RU2005131770A - METHOD FOR DETERMINING OWN SHAPES OF ELASTIC STRUCTURE - Google Patents

METHOD FOR DETERMINING OWN SHAPES OF ELASTIC STRUCTURE Download PDF

Info

Publication number
RU2005131770A
RU2005131770A RU2005131770/28A RU2005131770A RU2005131770A RU 2005131770 A RU2005131770 A RU 2005131770A RU 2005131770/28 A RU2005131770/28 A RU 2005131770/28A RU 2005131770 A RU2005131770 A RU 2005131770A RU 2005131770 A RU2005131770 A RU 2005131770A
Authority
RU
Russia
Prior art keywords
frequencies
measured
points
natural
determining
Prior art date
Application number
RU2005131770/28A
Other languages
Russian (ru)
Other versions
RU2308687C2 (en
Inventor
Виктор Николаевич Вернигор (RU)
Виктор Николаевич Вернигор
Сергей В чеславович Крюков (RU)
Сергей Вячеславович Крюков
Original Assignee
Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU)
Открытое акционерное общество "Научно-производственное объединение "Сатурн"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU), Открытое акционерное общество "Научно-производственное объединение "Сатурн" filed Critical Открытое акционерное общество "Научно-производственное объединение "Сатурн" (RU)
Priority to RU2005131770/28A priority Critical patent/RU2308687C2/en
Publication of RU2005131770A publication Critical patent/RU2005131770A/en
Application granted granted Critical
Publication of RU2308687C2 publication Critical patent/RU2308687C2/en

Links

Landscapes

  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Claims (1)

Способ определения собственных форм колебаний упругой конструкции в m заданных точках наблюдения Вj (j=1, 2, 3,..., m), при котором измеряют собственные частоты колебаний конструкции, возбуждают конструкцию на нескольких частотах, лежащих вне окрестности собственных частот, выбирают точку наблюдения А, в которой собственные формы колебаний условно принимают равными единице, и измеряют амплитуды изменения параметра наблюдения на каждой из частот возбуждения в каждой из m заданных точек, а также в выбранной точке наблюдения А конструкции, отличающийся тем, что амплитуды изменения параметра наблюдения в каждой из m заданных точек Вj (j=1, 2, 3,..., m) и выбранной точке наблюдения А измеряют одновременно, а значения амплитудных функций
Figure 00000001
,
Figure 00000002
, ...,
Figure 00000003
определяющих собственные формы колебаний конструкции в каждой заданной точке Вj, определяют из условия минимума целевой функции
The method for determining the natural vibration modes of an elastic structure at m given observation points B j (j = 1, 2, 3, ..., m), in which the natural frequencies of the structural vibrations are measured, the structure is excited at several frequencies outside the vicinity of the natural frequencies, choose observation point A, in which the natural modes of vibration are conventionally taken equal to one, and measure the amplitudes of the change in the observation parameter at each of the excitation frequencies at each of m given points, as well as at the selected observation point A of the structure, yuschiysya in that the amplitude variation in each observation parameter set of m points B j (j = 1, 2, 3, ..., m) and a selected observation point A is measured simultaneously, and the values of the amplitude functions
Figure 00000001
,
Figure 00000002
, ...,
Figure 00000003
determining the eigenmodes of vibration of the structure at each given point B j , determine from the condition of minimum objective function
Figure 00000004
Figure 00000004
где
Figure 00000005
(k=2, 3,..., n), y(A, Ωi) - амплитуда колебаний в выбранной точке наблюдения А конструкции, измеренная на частоте возбуждения Ωi (i=1, 2,..., N}; y(Bj, Ωi) - амплитуда колебаний в каждой из заданных Bj точек конструкции, измеренная на частоте возбуждения Ωi; n - число определяемых форм колебаний; N - число частот возбуждения.
Where
Figure 00000005
(k = 2, 3, ..., n), y (A, Ω i ) is the oscillation amplitude at the selected observation point A of the structure, measured at the excitation frequency Ω i (i = 1, 2, ..., N} ; y (B j , Ω i ) is the amplitude of oscillations at each of the design points specified by B j measured at the excitation frequency Ω i ; n is the number of determined vibration modes; N is the number of excitation frequencies.
RU2005131770/28A 2005-10-13 2005-10-13 Method of measuring natural vibration of flexible structure RU2308687C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005131770/28A RU2308687C2 (en) 2005-10-13 2005-10-13 Method of measuring natural vibration of flexible structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005131770/28A RU2308687C2 (en) 2005-10-13 2005-10-13 Method of measuring natural vibration of flexible structure

