In general, a large mirror without weight reduction in large optical or space telescope systems can increase the system’s weight or lead to significant deformation of the mirror surface. Thus, it is imperative to pursue lightweight design strategies. In this paper, the structure design of a spherical mirror, a diameter of 600mm and a mirror radius of 2,000mm, was investigated to reduce weight and minimize deformation. To establish load paths for internal and external loads, stiffeners were added across the lateral supports. This approach effectively reduced both weight and deformation caused by gravity. Weight reduction and reduction percentages were quantified, and the mirror deformation was evaluated by using finite element analysis (FEA). The proposed structures were compared with honeycomb structures for weight reduction. This evaluation allowed to assess the deformation characteristics and the potential advantages of the proposed structures for lightweight mirrors.

Zerodur, one of the optical materials, was used for large spherical mirrors in this study. For weight reduction, several types of honeycomb structures were investigated. The finite element simulation was used for deformation and mode analysis. It was revealed that the weight reduction rate and maximum deflection due to the gravity effect vary depending on the honeycomb structures. Additionally, this study highlights the potential of spline-shaped honeycomb structures as an alternative for weight reduction, and triangular honeycomb structures demonstrated the less deformation by the gravity effect. The findings from this study provide valuable insights for designing lightweight and high-performance spherical mirrors in optical systems.

The purpose of this study was to develop high quality dark film honeycomb fabric curtains. The results of producing the prototype for various color tone development, hot melt viscosity, and adhesiveness test for the final prototype were as follows. The hexagonal honeycomb structure is easy to manufacture, has a good coupling force, and has a dark honeycomb fabric curtain. The hot melt condition was obtained with 540g of hot melt and 1.5kg of diluent, 242.3cp, and the curing result was obtained at 140°C. Seven different colors were developed using yellow, red, blue, and white four primary colors. The adhesive force test device was designed to enable more than 5,000 real tests by the automatic opening and closing device for the convenience of the field workers. The size of the test sample was designed to be 1,000mm × 1,200mm. As a result of designing and manufacturing the prototype to attach the monitor and the control device to automatically count, the prototype was made to be measured 10,000 times. The combined force of the honeycomb fabric curtain was maintained after 5,000 tests on the manufactured rock film honeycomb fabric curtain.

The objective of this study is to analysis the seismic response of 200m spanned honeycomb lattice domes under horizontal and up-down ground motion of El Centro earthquake. For the analysis of seismic response of the honeycomb lattice domes by rise/span ratio, the time history analysis is used for the estimation of the dynamic response. The low rise lattice dome is less deformed and less stressed than the high rise lattice dome for the earthquake ground motion. The 3-dimensional earthquake response is not significantly different the dynamic response of one directional ground motion. The earthquake response of domes with LRB isolation system is significantly reduced for the asymmetric vertical deformation and the horizontal and vertical accelerations.

현재 해양플랜트용 패널의 주요한 중심재는 다공성재료(미네랄울) 이지만, 뛰어난 차음성능에도 불구하고 환경적인 이유로 이 를 대체할 재료가 요구되고 있다. 허니컴 구조는 무게 대비 강도가 우수하여 산업전반에서 많이 쓰이고 있다. 하지만 소음진동 측면에서의 연구는 미미하다. 다공성재료를 대체하기 위한 연구로서 허니컴의 음향학적 연구가 필요하다. 본 논문에서는 허니컴패널을 대칭모드와 비 대칭모드의 중첩으로 가정하여 수치해석을 진행하였다. 이러한 이론을 통한 수치해석과 실험결과를 비교하여 수치해석의 신뢰성을 검증 하였다. 그리고 수치해석을 통해 허니컴패널의 차음특성을 연구하고 중심재로서의 가능성을 평가하였다. 패널두께를 키울수록 일치주파 수가 저주파수로 이동하였다. 셀사이즈와 셀벽의 사이각이 감소함에 따라 차음성능이 개선되었고, 셀벽두께의 경우 증가할수록 차음성능 이 향상되었다.

