Patents by Inventor Vyacheslav Nikolaevich Nikitin

Vyacheslav Nikolaevich Nikitin 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).

  • LIGHT MULTI-PURPOSE AIRCRAFT WITH A CONTROLLING INTEGRATED COMPLEX
    Publication number: 20100030402
    Abstract: A light multi-purpose aircraft with a controlling integrated complex comprises a fuselage (1); a wing (2); a fin assembly (3); a landing gear (4); a power plant (5); a radio inertial navigation and landing complex; an integrated electronic display system; a complex emergency escape system; an objective monitoring system; a complex control system; a general-purpose aircraft equipment system; a crest-of-helmet target indication system; a speech information control system; a data input system; control panels; an on-board communication complex; on-board maintenance panels; and also a controlling integrated complex (6) incorporating an on-board digital computer system (7); an information exchange system composed of multiplexer and radial channels; and systems and/or units for interfacing with all functional complexes and systems of the aircraft in which the on-board digital computer system (7), through corresponding interfacing systems and/or units, is connected by multiplexer channels with the aircraft systems, i
    Type: Application
    Filed: December 25, 2006
    Publication date: February 4, 2010
    Inventors: Oleg Fedorovich Demchenko, Nikolai Nikolaevich Dolzhenkov, Konstantin Fedorovich Popovich, Vladimir Petrovich Shkolin, Arkady Iosifovich Gurtovoi, Vladimir Grigorievich Kuznetsov, Vyacheslav Nikolaevich Nikitin, Valery Grigorievich Kodola
  • LIGHT MULTIPURPOSE AIRCRAFT
    Publication number: 20100012767
    Abstract: A light multi-purpose aircraft comprises a fuselage (1); a wing (2); a fin assembly (3); a landing gear (4); a main power plant (5); an auxiliary power plant (7); pylons (10); outboard suspension objects (9) arranged on the undersurface and at the ends of the wing (2); at least one outboard suspension object (9) being arranged on the undersurface of the wing (2) and at least one outboard suspension object (9) being arranged at each end of the wing (2); a gun mount (8) or a guidance and tracking mount arranged in the lower part of the fuselage (1); a controlling integrated complex of airborne electronic equipment (17) with an electric power supply system (16) and an armament control complex (19) incorporating an on-board electronic guidance and tracking system (20); a defense system (21); a multi-purpose control panel (22); a group interaction system (23); an armament control system (24) which are related to each other and to the controlling integrated complex of airborne electronic equipment (17) through a mu
    Type: Application
    Filed: December 25, 2006
    Publication date: January 21, 2010
    Inventors: Oleg Fedorovich Demchenko, Nikolai Nikolaevich Dolzhenkov, Konstantin Fedorovich Popovich, Vladimir Petrovich Shkolin, Arkady Iosifovich Gurtovoi, Vladimir Grigorievich Kuznetsov, Vyacheslav Nikolaevich Nikitin, Vyacheslav Mikhailovich Ilin, Viktor Lavrentievich Bozhanov, Valery Grigorievich Kodola