• 반도체디스플레이기술학회지
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• 제11권3호
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• pp.27-31
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• 2012

This paper presents a study on the design of photovoltaic system with reversal tracking reflector. The reversal tracking reflector is conceptually designed by using TRIZ. The 20 to 30% of incident rays cannot produce the current and reflected back to the glass surface because of high refractive index of solar cell which are produced from Si, GaAs. The solution of this problem has been derived using 6SC(6 steps creativity)TRIZ. The reflector which has the actuator can be trackback the sun. Reversal tracking reflector which mounted on the top of the system prevents the shadowing loss and improve the efficiency of track back function. The anti-glare reflector prevents the heat due to the concentrated reflected light rays.

• 조명전기설비학회논문지
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• 제25권11호
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• pp.67-72
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• 2011

Recently, photovoltaic generator system is widely extended by energy policy of the government. Add to this, for high efficiency of power generation per natural light unit area is needed to sun tracking system. And it is needed to condensed light generator for reducer of equipment expense. As method of solving this problem, this paper is developed multi-flat reflector sun tracking system for sun photocell maximum power generation. The system is consisted of multi-flat reflector and two axes machinery and sun location perceiver and AVR controller. GaAs 3J cell generated 6.75 times power more than silicon cell by times condensing light system. As a result, condensing light system of multi-flat reflector generated maximum power and showed reducing costs to photovoltaic generator.

• 전기전자학회논문지
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• 제3권1호
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• pp.1-10
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• 1999

In this paper, the design for the shaped offset cassegrain antenna system combined with corrugated feed horn is presented. First, spherical-mode wave theory is applied to the corrugated conical horn and its radiation patterns are investigated. Using the radiation patterns, design data of the corrugated conical horn are obtained by efficiency investigation of horn antenna. When the investigation is completed, the flare angle and length of the corrugated conical horn is determined. Next, the main and sub-reflector is designed using Snellis law and the conservation principle of energy. Then the uniform direction and energy density of the traveling wave at the aperture of the main-reflector is obtained. The maximum size of the main-reflector is determined by investigation of the illumination and spillover efficiency. Finally, the curvature of the main-reflector is modified to satisfy the condition of the uniform phase. From the calculated efficiencies, the designed site of the main-reflector and sub-reflector, system gain of the shaped offset cassegrain antenna has been obtained 40.5dB in Ka-band frequency. It has better characteristics than the result of SABOR with 39dB gain.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2001년도 춘계학술대회 논문집
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• pp.114-118
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• 2001

HP Laser Interferometer Measurement System[HP5529A] is one of the most powerful equipment for measurement of the motion accuracy. The straightness measurement system of the HP5529A is composed of wollastone prism and reflector. In this system, straightness error is measured by relative lateral motion between prism and reflector. But rotating motion of prism or reflector as moving optic causes not real straightness error but additive straightness error. Especially unwanted straightness error as this becomes very large when reflector is used as moving optic and an interval between reflector and prism is distant. In this paper, the compensation method is proposed for removing additive error and experiment is carried out for theoretical verification.

• 한국정밀공학회지
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• 제22권9호
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• pp.69-76
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• 2005

The laser interferometer system such as HP5529A is one of the most powerful equipment fur measurement of the straightness error in precision stages. The straightness measurement system, HP5529A is composed of a Wollaston prism and a reflector. In this system, the straightness error is defined as relative lateral motion change between the prism and the reflector and computed from optical path difference of two polarized laser beams between these optics. However, rotating motion of the prism or the reflector used as a moving optic causes unwanted straightness error. In this paper, a compensation method is proposed for removing the unwanted straightness error generated by rotating the moving optic and an experiment is carried out for theoretical verification. The result shows that the unwanted straightness error becomes very large when the reflector is used as the moving optic and the distance between the reflector and the prism is far. Therefore, the prism must be generally used as the moving optic instead of the reflector so as to reduce the measurement error. Nevertheless, the measurement error must be compensated because it's not a negligible error if a rotating angle of the prism is large. In case the reflector must be used as the moving optic, which is unavoidable when the squareness error is measured between two axes, this compensation method can be applied and produces a better result.

• 설비공학논문집
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• 제20권8호
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• pp.563-569
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• 2008

Radiative, heating is suitable for outdoor heating system in windy and cold seasons. Optimal design of the reflector is very important to maximize heat transfer to a specific target area in the open space. The geometrical optical theory can be applied to analyze efficiency of the reflector. Commercial ray tracing computer programs are available only for limited geometries of the reflector. Alternatively, it may be designed and analyzed through an approximated simple lens theory. Two types of reflectors are analyzed using either of these methods. The key issue in this paper is to propose a new illumination experimental method for determination of the radiative efficiency. Optical light source and illuminometer are employed. The calculated efficiency of the reflector is compared with experimental one for checking the reliability. The relative errors between the experimental and analytical results are less than 5%, which proves the validity of this method. Based on these methodologies, a practical reflector and heating lamp unit is developed.

