Národní úložiště šedé literatury Nalezeno 79 záznamů.  začátekpředchozí21 - 30dalšíkonec  přejít na záznam: Hledání trvalo 0.00 vteřin. 
Vibrační zkoušky a dynamická analýza třecích účinků u železničního kola tlumeného tlumícím kroužkem
Pešek, Luděk ; Půst, Ladislav ; Bula, Vítězslav ; Šnábl, Pavel ; Boháč, T. ; Tašek, H. ; Běhálek, V.
Pro návrh tlumícího třecího kroužku s proměnnou křivostí s optimálním rozložením kontaktních tlaků v drážce, jež je cílem projektu DELTA, proběhla v dynamické laboratoři Bonatrans a.s. ve dnech 11. až 16. června 2019 experimentální modální analýza s jedním (SIMO) a dvěma (MIMO) budiči s těmito cíli: a) vytvořit metodiku zkoušky pro vyhodnocení třecího účinku tlumícího kroužku na tlumení vibrací kola, b) pomocí změn naměřených dynamických amplitudo-frekvenčních a fázově-frekvenčních charakteristik na amplitudu buzení popsat projevy nelineárního chování třecí vazby kruhového tlumícího kroužku v drážce kola pro různé vlastní tvary kmitání. Popis navržené metodiky a analýza naměřených výsledků z hlediska účinku třecích vazeb kruhového drátu jsou obsahem této zprávy. \n\n
Experimental and computer modelling study of glottal closing velocity during phonation
Horáček, Jaromír ; Radolf, Vojtěch ; Bula, Vítězslav ; Šidlof, P. ; Geneid, A. ; Laukkanen, A. M.
This preliminary study shows that the impact stress between the colliding vocal folds during phonation should not be evaluated from the maximum velocity of the glottal closing because the velocity of the closing diminishes just before the glottal closure. This phenomenon, which can be caused by a pressure cushion effect in the fast narrowing glottal gap, is demonstrated with measurements from high speed camera images recorded from human and on a physical laboratory model for vowel [u:] phonation and on a three-mass computer model employing a Hertz model of impact force. For a more detailed future study of this phenomenon a faster camera has to be used. \n
Experimental analysis of bladed wheel modelwith tie-boss couplings – steady and rotational states
Pešek, Luděk ; Bula, Vítězslav ; Šnábl, Pavel ; Cibulka, Jan
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was performed for validation of the numerical FE model. The pre-stresses in contacts were set and evaluated indirectly by the magnetic torque sensor. Then dynamical tests of bladed wheel under revolutions were performed. Theelectromagnetic synchronized pulses were used for excitation of forced vibration of the wheel. The Campbell diagram of the wheel with prestressed contacts was created from the measurement under revolutions. From the attenuation of resonant vibration of the wheel the dampingwas evaluated.
The Experimental Study of Aeroelastic Coupling of the Moveable Blade Grid with the Flow Field at Reynolds Number up to 150 000
Procházka, Pavel P. ; Uruba, Václav ; Pešek, Luděk ; Bula, Vítězslav
This experimental study was conducted to help clarify an aeroelastic coupling in the case of rotational periodic bodies. The blade grid was placed behind the outlet of the blow-down wind tunnel. Three of five blades were constructed to allow vertical position changing by the action of three shakers. Particle Image Velocimetry was used to study the flow field statistical and dynamical parameter. The parameters, whose presence indicates the aeroelastic coupling, are searched.
EXPERIMENTAL ANALYSIS OF BLADED WHEEL MODEL WITH TIE-BOSS COUPLINGS – STEADY AND ROTATIONAL STATES
Pešek, Luděk ; Bula, Vítězslav ; Šnábl, Pavel ; Cibulka, Jan
Experimental modal analysis of the proposed model of bladed wheel with tie-boss couplings was performed for validation of thenumerical FE model. The pre-stresses in contacts were set and evaluated indirectly by the magnetic torque sensor. Then dynamical tests of bladed wheel under revolutions were performed. The\nelectromagnetic synchronized pulses were used for excitation of forced vibration of the wheel. The Campbell diagram of the wheel with prestressedcontacts was created from the measurement under revolutions. From the attenuation of resonant vibration of the wheel the dampingwas evaluated.
The experimental study of aeroelastic coupling of the moveable blade grid with the flow field at Reynolds number up to 150 000
Procházka, Pavel ; Uruba, Václav ; Pešek, Luděk ; Bula, Vítězslav
This experimental study was conducted to help clarify an aeroelastic coupling in the case of rotational periodic bodies. The blade grid was placed behind the outlet of the blow-down wind tunnel. Three of five blades were constructed to allow vertical position changing by the action of three shakers. Particle Image Velocimetry was used to study the flow field statistical and dynamical parameter. The parameters, whose presence indicates the aeroelastic coupling, are searched.
