
  • Fuselage pitot-static tube and the aerodynamic profile of its strut
    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