• 한국안광학회지
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• 제13권1호
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• pp.65-69
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• 2008

목적: Doublet 반사경을 이용한 조준사격용 도트 사이트 장치의 개발. 방법: Sigma 2000 광학 설계 프로그램으로 Singlet 반사경과 Doublet 반사경을 설계하여 비교 검토하였다. 결과: 유한광선수차 분석에서 기존 Singlet 반사경을 사용한 도트 사이트 장치에 비해 시차(parallax)가 제거된 유효 시야가 3.3배 확대되는 성능을 보인다. Doublet 반사경을 사용하는 경우 광학계의 중심 두께가 기존 Singlet 반사경을 사용한 경우보다 2배 이상 두꺼워지기 때문에 목표점이 관측자의 망막에 결상할 때 Singlet 반사경의 경우와 같이 제1면과 제3면의 곡률반경을 동일하게 할 경우에는 배율 변화가 나타난다. 이를 극복하기 위해 Doublet 반사경인 경우에는 어포칼 조건을 만족하는 것이 필요하다. 결론: 기존의 Singlet 반사경의 방식보다 시차(parallax)가 제거된 유효 시야가 3.3배 확대되는 성능을 가지는 Doublet 반사경을 이용한 조준사격용 도트 사이트 장치를 개발하였다.

• Journal of the Optical Society of Korea
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• 제19권4호
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• pp.421-426
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• 2015

This paper presents a hybrid single optical system for an LED surgical light that combines the advantages of both lens- and reflector-type single optical systems. The proposed hybrid single optical system includes a lens in the center and the LED light originating from the lens is redirected using a reflector to achieve a high beam spread. Iterative optical software simulations are used to provide data for the design of the lens and reflector for a single optical system, and for a complex optical system for the LED light assembly. The resulting data is also used to fabricate a prototype system. Experiments using the prototype of the hybrid single optical system and a mock-up LED surgical light confirm the system's shadow dilution performance and its applicability to surgical operations.

• Composites Research
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• 제37권3호
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• pp.219-225
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• 2024

정찰위성의 탑재체인 위성용 전개형 반사판 안테나는 발사 환경에 대한 구조안정성 및 궤도 환경에 대한 운용 성능을 고려하여 경량화, 고성능의 구조 개발이 필수적이다. 그 중, 복합재 주반사판은 전개형 반사판 안테나를 구성하는 핵심 구성품이며, 발사체 탑재 성능을 고려한 경량 설계 뿐만 아니라 위성체 임무 수행 중 민첩한 자세제어 기동 이후 높은 품질의 위성 영상을 획득하기 위해서는 높은 전개 시 강성을 갖는 고성능의 주반사판 개발이 요구된다. 주반사판 개발을 위해 전개형 반사판 안테나를 구성하는 복합재 주반사판의 적층 설계 및 재료 물성에 따른 구조적 성능을 분석하여 주반사판의 초기 설계안을 도출하였으며, 도출된 초기 설계안을 기준으로 제작 공정을 변수로 4가지 타입의 복합재 주반사판을 제작하였다. 공정 변수로는 복합재 구조의 성형 공정, 탄소 섬유 복합재 시트와 허니콤 코어 간 접착 필름의 적용 유/무, 샌드위치 복합재 내부의 벤팅 경로를 선정하였다. 제작된 4가지 종류의 주반사판에 대해 무게 측정, 비파괴 검사, 표면오차 측정 및 모드 시험을 통한 전개 시 강성 측정을 수행하였으며, 경량 및 구조적 성능을 향상시킬 수 있도록 접착 필름을 미적용하며 벤팅 경로를 포함하는 주반사판 제작 공정을 선정하여 SAR(합성 개구 안테나)를 포함한 위성체에 실 적용이 가능한 복합재 주반사판을 개발하였다.

• 한국생산제조학회지
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• 제5권2호
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• pp.73-82
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• 1996

A simtered carbide roller mold for reflector which is used for coverof automobile lamp and beacon plate of highway has been developed. The geometry of sintered carbide roller mold has been determined from the analysis of reflector geometry. An acute angle diamond wheel and dressing system also has been designed and developed to manufacture the sintered carbide roller mold.