Deformation energy of Yeoh hyperelastic model and constant hyperelastic proportional damping
Šulc, Petr ; Pešek, Luděk ; Bula, Vítězslav ; Košina, Jan ; Cibulka, Jan
The paper deals with a proposal of the dissipated energy of hard rubbers as a function of the deformation energy expressed by the Yeoh hyperelastic model. Then the deformation energy may be dependent only on the first invariant of deformation. Based on the experiment, a “hyperelastic proportional damping” (HPD) is proposed for hard rubbers under finite strains. It is analogical to the model of proportional damping in the elastic theory, i.e. the dissipated energy is proportional to the deformation energy multiplied by the frequency of dynamic harmonic loading. The Yeoh model is chosen since the deformation function is dependent only on the first strain invariant for a description of the simple shear of a surface cylinder. The constants are used to an enumeration of the deformation energy of the Yeoh model for the specific cases of tested rubbers. The coefficients of hyperelastic proportional damping are evaluated on the basis of experimental results,too.
Experimentální analýza kmitání pružných čepů čtyřplanetové převodovky za rotace
Pešek, Luděk ; Bula, Vítězslav ; Cibulka, Jan
Cílem této zprávy je popis měření a analýzy výsledků měření rotující čtyř-planetové převodovky s pružnými čepy planet navržené a vyrobené společností Wikov Gear. Měření převodovky se realizovala na zkušebně společnosti Wikov Gear v Plzni ve dnech 17.5. a 21.5.2017. Zkoušely se dvě varianty ložisek planet: a) standartní kluzkná ložiska (17.5), b( kluzná ložiska s plovoucím kroužkem (tzv. "flouting bush"). Při použití standartních ložisek planet bylo dosaženo maximální otáčkové rychlosti 8500 ot/min a u ložisek s plovoucím kroužkem bylo dosažena až otáček 14500ot/min. Měření ohybových kmitů čepů planetové převodoky bylo snímáno tenzometricky. Metodika měření byla navržena v ÚT AV ČR. Analýza byla zaměřena na vyhodnocení frekvenčních spektrogramů pro nalezení významných rezonancí kmitání čepů převodovky. Tyto poznatky sloužily k validaci vyvíjených numerických modelů v ÚT AV ČR a ladění jejich parametrů.
Dissipated energy of hard rubbers at dynamic torsional finite straining
Šulc, Petr ; Pešek, Luděk ; Bula, Vítězslav ; Cibulka, Jan ; Košina, Jan
The paper deals with a stress analysis of hard rubber under large torsion deformations. This study was motivated by effort to find the dependency the dissipated energy on the deformation energy. Based on the results of an experiment, a function of dissipation energy of hard rubbers for finite strains using the theory hyperelasticity was proposed herein analogically as a prportional damping for elastic theory. Samples of hard rubber of different hardness (EPDM, Silcone) were dynamically tested on the developed torsional test-rig at different frequencies, amplitudes. First the Mooney Rivlin model (MRM) for a shear case of loading was analytically developed and then MRM constants were attained by fitting of the MRM to the experimental torsion-deformation curve. These constants were used to obtain the deformation energy of the MRM models. The coefficients of hyperelastic proportional damping relating a dissipated energy to a strain energy were evaluated for tested rubbers on the basis of experimental results.
Design of low-subsonic blade cascade model for aero-structural dynamic testing
Pešek, Luděk ; Hála, Jindřich ; Šulc, Petr ; Chládek, Štěpán ; Bula, Vítězslav ; Uruba, Václav ; Cibulka, Jan
Low-subsonic blade cascade model for aerodynamic testing was design in the Institute. The aim is to study the flow dynamics and flutter phenomenon in the cascade with moving blade profiles. The numerical calculations of two proposed cascades were performed for analysis of influence of stagger angle, incident angle of flow and inter-blade phase angles of the relative movement of blades. The results of numerical simulations of fluid dynamics of non-stationary flow both as viscid and non-viscid are presented. Futhermore the solution of the physical model of the designed cascade including excitation of profiles, measuring of the profile displacement and aerodynamic forces are described.

Národní úložiště šedé literatury : Nalezeno 79 záznamů.   začátekpředchozí21 - 30dalšíkonec  přejít na záznam:
Chcete být upozorněni, pokud se objeví nové záznamy odpovídající tomuto dotazu?
Přihlásit se k odběru RSS.