Patents by Inventor Nikolai Nikolaevich Dolzhenkov

Nikolai Nikolaevich Dolzhenkov 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: 20100327112
    Abstract: A light multi-purpose aircraft comprises a fuselage 1; a wing 2; a fin assembly 3; a landing gear 4; main and auxiliary power plants 5; a crew protection system; an integrated complex for controlling a general-purpose aircraft equipment which is engaged through a multiplexer channel with a set of on-board digital computers, electronic control systems of port and starboard engines, a recording and monitoring system, a guidance and landing equipment, a complex control system and is engaged through code communication lines with a fuel control and monitoring system, a voice message equipment, a complex electron display system, characterized in that the crew protection system is made in the form of a multilayer screen of auxiliary and main equipment configured in order of increasing its significance farther and farther away from the shell and load-bearing elements of the fuselage 1; the greatest component density is ensured with due regard for the most likely zones and aspect angles of injury: ˜30° with respect to
    Type: Application
    Filed: July 11, 2007
    Publication date: December 30, 2010
    Inventors: Oleg Fedorovich Demchenko, Nikolai Nikolaevich Dolzhenkov, Konstantin Fedorovich Popovich, Vladimir Petrovich Shkolin, Vitaly Jurievich Naryshkin, Valery Grigorievich Kodola, Georgy Aleksandrovich Fedotov
  • Publication number: 20100133388
    Abstract: An aircraft (1) at enhanced maneuvering properties comprising a fuselage, a wing, a fin assembly, a landing gear, a power plant, a multi-purpose integrated electronic complex (3), incorporating an information exchange system, a set of on-board digital computers (19) for controlling flight and training and combat operations, an external storage and an information input system, a radio inertial navigation and landing system, a complex aircraft control system, an armament control system, a complex system for electronic display, control and sighting, an emergency warning board, a general-purpose aircraft equipment control system, an on-board objective monitoring system, a speech information control system, an electric power supply system, external and internal lighting facilities, a complex emergency escape system, an electronic power plant control system, characterized in that an optoelectronic vision-sight system (5) comprises an automatic caging system (31) that fixes orientation of visual fields of a laser ra
    Type: Application
    Filed: July 11, 2007
    Publication date: June 3, 2010
    Inventors: Oleg Fedorovich Demchenko, Nikolai Nikolaevich Dolzhenkov, Konstantin Fedorovich Popovich, Vladimir Petrovich Shkolin, Arkady Iosifovich Gurtovoi, Valery Grigorievich Kodola, Vyacheslav Georgievich Kalugin, Kirill Veniaminovich Obrosov
  • 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
  • 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