AIRCRAFT PROPULSOR Russian patent published in 1997 - IPC

Abstract RU 2094326 C1

FIELD: modification of aircraft with turbojet engines located in wing. SUBSTANCE: engines are mounted in wing with turbine forward in way of flight and with compressor backwards counter-flight. Engines are provided with additional slotted air intakes made in rear portion of wing underneath along trailing edge and slotted outlet nozzles located at the top along leading edge of wing. EFFECT: improved aerodynamic characteristics of wing and enhanced economical efficiency of aircraft. 2 dwg

Similar patents RU2094326C1

Title	Year	Author	Number
AIRCRAFT	1998	Duchenko A.L.	RU2134649C1
PROPULSOR	1997	Duchenko Nikolaj Aleksandrovich	RU2120396C1
AIRPLANE	1990	Duchenko Aleksandr Lazarevich	RU2010744C1
HELICOPTER	1993	Duchenko Aleksandr Lazarevich	RU2089455C1
SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL	2018	Sychev Vladimir Borisovich Ambrozhevich Aleksandr Vladimirovich Pshichenko Dmitrij Viktorovich Kartashev Andrej Sergeevich Kornev Aleksej Vladimirovich Sereda Vladislav Aleksandrovich Karavaev Nikolaj Andreevich Sychev Sergej Vladimirovich Kulikov Boris Mikhajlovich Grishchenko Aleksandr Vladimirovich Migalin Konstantin Valentinovich Sidenko Aleksej Ilich Karavaev Nikolaj Andreevich Sychev Sergej Vladimirovich Kulikov Boris Mikhajlovich Grishchenko Aleksandr Vladimirovich Migalin Konstantin Valentinovich Sidenko Aleksej Ilich	RU2711633C2
SHORT TAKE-OFF AND LANDING AIRCRAFT WITH GAS-DYNAMIC CONTROL	2018	Sychev Vladimir Borisovich Ambrozhevich Aleksandr Vladimirovich Pshichenko Dmitrij Viktorovich Kartashev Andrej Sergeevich Kornev Aleksej Vladimirovich Karavaev Nikolaj Andreevich Sychev Sergej Vladimirovich Kulikov Boris Mikhajlovich Grishchenko Aleksandr Vladimirovich Migalin Konstantin Valentinovich Sidenko Aleksej Ilich Sereda Vladislav Aleksandrovich	RU2711760C2
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
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
"TAILLESS" FLARECRAFT	2022	Pavlov Gennadij Alekseevich	RU2776632C1
PLANAR NOZZLE WITH CENTRAL BODY	1995	Gorelov G.M. Chikalov V.G. Chistjakov V.A. Reznik V.E. Mikhajlov S.V.	RU2153591C2

RU 2 094 326 C1

Authors

Duchenko Aleksandr Lazarevich

Dates

1997-10-27—Published

1996-03-01—Filed