SYSTEM AND METHOD FOR COMPENSATION OF AIR MASS FLOW FOR AIRBORNE VEHICLES Russian patent published in 2019 - IPC B64C17/00 G05D1/08 B64C13/16 

Abstract RU 2706679 C2

FIELD: aviation.

SUBSTANCE: group of inventions relates to a system and method for compensation of an air mass burst, an airborne aircraft. System comprises a sensor subsystem, an air mass burst signal subsystem configured to output a signal for movement of control surfaces in response to said signal. Method includes detecting at least one parameter of an airborne aircraft using a first sensor arranged near a front portion of an aircraft, outputting a first signal based on said at least one parameter from first sensor, detecting said at least one airborne vehicle parameter by second sensor, outputting a second signal based on said at least one parameter from the second sensor, using the air bursting signal subsystem to generate an airflow burst signal based on analyzing the first and second signals, change of signal of load parameter with the help of burst signal of air mass in response to signal of air mass burst. Aircraft comprises air mass flow compensation system configured to adaptively reduce load as a result of air mass burst affecting airborne aircraft.

EFFECT: providing adaptive load reduction as a result of air mass impact acting on aircraft.

20 cl, 5 dwg

Similar patents RU2706679C2

Title Year Author Number
ADAPTIVE FILTRATION SYSTEM FOR AERODYNAMIC ANGLES OF AIRCRAFT 2017
  • Lo Tszya
RU2735751C2
INTEGRATED AIRCRAFT VORTEX SAFETY SYSTEM 2003
  • Baranov Nikolaj Alekseevich
  • Belotserkovskij Andrej Sergeevich
  • Kanevskij Mikhail Igorevich
  • Pasekunov Igor' Vladimirovich
RU2324953C2
LIGHT MULTIMODE AIRCRAFT 2007
  • Voronkov Jurij Sergeevich
  • Voronkov Oleg Jur'Evich
RU2348568C1
METHOD AND DEVICE FOR CALCULATING CURRENT VALUE OF ANGULAR ATTACKS AND GLIDING OF AERIAL VEHICLE 2016
  • Maksimov Anatolij Konstantinovich
  • Shchitaev Nikolaj Grigorevich
  • Avakyan Aleksandr Anushavanovich
  • Nasenkov Igor Georgievich
RU2663315C2
FLIGHT MEASURING AIR PARAMETERS SYSTEM 2005
  • Vozhdaev Evgenij Semenovich
  • Vjalkov Andrej Viktorovich
  • Golovkin Mikhail Alekseevich
  • Efremov Andrej Aleksandrovich
  • Kravtsov Vladimir Georgievich
  • Nazarov Oleg Ivanovich
  • Djatlov Vjacheslav Nikolaevich
  • Klimov Aleksandr Sergeevich
RU2290646C1
METHOD FOR ENSURING THE VORTEX SAFETY OF AN AIRCRAFT 2021
  • Selvesyuk Nikolaj Ivanovich
  • Golovnev Igor Georgievich
  • Lapshin Kirill Vasilevich
  • Korsun Oleg Nikolaevich
  • Kulchak Aleksej Mikhajlovich
  • Ryabtsev Vladimir Vasilevich
RU2774083C1
SMART CREW SUPPORT SYSTEM 2015
  • Efanov Vasilij Vasilevich
RU2598130C1
INTELLIGENT SYSTEM OF CREW SUPPORT 2013
  • Jakushev Anatolij Fedorovich
  • Jasenok Andrej Vasil'Evich
  • Mineev Mikhail Ivanovich
  • Kalinin Jurij Ivanovich
  • Bolin Vjacheslav Pavlovich
  • Pavlenko Jurij Maksimovich
  • Drozhzhina Anna Jur'Evna
  • Ternovskij Sergej Aleksandrovich
  • Jakushev Vjacheslav Anatol'Evich
  • Musikhina Ol'Ga Anatol'Evna
  • Frolkina Ljudmila Veniaminovna
RU2541902C2
LIGHT SUPERSONIC MULTI-PURPOSE AIRCRAFT 2004
  • Demchenko Oleg Fedorovich
  • Dolzhenkov Nikolaj Nikolaevich
  • Matveev Andrej Ivanovich
  • Popovich Konstantin Fedorovich
  • Gurtovoj Arkadij Iosifovich
  • Shkolin Vladimir Petrovich
  • Kodola Valerij Grigor'Evich
RU2271305C1
AC ACTIVE PROTECTION METHOD AND SYSTEM FOR ITS IMPLEMENTATION (VERSIONS) 2015
  • Shkolin Vladimir Petrovich
  • Popovich Konstantin Fedorovich
  • Levitskij Sergej Vladimirovich
  • Shapiro Nikita Sergeevich
  • Lebedev Vitalij Viktorovich
  • Mikheicheva Anastasiya Sergeevna
RU2601241C2

RU 2 706 679 C2

Authors

Abdel-Motagali Kkhaled

Kajsedo Rafael I.

Dallara Kristofer D.

Kho Aleksandr K.

Nadzhmabadi Klumars

Syu Tsze L.

Strefling Pol K.

Yamasiro Khisako

Dates

2019-11-19Published

2016-03-02Filed