CONTROL OVER AIRCRAFT EQUIPPED WITH ENGINE WITH JET NOZZLES Russian patent published in 2015 - IPC B64C15/00 

Abstract RU 2570745 C2

FIELD: aircraft engineering.

SUBSTANCE: this control method consists fitting at least three jet nozzles at aircraft airframe bottom edge and in intermittent feed of spoiler ailerons by push-and-pull drive to gas jet of jet nozzle adjacent spoiler gas jet. At least three spoilers are used for control over aircraft arranged between different adjacent jet nozzles. Said push-and-pull drive feed intermittently every spoiler to whatever jet nozzle gas jet adjacent to spoiler.

EFFECT: higher efficiency of aircraft roll control.

7 dwg

Similar patents RU2570745C2

Title Year Author Number
CONTROL OVER AIRCRAFT EQUIPPED WITH ENGINE WITH JET NOZZLES 2014
  • Erakhtin Mikhail Mikhajlovich
  • Mishchenko Anatolij Petrovich
  • Semenenko Jurij Nikolaevich
  • Chernov Leonid Aleksandrovich
RU2570743C2
AIRBORNE VEHICLE 2014
  • Erakhtin Mikhail Mikhajlovich
  • Mishchenko Anatolij Petrovich
  • Semenenko Jurij Nikolaevich
  • Chernov Leonid Aleksandrovich
RU2555085C1
DEVICE AND METHOD FOR CONTROL OF SPACE VEHICLE LANDING 1994
  • Burdakov V.P.
  • Kanaev A.I.
RU2097286C1
JET ENGINE THRUST VECTOR CONTROL DEVICE 2012
  • Aleksenko Mikhail Nikitovich
RU2527798C2
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
NOZZLE 2022
  • Novikov Igor Evgenevich
RU2791932C1
GYRATING ROCKET STAGE WITH COMBINED POWER PLANT AND METHOD OF CONTROLLING ROCKET FLIGHT 2010
  • Aliev Ali Vejsovich
  • Loshkarev Anatolij Nikolaevich
  • Sermjagin Konstantin Viktorovich
  • Mironov Andrej Nikolaevich
RU2427507C1
DOUBLE-FLOW TURBOJET ENGINE NOZZLES SYSTEM 2018
  • Arutyunov Artem Georgievich
  • Arutyunov Artur Georgievich
  • Dubinin Viktor Vitalevich
RU2716651C2
DISC AIRCRAFT OF KRISHTOP (DAK), HYBRID POWER PLANT (HPP) FOR DAK AND METHOD OF FUNCTION FOR DAK WITH HPP (VERSIONS) 2019
  • Krishtop Anatolij Mikhajlovich
RU2714553C1
SPACECRAFT ENGINE OPERATION METHOD 2021
  • Sattarov Albert Gabdulbarovich
  • Sochnev Aleksandr Vladimirovich
  • Ziganshin Bulat Rustemovich
RU2757615C1

RU 2 570 745 C2

Authors

Erakhtin Mikhail Mikhajlovich

Mishchenko Anatolij Petrovich

Semenenko Jurij Nikolaevich

Chernov Leonid Aleksandrovich

Dates

2015-12-10Published

2014-04-17Filed