Publications (2)

Publication Number Publication Date
RU2005131770A true RU2005131770A (en) 2007-04-20
RU2308687C2 RU2308687C2 (en) 2007-10-20

Family

ID=38036694

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005131770/28A RU2308687C2 (en) 2005-10-13 2005-10-13 Method of measuring natural vibration of flexible structure

Country Status (1)

Country Link
RU (1) RU2308687C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113970416A (en) * 2021-10-28 2022-01-25 中国地质大学(武汉) Method for rapidly testing static human body dynamic characteristics by utilizing artificial rhythmic excitation

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2658125C1 (en) * 2017-06-02 2018-06-19 Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина" Method for determining parameters of natural tones of structure vibrations in resonant tests

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113970416A (en) * 2021-10-28 2022-01-25 中国地质大学(武汉) Method for rapidly testing static human body dynamic characteristics by utilizing artificial rhythmic excitation

Also Published As

Publication number Publication date
RU2308687C2 (en) 2007-10-20

Similar Documents

Publication Publication Date Title
RU2014105294A (en) VIBRATION METER AND APPROPRIATE METHOD FOR DETERMINING THE RESONANCE FREQUENCY
RU2008139330A (en) METHOD FOR DIAGNOSTIC OF TURBOCHARGER OPERATIONS
RU2005131770A (en) METHOD FOR DETERMINING OWN SHAPES OF ELASTIC STRUCTURE
RU2017125419A (en) GYROSCOPE
KR102142043B1 (en) Method for extracting mode fair of revolutionary shell structure using beat waves
JP4121426B2 (en) Method and apparatus for measuring coefficient for vibration energy loss
RU2445575C2 (en) Sensitive element of vibration coriolis gyroscope
RU2002124038A (en) METHOD FOR MONITORING PRODUCT DEFICIENCY
CN102680075A (en) Device and method for testing vibration isolation performance of corrugated pipe under free work condition
RU2473880C2 (en) Method to determine concrete modulus of elasticity in elastic reinforced concrete structures of beam type
RU2619812C1 (en) Method of non-destructive testing of hidden defects in technically complex structural element which is not accessible and device for its implementation
RU2008115465A (en) MEASURING ELECTRONICS AND METHODS FOR INSPECTION DIAGNOSTICS FOR FLOW METER
Zonzini et al. Heterogeneous sensor-network for vibration-based SHM
RU193215U1 (en) Toothed cavity of an inertial micromechanical sensor
RU2303774C1 (en) Method of detecting defects in flexible structure
Maloney et al. Modal testing of a soprano pan using a 3D laser Doppler vibrometer
RU2473879C2 (en) Method to determine diameter of longitudinal reinforcement in elastic reinforced concrete structures of beam type
SU1048344A1 (en) Method of investigatng aerodynamic compendency of flat grating blade oscillation in aerodynamic flow
RU2280846C1 (en) Method and device for extracting information on stressed-deformed condition of water-development works
JP2004053485A (en) Transfer characteristic measuring procedure and its device of power train
RU2006126620A (en) METHOD FOR MEASURING ULTRA-SMALL PHYSICAL VALUES THROUGH THE RESPONSIBILITY THRESHOLD OF THE RESONANT VIBRATION SYSTEM
RU2017102939A (en) STAND FOR VIBROACOUSTIC TESTS OF MODELS OF VIBROINSULATION SYSTEMS OF SHIP'S POWER ENGINEERING UNITS
RU2239165C1 (en) Method of determination of mechanical parameters and parameters of resonance oscillations
RU45525U1 (en) DEVICE FOR DETERMINING THE FREQUENCY SPECTRUM OF OWN RESONANCE OBSERVATIONS OF THE OBJECT
RU2531203C1 (en) Method of determining forms and frequencies of natural oscillation of rotor blades of gas turbine engines