A simulation method to estimate microstructure dependent material properties and their influence on performance for a honeycomb structured SiC heating element has been established. Electrical and thermal conductivities of a porous SiC sample were calculated by solving a current continuity equation. Then, the results were used as input parameters for a finite element analysis package to predict temperature distribution when the heating element was subjected to a DC bias. Based on the simulation results, a direction of material development for better heating efficiency was found. In addition, a modified metal electrode scheme to decelerate corrosion kinetics was proposed, by which the durability of the water heating system was greatly improved.

본 연구에서는 허니컴 패널의 지배방정식을 이용하여 경계행렬식을 유도하였고, 이를 전달행렬법에 적용하여 허니컴 패널을 적용한 차음패널에 대한 해석 이론을 정립하였다. 또한, 허니컴 패널을 선박용 차음패널의 표면재로 적용하여 차음성능을 분석하였고, 철판을 표면재로 적용한 기존의 선박용 차음패널과 차음성능을 무게 당 감음량 기준으로 비교 분석하였다. 그 결과, 허니컴 패널의 차음성능이 0.35 mm 철판에 비해 STC 기준으로 2dB 높게 나와 허니컴 패널을 적용한 차음패널의 차음성능이 철판을 사용한 차음패널에 비해 무게 당 감음량을 고려할 시 우수하다는 것을 확인하였다. 또한, 허니컴 패널을 표면재로 사용한 차음패널의 면밀도가 철판을 사용한 차음패널에 비해 약 5.2 kg/㎡ 가볍게 나타났고, 이는 약 31.7 % 무게 감소를 의미한다.

In this study, the impact properties of aluminum honeycomb core composite are investigated through simulation analysis. The specimens are applied with different impact energies of 50 J, 70 J, and 100 J. The maximum load occurs at 3.7 ms for 50 J, 3.7 ms for 70 J and 2.3 ms for 100 J. The maximum load occurs when the striker is penetrating the upper face sheet in all cases. In case of 50 J impact energy, striker does not penetrate the lower face sheet and honeycomb core sandwich can be stable as the energy of 38 J happens. In case of 70 J impact energy, the striker penetrates into the specimen. The striker then causes the damage to the lower face sheet after penetrating the upper face sheet and the core as the energy of 53 J happens. In case of 100 J impact energy, the striker penetrates through all of the upper face sheet, core and lower face sheet as the energy of 65 J happens. This study can be utilized at the design of aluminum honeycomb core sandwich composite structure by understanding stability through the impact property.

The rheological behavior of a cordierite honeycomb extrusion paste was investigated by measuring torque values in a Brabender plastograph. The extrusion pastes were formulated using binder (methy cellulose, MC), solvent (water), plasticizer (ploy ethylene glycol, PEG) and lubricants (oleic acid, OA). The mixing sequence and optimum organic binder, at least for homogeneous mixed state, can be determined from the rheological point of view. 3%MC-30%-1.5%PEG-1.0%OA with respect to the cordierite powder was chosen as a binder composition for the extrusion process of cordierite powder.

에너지원으로서 수소를 생산하기 위하여 하니컴 구조를 갖는 모노리스에 10 wt% Ni/CeO2-ZrO2 촉매를 담지한 후 메탄의 수증기 개질 실험을 수행하였다. 다른 CeO2/ZrO2 몰비를 갖는 촉매들 중에서, Ni/CeO2-ZrO2(CeO2/ZrO2=4/1)촉매가 700-800℃에서 높은 메탄의 전환율을 보여 주었다. 10wt% Ni/CeO2-ZrO2 촉매가 담지된 금속 모노리스 촉매체는 높은 열전도도와 비표면적들로 인하여 좋은 촉매 특성을 보여줌을 확인할 수 있었다. 또한, 금속모노리스 촉매체는 반응물에서 과다의 수증기에 의한 수소 수율에서 크게 영향을 받지 않음을 알 수 있었다. GHSV=30,000h-1, 반응물 비(H2O/CH4=3.0) 반응온도 800℃에서 금속모노리스 촉매체는 98%이상의 메탄의 전환율을 보여주었다. 생성물 가스에서 CO2/CO의 비는 수증기/메탄의 반응물비가 증가할수록 수성가스화 반응에 의하여 증가됨을 알 수 있었다.

