• Applied Science and Convergence Technology
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• 제24권5호
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• pp.142-150
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• 2015

A failure analysis of tungsten filaments used in quadrupole mass spectrometer for plasma process monitoring was carried by using SEM and EDS. Failed at high temperature, filaments showed two kinds of failure modes. The one is that diameter of filament became thinner gradually and finally snapped. The other is that filament abruptly snapped almost at a right angle. The EDS analysis showed Fe and C, including W and Fe, on the surface of failed filament. when failed filaments were treated with plasma in mixture of Ar and $CF_4$, the amount of Fe and C decreased. The failure analysis of filament showed that the cause of filament failure is thermal evaporation and grain growth of tungsten at high temperature.

• Journal of Advanced Marine Engineering and Technology
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• 제25권3호
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• pp.617-622
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• 2001

The purpose of this study is to design and the analyze the stress of composited shaft which is wound by filament winding method. The composites shaft has high strength and reduction in weight compared to metal shaft. The classical laminate plate theory(CLT) was used fro analysis the stress, and for structure design. In order to replace metal shaft by composites shaft, the diameter of shaft was determined to $\phi$ 40. The ration of diameter was determined to 0.4 for torsional moment with CLT. In this result of analyzing the stress, composites shaft was safe $30^{\circ}~60^{\circ}$C of winding angle, and was fractured on $90^{\circ}$.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.193-196
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• 2001

The purpose of this study is the design of composite shaft which is wound by Filament Winding method. Classical laminated plate theory was used for analyzing the stress, and for structure design. The diameter and thickness of composite shaft were calculated by this theory. The result that if tensile stress was zero, torsion stress was a certain value below 0.4(diameter rate) and torsion strength was the highest value on $45^{\circ}C$(winding angle). In case of $90^{\circ}C$(winding angle), we have to consider the torsional monent when the composites shaft was load.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2001년도 춘계학술대회 논문집
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• pp.140-145
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• 2001

The purpose of this study is the design of composite shaft which is wound by Filament Winding method. Classical laminated plate theory was used for analyzing the stress, and for structure design. The diameter and thickness of composite shaft were calculated by this theory. The result that if tensile stress was zero, torsion stress was a certain value below 0.4(diameter rate) and torsion strength was the highest value on 45$^{\circ}$(winding angle). In case of 90$^{\circ}$(winding angle), we have to consider the torsional moment when the composites shaft was load.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2000년도 제18회 학술발표회 논문개요집
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• pp.210-210
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• 2000

Vertically well aligned multi-wall carbon nanotubes (CNT) were grown on nickel coated glass substrates by plasma enhanced hot filament chemical vapor deposition at low temperatures below 600$^{\circ}C$. Acetylene and ammonia gas were used as the carbon source and a catalyst. Effects of growth parameters such as pre-treatment of substrate, plasma intensity, filament current, imput gas flow rate, gas composition, substrate temperature and different substrates on the growth characteristics of CNT were systematically investigated. Figure 1 shows SEM image of CNT grown on Ni coated glass substrate. Diameter of nanotube was 30 to 100nm depending on the growth condition. The diameter of CNT decreased and density of CNT increased as NH3 etching time etching time increased. Plasma intensity was found to be the most critical parameter to determine the growth of CNT. CNT was not grown at the plasma intensity lower than 500V. Growth of CNT without filament current was observed. Raman spectroscopy showed the C-C tangential stretching mode at 1592 cm1 as well as D line at 1366 cm-1. From the microanalysis using HRTEM, nickel cap was observed on the top of the grown CNT and very thin carbon amorphous layer of 5nm was found on the nickel cap. Current-voltage characteristics using STM showed about 34nA of current at the applied voltage of 1 volt. Electron emission from the vertically well aligned CNT was obtained using phosphor anode with onset electric field of 1.5C/um.

• 공업화학
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• 제22권5호
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• pp.467-472
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• 2011

본 연구에서는 천연물을 이용한 기능성 섬유를 제조하기 위하여 미처리 및 불소화 일라이트를 첨가하여 일라이트/PP 복합섬유를 용융방사로 제조하고 그 물리적 특성을 고찰하였다. 복합필라멘트 형성 시 층상구조를 가지는 일라이트의 윤활특성으로 순수 PP 필라멘트에 비해 복합필라멘트의 직경이 감소하는 현상이 나타났으며, 불소화의 효과로 인한 계면 친화성 향상 및 분산성 향상으로 불소화 일라이트/PP 복합필라멘트의 직경이 순수 PP 필라멘트의 2/3 정도로 감소하였다. 미처리 및 불소화 일라이트 모두 일라이트/PP 복합필라멘트의 열안정성을 향상시키는 효과가 있는 것으로 확인되었다. 또한, 미처리 일라이트/PP 복합필라멘트는 연신 공정을 거칠 때 절사가 발생하여, 복합섬유로서 활용될 수 없었으나, 불소화 일라이트/PP 복합필라멘트는 연신 후 순수 PP 필라멘트와 비슷한 인장강도를 가지고, 50% 정도 증가한 탄성률을 가지는 것으로 보아 복합섬유로서 사용될 수 있음을 확인할 수 있었다. 일라이트/PP 복합필라멘트를 형성 시, 불소화를 통하여 일라이트/PP간의 계면 친화성이 향상되고 고분자 내 분산성은 향상이 되었으나, 층간 결합력이 강한 비팽윤성 일라이트 고유의 성질로 인하여 일라이트의 박리나 PP의 일라이트 내 층간삽입이 충분히 발생하지 않은 것으로 보아 나노복합체가 아닌 마이크로 복합체를 형성하는 것으로 여겨진다.

