• Title/Summary/Keyword: 커플런트

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Development and Characterization of Ultrasonic transducers for High Temperature Contact Measurement (고온 접촉식 탐상용 초음파 탐촉자 개발 및 평가)

  • Kim, Ki-Bok;Kim, Byoung-Geuk;Lee, Seung-Seok;Yoon, Nam-Won;Yoon, Dong-Jin;Ahn, Yoon-Kook
    • Journal of the Korean Society for Nondestructive Testing
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    • v.23 no.1
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    • pp.14-20
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    • 2003
  • Piezoelectric ultrasonic transducers for high temperature contact measurement were developed. These high temperature ultrasonic transducers (HTUT) consisted of bismuth titanate piezoceramic element whose Curie temperature is higher than $600^{\circ}C$, a backing material of the mixture of tungsten powder and inorganic binder, an inner alumina tube, a wear Plate and a housing. The operational frequencies or the HTUT were 1.04 and 2.08 MHz, respectively. Various commercially available couplants for high temperature were evaluated and compared. As a couplant for high temperature ultrasonic testing between HTUT and test specimen, gold epoxy was selected. The peak amplitude of pulse-echo signals from steel test specimen decreased with increasing temperature. The operational temperature of the HTUT reached up to $500^{\circ}C$ at which the continuous contact measurement was possible.

The principle and a prototype system for burning rate measurement of solid propellants using ultrasound (초음파를 이용한 고체추진제 연소속도의 측정원리 및 시범시스템 개발)

  • Song Sung-Jin;Jeon Jin-Hong;Kim Hak-Joon;Kim In-Chul;Ryoo Baek-Neung;Yoo Ji-Chang;Jung Jung-Yong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.259-265
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    • 2005
  • To measure burning rate of solid propellants using ultrasonic technique, a special closed bomb and an ultrasonic and pressure measurement system are fabricated. During pressurization tests and burning tests on propellants, ultrasonic and pressure signal are acquired in realtime fashion by this system. Based on acquired signals, analysis programs using two different algorithm which can measure burning rates corresponding to pressures are compared. One algorithm is to correct sound velocity variation of propellants and solid couplant, another one is only to correct sound velocity variation of propellants. And accuracies of homing rates measured through these algorithms are calculated through comparison with homing rates measured using strand burner method.

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The Principle and a Prototype System for Burning Rate Measurement of Solid Propellants Using Ultrasound (초음파를 이용한 고체추진제 연소속도 측정원리 및 시범시스템 개발)

  • Song, Sung-Jin;Jeon, Jin-Hong;Kim, Hak-Joon;Oh, Hyun-Taek;Kim, In-Chul;Yoo, Ji-Chang;Jung, Jung-Yong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.4
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    • pp.61-68
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    • 2006
  • To measure burning rate of solid propellants using ultrasound, a special closed bomb and an ultrasonic and pressure measurement system are fabricated. During pressurization tests and homing tests on propellants, ultrasonic and pressure signal are acquired in real time fashion by this system. Based on acquired signals, analysis programs using two different algorithm which can measure burning rates corresponding to pressures are compared. One algorithm is to correct sound velocity variation of propellants and solid couplant, another one is only to correct sound velocity variation of propellants. And accuracies of homing rates measured through these algorithms are calculated through comparison with the burning rates measured using strand burner method.

Development of a Modular Magnetostrictive Transducer for Torsional Guided Wave Transduction in a Cylindrical Structure (원통형 구조물에서 비틀림 유도초음파 변환을 위한 모듈형 자기변형 트랜스듀서 개발)

  • Cho, Seung-Hyun;Park, Jae-Ha;Kwon, Hyu-Sang;Ahn, Bong-Young;Lee, Seung-Seok
    • Journal of the Korean Society for Nondestructive Testing
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    • v.29 no.5
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    • pp.427-435
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    • 2009
  • Cylindrical structures such as pipes and shafts are widely used in various industrial facilities. Recently, researches on magnetostrictive transduction of torsional waves have been actively reported for the nondestructive evaluation of those cylindrical structures. However, the existing magnetostrictive patch transducer has somewhat inconvenient and time.consuming process like patch bonding to a structure since it should employ a magnetostrictive patch having strong magnetostriction. To overcome these limitations of the existing transducer, in this work, we develop a novel modular magnetostrictive transducer to generate and measure torsional waves to inspect a cylindrical structure. The proposed transducer can be applied as viscous liquid coupling with shear couplant or dry coupling without coupling media instead of patch bonding to a structure. We describe a detailed structure of the modular transducer and conduct some experiments to verify its performance.

Development of an SH Wave Magnetostrictive Transducer Module for Guided Wave Testing of Plate Structures (판형 구조물 유도초음파 검사를 위한 SH파 자기변형 트랜스듀서 모듈 개발)

  • Cho, Seung-Hyun;Park, Jae-Ha;Kwon, Hyu-Sang;Ahn, Bong-Young;Lee, Seung-Seok
    • Journal of the Korean Society for Nondestructive Testing
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    • v.29 no.2
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    • pp.122-129
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    • 2009
  • Recently much attention has been paid to a guided wave due to its effective applicability to long range and fast inspection of structures. In guided wave based NDE, the appropriate selection of wave modes is one of important factors since the test performance is highly dependent on which mode of guided waves is employed. As far as plate-like structures are concerned, so far, SH guided wave has not been frequently applied compared to Lamb waves, which is mostly caused by the lack of proper and convenient transducers to generate and measure the SH waves. In this investigation, a new small-sized SH guided wave transducer based on magnetostriction is proposed. The present transducer was designed to be modular and be used with shear couplant to avoid the inconvenience of the existing magnetostrictive patch transducers, which comprises the ferromagnetic patch tightly bonded to a structure. The wave transduction mechanism and the detailed configuration of the present transducer are presented. Experimental verification is also conducted on test specimens and the results confirm the good performance of the present transducer module.