VERTICAL TAKEOFF AND LANDING FLYING VEHICLE Russian patent published in 1997 - IPC

Abstract RU 2093422 C1

FIELD: aviation. SUBSTANCE: wing 9 is made according to biplane lay-out; engines with propellers 11 are rigidly mounted between upper and lower panels on pylons 10. Wing is movable along fuselage. EFFECT: enhanced reliability. 4 dwg

Similar patents RU2093422C1

Title Year Author Number
CARRIER HELICOPTER-AMPHIBIOUS AIRCRAFT 2017
  • Durov Dmitrij Sergeevich
RU2658739C1
HIGH-SPEED HELICOPTER WITH PROPULSION-STEERING SYSTEM 2016
  • Durov Dmitrij Sergeevich
RU2629478C2
UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING AND METHOD OF MANUFACTURING THEREOF 2023
  • Vruchtel Vilyam Markisovich
  • Onuprienko Aleksandr Vitalevich
  • Bajderyakov Sergej Vasilevich
RU2819460C1
AMPHIBIOUS CONVERTIBLE HELICOPTER 2005
  • Durov D.S.
RU2310583C2
UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT 2016
  • Durov Dmitrij Sergeevich
RU2627975C2
MULTI-MODE GROUND-EFFECT VEHICLE - AIRPLANE 2019
  • Bolshakov Anton Vladimirovich
  • Gavrilov Nikolaj Fedorovich
  • Kondratev Vyacheslav Petrovich
  • Pronichev Vladimir Egorovich
RU2719993C1
AMPHIBIOUS WITH INCREASED CARRYING CAPACITY 2020
  • Shchelochkov Matvej Anatolevich
  • Seleznev Sergej Viktorovich
  • Galimov Rinat Minakhmetovich
RU2739451C1
HIGH-SPEED TURBOFAN COMBINED HELICOPTER 2016
  • Durov Dmitrij Sergeevich
RU2629475C1
MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING 2019
  • Papiashvili Shota Georgievich
  • Klochkov Dmitrij Vyacheslavovich
  • Ratnikov Kirill Vladimirovich
RU2714176C1
FAST-SPEED CONVERTIBLE COMPOUND HELICOPTER 2015
  • Durov Dmitrij Sergeevich
RU2609856C1

RU 2 093 422 C1

Authors

Safronov Venidikt Pavlovich

Dates

1997-10-20Published

1994-02-08Filed