In this study, we attempt to synthesize the cordierite from the reaction of fly-ash, alumina, silicon dioxide, and magnesia powders. For the purpose of air purification, the honeycomb filter with porous cordierite was fabricated from the combination of synthetic cordierite and pore forming agent. Fabricated porous cordierite honeycomb was prepared with high porosity (58%), and good compressive strength (69MPa).

Four kinds of plasma blacks were prepared by plasma pyrolysis under various metallic catalysts coated on honeycomb, and investigated the catalytic effect on the characteristics of the plasma blacks prepared under plasma pyrolysis condition. Pt, Pt-Rh, and Pd catalysts were employed as active materials to prepare the plasma blacks. In the experimental range studied, the metallic catalysts influenced on surface area, particle size, surface oxygen content and electrical conductivity of the plasma blacks prepared. It was showed that more dense particle of plasma blacks were prepared under existence of metallic catalysts. Presence of the metallic catalyst reduces the electrical resistivity of plasma blacks due to the decrease in the amount of oxygen functional groups. The highest electrical conductivity of plasma black was observed in the Pt catalyst and then followed by those Pt-Rh, Pd and bare cordierite honeycomb.

본 논문에서 알루미늄 하니콤 샌드위치판 구조(AHSP)의 특성에 대해 해석한 결과는 다음과 같다. 1) AHSP의 H/T비가 낮아질수록 응력이 감소하며, 셀 크기(H)보다는 코어의 두께(T)가 두꺼워질수록 강도와 강성이 증가함을 알 수 있다. 2) AHSP 구조가 동일한 질량에서부터 증가하면서 EASP 구조에 비해 2.5～6.0배 정도의 높은 강도를 보이는 것을 알 수 있다. 3) AHSP의 면재의 두께변화는 AHSP 전체의 강성에 별로 영향을 미치지 못했으나, 심재의 두께가 증가할수록 단면 2차 모멘트의 값이 커지기 때문에 AHSP의 강성이 매우 커짐을 알 수 있다. 4) EASP보다 강성이 큰 AHSP의 고유진동수가 크며, 진동 모드 사이의 차도 커짐을 알 수 있다. 5) 비교연구 결과 AHSP 구조가 EASP 구조보다 적은 질량으로 훨씬 더 높은 강성을 갖는, AHSP 구조의 우수성이 입증된다. 따라서 중량경감이 가장 중요한 문제 중의 하나인 초고속선 및 대형선의 경우 AHSP 구조가 높은 굽힘강성을 갖고 다른 재료에 비해 상대적으로 적은 중량이 필요하므로 구조 재료로서의 적합성을 알 수 있다.

We investigated the androgenic effects of 11-ketotestosterone (11-KT) on gonadal sex reversal and spermatogenesis in honeycomb grouper Epinephelus merra by method of gonadal biopsy. 11-KT was injected intramuscularly at a concentration of 1 and body weight. The proportion of cross sectional area of the gonad occupied by each germ cell type was measured and compared pre- and post-injection group. During the sex change phase, the distribution ratio of oocytes was decreased in all fish of 11-KT treatment group while the distribution ratio of spermatocytes was increased than pre-injection group. In male phase, all fish of 11-KT treatment group shown the increased distribution ratio of spermatocytes, but the distribution ratio of spermatozoa was decreased than pre-injection group. The present results suggest that 11-KT can stimulate degeneration of oocytes, proliferation of spermatocytes and spermiation in honeycomb grouper.

2000년 2월부터 2001년 2월까지 남태평양 미크로네시아 군도의 Chuju 연안에 서식하는 주Epinephelus merra 암컷을 대상으로 생식주기를 조사하였다. 생식소숙도지수 (GSI)는 2월부터 증가하기 시작하여 3월에 최고치 (3.410.84)를 보였다. 조직학적 관찰결과 3월과 4월의 난소 안에는 난황을 가진 다양한 단계의 난모세포와 배란여포들이 존재하였다. 6월부터 1월에 난소 안에는 미성숙 난모세포만 있었다. 이들 결과로 E. merra