METHOD OF GENERATION OF LIFTING FORCE OF AIRCRAFT (VERSIONS) AND AIRCRAFT Russian patent published in 2014 - IPC B64C29/00 

Abstract RU 2531437 C1

FIELD: aviation.

SUBSTANCE: method of generation of lifting force of the aircraft consists in the use of the gas jet emerging from the nozzle of an aircraft jet engine, supplied to the bearing device equipped with the gas duct in which the disconnector and the lifting elements are mounted. When the gas flow passes from engine the lifting force is generated due to the change in the direction of gas movement in the lifting elements. The device for implementing the said method of generation of lifting force comprises an aircraft with the jet engine and the bearing device with the gas duct. In with the gas duct one or more lifting elements are mounted, made in the form of elongated combs, straight or curved in the direction of movement of the gas flow, and the bending of the lifting elements is made such as to generate a lifting force acting on the bearing device through the lifting elements. The bearing element is provided with a disconnector of the gas flow, mounted in the gas duct.

EFFECT: increase in the lifting force, reduction of fuel consumption and increase in the range and speed of flight.

4 cl, 8 dwg

Similar patents RU2531437C1

Title Year Author Number
INTEGRATED TECHNOLOGY OF OPERATION AND PRODUCTION "MAXINIO" TRANSPORT FACILITIES: VTOL ELECTRIC AIRCRAFT (VERSIONS), ELECTRIC AIRCRAFT UNITS AND METHODS OF EMPLOYMENT ELECTRIC AIRCRAFT AND ITS PARTS 2010
  • Maksimov Nikolaj Ivanovich
RU2466908C2
VTOL AIRCRAFT 2014
  • Artamonov Aleksandr Sergeevich
  • Artamonov Evgenij Aleksandrovich
RU2546385C1
COMBINED AIRCRAFT WING 2013
  • Koshkarev Dmitry Georgievich
RU2626773C1
METHOD OF CREATING AIRCRAFT LIFT (VERSIONS), METHOD OF FLIGHT, NON-AERODYNAMIC ALL-WEATHER VTOL AIRCRAFT "MAXINIO" (VERSIONS), METHODS OF TAKE-OFF AND LANDING, AICRAFT CONTROL METHOD AND SYSTEM, FUSELAGE, WING (VERSIONS), THRUST REVERSE AND METHOD OF ITS OPERATION, LANDING GEAR SYSTEM, GAS SEPARATION AND DISTRIBUTION SYSTEM 2007
  • Maksimov Nikolaj Ivanovich
RU2349505C1
DEVELOPMENT OF VTOL AIRCRAFT DRIVE FORCES AND AIRCRAFT TO THIS END 2012
  • Ambrozhevich Aleksandr Vladimirovich
  • Migalin Konstantin Valentinovich
  • Sereda Vladislav Aleksandrovich
  • Grishchenko Aleksandr Vladimirovich
  • Silevich Vladimir Jur'Evich
  • Sidenko Aleksej Il'Ich
RU2531432C2
AIRCRAFT 2007
  • Bykovskij Sergej Ivanovich
  • Pavlov Viktor Andreevich
RU2378156C2
FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS 2010
  • Maksimov Nikolaj Ivanovich
RU2466061C2
METHOD FOR INCREASING AIRCRAFT WING LIFTING POWER WITH JET PROPULSION OF BYPASS TURBOJET ENGINES (BTJE) WITH CONTOUR DEGREE OF GREATER THAN 2 AND AIRCRAFT USING THIS METHOD (VARIANTS) 2017
  • Sushentsev Boris Nikiforovich
RU2670357C1
VERTICAL TAKE-OFF AND LANDING AIRCRAFT 2014
  • Turchenko Il'Ja Aleksandrovich
RU2574873C1
AIRCRAFT 2018
  • Krovyakov Vladimir Borisovich
  • Korolenko Viktor Vladimirovich
  • Trofimchuk Maksim Vasilevich
  • Andreev Maksim Vladimirovich
  • Kozhevnikov Ilya Aleksandrovich
RU2706760C1

RU 2 531 437 C1

Authors

Popov Ivan Ivanovich

Dates

2014-10-20Published

2013-05-06Filed