METHOD OF ASSESSING EFFECT OF AIR ON DAMPING STRUCTURAL VIBRATIONS Russian patent published in 2020 - IPC G01M9/06 G01M10/00 

Abstract RU 2737031 C1

FIELD: astronautics.

SUBSTANCE: invention relates to ground-based dynamic tests of space structures, for example, panels of solar panels and antenna reflectors. Method consists in hanging structures in a liquid medium, establishing an oscillation measurement system. At that said structures are pre-made in the form of scaling models, the scale of which corresponds to the damping of model oscillations in liquid medium damping oscillations of nature in air. Then, deviation of the model from the equilibrium position realizes the mode of free oscillations, by attenuation of which the damping characteristics of the oscillations of the model are determined, then scale models of structures are hung on elastic suspension in vacuum chamber and characteristics of damping by damped free oscillations of scaled models of structures in vacuum chamber are determined. Thereafter, the effect of the air medium on the damping of structural vibrations is evaluated by comparing damping characteristics obtained on scale models in a liquid medium with such characteristics obtained in a vacuum chamber.

EFFECT: technical result consists in simplification of experiment, reduction of time costs for conducting research.

1 cl, 3 dwg, 1 tbl

Similar patents RU2737031C1

Title Year Author Number
FRICTIONAL UNIT TEST TECHNIQUE 2006
  • Shapovalov Vladimir Vladimirovich
  • Chelokh'Jan Aleksandr Vartanovich
  • Lubjagov Aleksandr Mikhajlovich
  • Vorob'Ev Vladimir Borisovich
  • Shcherbak Petr Nikolaevich
  • Ozjabkin Andrej L'Vovich
  • Mogilevskij Viktor Anatol'Evich
  • Okulova Ekaterina Stanislavovna
  • Shub Mikhail Borisovich
  • Butov Ehduard Solomonovich
  • Kikichev Shamil' Vladimirovich
  • Zajkin Denis Sergeevich
  • Rodin Aleksandr Evgen'Evich
  • Konovalov Dmitrij Sergeevich
  • Aleksandrov Anatolij Aleksandrovich
  • Kharlamov Pavel Viktorovich
  • Voronin Vladimir Nikolaevich
  • Shaposhnikov Igor' Aleksandrovich
RU2343450C2
METHOD FOR DYNAMIC MONITORING OF HIGH MOBILE NON-LINEAR TECHNICAL SYSTEMS 2020
  • Kolesnikov Vladimir Ivanovich
  • Shapovalov Vladimir Vladimirovich
  • Kolesnikov Igor Vladimirovich
  • Novikov Evgenij Sergeevich
  • Ozyabkin Andrej Lvovich
  • Manturov Dmitrij Sergeevich
  • Kornienko Roman Andreevich
  • Mishchinenko Vasilij Borisovich
  • Shestakov Mikhail Mikhajlovich
  • Kharlamov Pavel Viktorovich
  • Burakova Marina Andreevna
  • Petrik Andrej Mikhajlovich
  • Ryabysh Denis Alekseevich
  • Fejzov Emin Eldarovich
  • Fejzova Valentina Aleksandrovna
  • Sangin Dzhasur Yakubovich
  • Koropets Petr Alekseevich
RU2745382C1
DEVICE FOR INVESTIGATING AEROELASTICITY OF HIGH BUILDING STRUCTURES 0
  • Belov Mikhail Dmitrievich
  • Bychkov Pavel Aleksandrovich
SU866430A1
METHOD OF ANALYZING PARAMETERS OF STRESS-STRAIN STATE OF ELASTIC OBJECTS 2018
  • Volokhov Grigorij Mikhajlovich
  • Gasyuk Aleksandr Sergeevich
  • Ovechnikov Mikhail Nikolaevich
  • Chunin Sergej Vladimirovich
  • Shabunevich Andrej Viktorovich
  • Shabunevich Viktor Ivanovich
RU2686870C1
CENTRIFUGAL PUMP DESIGN METHOD 2013
  • Kushnarev Vladimir Ivanovich
  • Kushnarev Ivan Vladimirovich
  • Oboznyj Jurij Sergeevich
RU2542160C1
METHOD OF SELECTION OF CONSTRUCTION OF CARRIER BUOY FOR SELF-CONTAINED BUOY STATION IN ACCORDANCE WITH DESIGN ASSIGNMENT 2006
  • Smirnov Gennadij Vasil'Evich
RU2321519C2
METHOD OF DETERMINATION OF THE CONTROL SIGNAL ON THE CORNER OF THE ROLL MODEL OF THE HYPERPOWER VEHICLE EQUIPMENT (HVE) FOR MONITORING THE AERODYNAMIC IDENTITY ON THE REINOLDS NUMBER OF TRAJECTORIES OF THE FLIGHT OF THE MODEL AND THE NUCLEAR ARTICLE WHEN CONDUCTING ANTI-STATE AIRCRAFT RESEARCH 2016
  • Lovitskij Lavrentij Lavrentevich
  • Sadrtdinov Vladislav Diyasovich
RU2615220C1
METHOD AND DEVICE FOR DETERMINATION OF AIRCRAFT AERODYNAMICS 2013
  • Moshkin Igor' Jur'Evich
  • Zhabotinskij Anatolij Danilovich
  • Kabanov Jurij Pavlovich
  • Pegov Valentin Ivanovich
  • Khlybov Vladimir Il'Ich
RU2561829C2
DEVICE FOR MODELLING EFFECT OF EXCAVATING EXPLOSION 0
  • Dyadyushko Viktor Romanovich
  • Zayarnyuk Vitalij Andreevich
  • Kireev Yurij Nikolaevich
  • Kovrigin Sergej Aleksandrovich
SU1730449A1
METHOD OF MODELING STRESSED-DEFORMED STATE IN AVIATION PANEL 2003
  • Baburchenkov M.F.
  • Borodachev Nikolaj Maksimovich
RU2243525C1

RU 2 737 031 C1

Authors

Berns Vladimir Andreevich

Lushin Viktor Nikolaevich

Marinin Dmitrij Aleksandrovich

Dates

2020-11-24Published

2019-11-11Filed