METHOD FOR LAUNCHING AND ACCELERATING UNMANNED AERIAL VEHICLES WITH A TURBOJET ENGINE AND A DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2022 - IPC F41F1/06 F41F3/42 B64C39/02 

Abstract RU 2770510 C1

FIELD: rocket technology.

SUBSTANCE: invention relates to rocket technology, and in particular to takeoff and acceleration systems for unmanned aerial vehicles (UAVs). The method consists in launching and accelerating the aircraft to takeoff speed using a mortar method, characterized by opening the aircraft nozzle, starting the aircraft engine, inflating the receiver with the exhaust gases of the aircraft turbojet engine, adjusting the pressure required for starting the pressure reducing valve of the receiver, releasing the wad with the UAV fixed on it by means of a lock-starter mechanism, separating the wad from the UAV and bringing the nozzle of the turbojet engine to its normal state after the latter exits the mortar barrel. The device for implementing the method includes a mortar barrel rigidly mounted on a receiver equipped with a pressure reducing valve, tightly inserted and fixed by a lock-start mechanism located on the mortar barrel, into the wad barrel, on which the tail section is installed and secured with an aircraft lock.

EFFECT: launch of the UAV is carried out "according to the mortar" principle, while the turbojet engine of the aircraft itself is the source of energy.

5 cl, 9 dwg

Similar patents RU2770510C1

Title Year Author Number
AIRCRAFT LAUNCHING CATAPULT 2012
  • Gromov Vladimir Vjacheslavovich
  • Gushchin Konstantin Aleksandrovich
  • Lipsman David Lazorovich
  • Majakin Vladimir Vladimirovich
  • Petrov Igor' Jakovlevich
  • Pikalin Sergej Aleksandrovich
  • Pikin Vadim Anatol'Evich
  • Tonkachev Vladimir Viktorovich
  • Chernous Timofej Aleksandrovich
RU2497725C1
MOBILE COMPLEX FOR RAILWAY INSPECTION 2021
  • Sergeev Arkadij Anatolevich
  • Kochanov Rodion Andreevich
  • Kotov Maksim Alekseevich
  • Lomov Valerij Alekseevich
RU2759363C1
LAUNCH DEVICE 2021
  • Sysoev Sergej Nikolaevich
  • Cherkasov Yurij Vladimirovich
  • Fedin Aleksandr Viktorovich
  • Fedina Mariya Aleksandrovna
RU2771300C1
PISTON INTERNAL COMBUSTION ENGINE WITH LINEAR GENERATOR 2023
  • Ponomarenko Gleb Vladimirovich
RU2809423C1
UAV FROM STANDARDIZED PARTS AND ASSEMBLIES AND PRODUCTION METHOD 2023
  • Vruchtel Vilyam Markisovich
  • Onuprienko Aleksandr Vitalevich
  • Bajderyakov Sergej Vasilevich
RU2812011C1
PNEUMATIC HYDRAULIC CATAPULT 2019
  • Migalin Konstantin Valentinovich
  • Sidenko Kirill Alekseevich
  • Sidenko Aleksej Ilich
  • Migalin Kirill Konstantinovich
RU2721215C1
AIRCRAFT CATAPULT TAKEOFF METHOD AND AIRCRAFT TAKEOFF CATAPULT 2007
  • Baranov Sergej Konstantinovich
  • Targamadze Revaz Cholaevich
  • Moisheev Aleksandr Aleksandrovich
  • Douletov Igor' Il'Jasovich
RU2344971C1
DRONE, ITS VIDEO CONTROL HARDWARE AND CATAPULT LAUNCHER (VERSIONS) 2010
  • Kornushenko Aleksandr Vjacheslavich
  • Serokhvostov Sergej Vladimirovich
  • Zubarev Aleksandr Nikolaevich
  • Kudrjavtsev Oleg Valentinovich
  • Bagdasarjan Ehduard Garikovich
  • Kamyshova Tat'Jana Jur'Evna
RU2466909C2
CATAPULT FOR AIRCRAFT TAKEOFF 2022
  • Sysoev Sergej Nikolaevich
RU2789905C1
REUSABLE UNMANNED AERIAL VEHICLE IN A LAUNCHING CONTAINER AND A METHOD FOR LAUNCHING A REUSABLE UNMANNED AERIAL VEHICLE FROM A TRANSPORT LAUNCHING CONTAINER 2019
  • Leonov Aleksandr Georgievich
  • Zimin Sergej Nikolaevich
  • Izmalkin Oleg Sergeevich
  • Asaturov Sergej Mikhajeli
RU2714616C1

RU 2 770 510 C1

Authors

Ponomarenko Gleb Vladimirovich

Dates

2022-04-18Published

2021-04-30Filed