Simulation analysis method and system for dynamic response of three-dimensional blade tip gap of crack-containing blade
The invention discloses a dynamic response simulation analysis method and system for a three-dimensional blade tip gap of a crack-containing blade, and the method comprises the steps: enabling a crack to be equivalent to a radial extension spring of the blade for the radial vibration of the blade, a...
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creator | HUANG XIN ZHANG XIAODONG DAI FEI XIONG YIWEI FAN BOCHAO |
description | The invention discloses a dynamic response simulation analysis method and system for a three-dimensional blade tip gap of a crack-containing blade, and the method comprises the steps: enabling a crack to be equivalent to a radial extension spring of the blade for the radial vibration of the blade, and calculating the inherent frequency and vibration mode equation of the radial vibration of the blade; aiming at blade bending vibration, enabling the crack to be equivalent to a torsion spring and an extension spring in the width/thickness direction of the blade, and calculating an inherent frequency of the blade bending vibration and a vibration mode equation of displacement and a section corner caused by bending; a uniform-section torsion blade with penetrating cracks at the tail edge is used as a research object, according to the Hamiltonian principle, a dynamical model of the blade with the cracks is established in combination with a Galerkin method, the dynamical model is solved, and the dynamic response of |
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aiming at blade bending vibration, enabling the crack to be equivalent to a torsion spring and an extension spring in the width/thickness direction of the blade, and calculating an inherent frequency of the blade bending vibration and a vibration mode equation of displacement and a section corner caused by bending; a uniform-section torsion blade with penetrating cracks at the tail edge is used as a research object, according to the Hamiltonian principle, a dynamical model of the blade with the cracks is established in combination with a Galerkin method, the dynamical model is solved, and the dynamic response of</description><subject>CALCULATING</subject><subject>COMPUTING</subject><subject>COUNTING</subject><subject>ELECTRIC DIGITAL DATA PROCESSING</subject><subject>PHYSICS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzTEKwkAQBdA0FqLeYTxAwBCCaSUoVjbah3F3kgzuzoadFcntjegBrD4fHv8vs9eV_dNh4iCAgm5SVvCUhmDnbkEnTeShCxHsJOjZQCQdgyhB6CANkSi37El0nkAHd4eWIPEIPY4fYiKaR26CJGRh6b9inS06dEqbX66y7el4a845jaGdD9CQUGqbS1FU-6qud-Wh_Me8AaAnRhk</recordid><startdate>20230307</startdate><enddate>20230307</enddate><creator>HUANG XIN</creator><creator>ZHANG XIAODONG</creator><creator>DAI FEI</creator><creator>XIONG YIWEI</creator><creator>FAN BOCHAO</creator><scope>EVB</scope></search><sort><creationdate>20230307</creationdate><title>Simulation analysis method and system for dynamic response of three-dimensional blade tip gap of crack-containing blade</title><author>HUANG XIN ; 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aiming at blade bending vibration, enabling the crack to be equivalent to a torsion spring and an extension spring in the width/thickness direction of the blade, and calculating an inherent frequency of the blade bending vibration and a vibration mode equation of displacement and a section corner caused by bending; a uniform-section torsion blade with penetrating cracks at the tail edge is used as a research object, according to the Hamiltonian principle, a dynamical model of the blade with the cracks is established in combination with a Galerkin method, the dynamical model is solved, and the dynamic response of</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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subjects | CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS |
title | Simulation analysis method and system for dynamic response of three-dimensional blade tip gap of crack-containing blade |
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