• 대한기계학회논문집A
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• 제26권2호
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• pp.308-313
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• 2002

It is known that the composite material shafts using on small boats have various advantages comparing to forged steel shafts, fur examples, specific strength, fatigue strength, corrosion, etc. The analysis of the stresses and strains in the composite material shafts made by filament winding method is presented in this paper. The classical laminated plate theory is applied on the patch cut from the composite material hollow shafts. It is verified that the composite material hollow shafts of diameter 40 mm is the most optimum when the ratio of the inner diameter to the outer is 0.4 and winding angle is 45$^{\circ}$. It is also proven that the shear strain does not change seriously between 30$^{\circ}$and 60$^{\circ}$of winding angles. It is dangerous when the winding angle is over 75$^{\circ}$because the values of shear strain and stress produced on the shaft are too high so it must be avoided to wind the filament by the angle over 75$^{\circ}$.

• Applied Microscopy
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• 제51권
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• pp.3.1-3.6
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• 2021

We examined the morphology of fertilized egg and ultrastructures of fertilized egg envelopes of dwarf rainbowfish (Melanotaenia praecox) belong to Melanotaeniidae using light and electron microscopes. The fertilized eggs were spherical with adhesive filament, transparent, demersal, and had a narrow perivitelline space and small oil droplets. The size of fertilized egg was 1.02 ± 0.18 mm (n = 30), and there were two kinds of adhesive filament on the fertilized eggs. The long and thick (diameter 12.22 ± 0.52 ㎛, n = 20) adhesive filaments were only at the area of animal pole, and short and thin (diameter 1.99 ± 0.23 ㎛, n = 20) adhesive filaments were around the long filaments. A micropyle was conical shaped with adhesive filament and located near the animal pole of egg. The outer surface of fertilized egg was rough side. Also, the total thickness of the fertilized egg envelope was about 7.46 ± 0.41 ㎛ (n = 20), the fertilized egg envelope consisted of two layers, an inner lamellae layer and an outer layer with high electron-density. And the inner layer was 8 layers. Collectively, these morphological characteristics and adhesive property of fertilized egg with adhesive filaments, and ultrastructures of micropyle, outer surface, and section of fertilized egg envelope are showed species specificity.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1998년도 하계학술대회 논문집 A
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• pp.349-352
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• 1998

In future superconducting electrical machines and device. AC loss in the superconducting windings are one of the most impotent design paramenters. This paper descriptions a series of Characteristic of a high-Tc superconducting Bi-Pb-Sr-Ca-Cu-O Ag-sheathed filament. In the case simulation and design to reduce ac loss is considered the filament number, twitch pith number and diameter of filament. A filament sample with Tc of 78K is made by $835^{\circ}C$ sintering for 50h and $0.33^{\circ}C$/min heating rate in an atmosphere. The experiment observations are compared with self-field loss and AC losses of Bi-Pb-Sr-Ca-Cu-O filament at 77K in following environments ; (i)AC external parallel magnetic field in different frequencies. And an analytical expression of the loss the derivation of transposition from an optimum condition was derived for the external AC magnetic field, theoretical predictions were found to coincide with the experimental observations.

• 한국추진공학회지
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• 제25권6호
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• pp.74-86
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• 2021

복합재 격자구조체는 요구 하중을 최소한의 무게 및 두께로 지지하는 구조체로, 고강도 탄소섬유에 에폭시 수지를 함침시켜 필라멘트 와인딩 공법으로 제작된다. 구조적으로 반드시 필요한 부분만을 적층 및 제작하므로 항공기 동체, 위성발사체 및 유도무기 등에 적용하여 경량화를 극대화 할 수 있다. 본 논문에서는 대형 원통형 및 콘형 복합재 격자구조체의 설계, 해석, 제작 및 평가까지 전 순기에 해당하는 복합재 격자구조체 개발 및 평가를 수행하였다. 실제 발사체 및 유도무기에 적용이 가능하도록 직경 2,600 mm, 길이 2,000 mm의 원통형 격자구조체와 상단 직경 1,300 mm, 하단 직경 2,500 mm, 길이 900 mm의 콘형 격자구조체를 개발하였으며, 하중시험을 통해 대형 복합재 격자구조체의 성능을 평가하였다.