• 제목/요약/키워드: orbital order

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안와종양의 임상경험 (Clinical Experiences of the Orbital Tumors)

  • 이경하;정화선
    • Journal of Yeungnam Medical Science
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    • 제13권1호
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    • pp.78-85
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    • 1996
  • 영남대학교 의과대학 부속병원 안과에서 1984년 3월부터 1994년 8월까지 병리조직검사로 확인된 안와종양 95례를 대상으로 임상적 고찰을 실시하였다. 안와종양의 발생빈도는 성별로는 남자가 46명(48.4%), 여성이 49명(51.6%)으로서 유의한 차이를 보이지 않았으며, 연령분포는 양성종양의 경우 전 연령층에 걸쳐 고루 분포하였고, 악성종양의 경우 10세 미만과 50-60대에 특히 많은 발생을 보였다. 광학 현미경으로 살펴본 병리조직학적 검사상 양성 대 악성의 비율은 82% : 18%로서 다른 연구에서 보다 양성종양의 비율이 높았다. 종류별로는 피부지방종(20례, 21%), 유피낭(11례, 11.6%), 점액류(8례, 8.4%), 지방종(7례, 7.4%), 다형생 선종(5례, 5.3%) 순이었다. 양성종양은 성인의 경우 점액류, 유피낭, 다형성 선종, 해면혈관종 순의 발생빈도를 보였고, 소아의 경우 피부지방종, 유피낭, 지방종, 망막모세포종 순의 발생빈도를 보였다. 악성종양은 망막모세포종 3례, 악성 흑색종 2례, 피지선암 2례, 상악동암 2례 등이었다. 악성종양중 사망한 경우는 17례 중 8례 (47.0%)로서 모두 이차성 혹은 전이성 안와종양이었다.

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Application of 3D Simulation Surgery to Orbital Wall Fracture : A preliminary Case Study

  • Choi, Jong-Woo
    • Journal of International Society for Simulation Surgery
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    • 제1권1호
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    • pp.16-18
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    • 2014
  • The orbit has a very special anatomical structure. The complex anatomical structure should be restored when we encounter the patient with orbital wall fracture. Unless these specific anatomy were reconstructed well, the patient should suffer from various complications such enophthalmos, diplopia or orbital deformity. In addition, because the patient has a his own specific orbital shape, individualized approach will be necessary. The aim of this trial is to try to restore the original orbit anatomy as possible based on the mirrored three dimensional CT images based on the computer simulation. Preoperative computed tomography (CT) data were processed for the patient and a rapid prototyping (RP) model was produced. At the same time, the uninjured side was mirrored and superimposed onto the traumatized side, to create a mirror-image of the RP model. In order to restore the missing skipped images between the cuts of CT data because of the thinness of the orbital walls, we manipulated the DICOM data for imaging the original orbital contour using the preoperatively manufactured mirror-image of the RP model. And we fabricated Titanium-Medpor to reconstruct three-dimensional orbital structure intraoperatively. This prefabricated Titanium-Medpor was then inserted onto the defected orbital wall and fixed. Three dimensional approach based on the computer simulation turned out to be very successful in this patient. Individualized approach for each patient could be an ideal way to manage the traumatic patients in near future.

공작기계용 힌지벨트형 칩컨베이어 핀헤드 성형공정 개발에 관한 연구 (A Study on Development of Pinhead Forming Process using Hinge Belt Typed Chipconveyor for Machine Tools)

  • 박동근;최치혁;이춘만
    • 한국정밀공학회지
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    • 제27권4호
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    • pp.27-32
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    • 2010
  • This paper presents an investigation into the pinhead forming process with the objective of finding the optimal forming conditions. In order to this, the orbital forming analysis of a heading MIG was carried out using the explicit finite element method. Relationships between temperature by forming of load and stresses, rake angle by forming final shape and stress distribution were investigated through analysises in order to find an efficient solution. As a result, the higher temperature and orbital rake angle were the better forming conditions.

Modeling Satellite Orbital Segments using Orbit-Attitude Models

  • Kim Tae-Jung
    • 대한원격탐사학회지
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    • 제22권1호
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    • pp.63-73
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    • 2006
  • Currently, in order to achieve accurate geolocation of satellite images we need to generate control points from individual scenes. This requirement increases the cost and processing time of satellite mapping greatly. In this paper we investigate the feasibility of modeling entire image strips that has been acquired from the same orbital segments. We tested sensor models based on satellite orbit and attitude with different sets of unknowns. We checked the accuracy of orbit modeling by establishing sensor models of one scene using control points extracted from the scene and by applying the models to adjacent scenes within the same orbital segments. Results indicated that modeling of individual scenes with $2^{nd}$ order unknowns was recommended. In this case, unknown parameters were position biases, drifts, accelerations and attitude biases. Results also indicated that modeling of orbital segments with zero-degree unknowns was recommended. In this case, unknown parameters were attitude biases.

내시경을 이용한 비강내 접근법과 속눈썹밑 절개를 동시에 이용한 안와내벽 재건술 (Two Portal Approach(Endoscopic Transnasal and Subciliary) in Medial Orbital Wall Fracture)

  • 장현;동은상;원창훈;윤을식
    • Archives of Plastic Surgery
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    • 제33권5호
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    • pp.552-556
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    • 2006
  • Purpose: As the use of computed tomographic scanning spread, the diagnosis of blow-out fractures of the medial orbital wall increased. Conventionally, the surgery of blow-out fractures in medial orbital wall was performed by various approaches with external incision or endoscopic approach. Although the field of orbital surgery has progressed significantly during the last decade, accurate realignment and replacement of component is difficult due to lack of visualization of the fracture site, blind dissection of the orbital wall, and difficulty in insertion of implant. In order to overcome these shortcomings, we explored the use of endoscopic transnasal approach together with subciliary approach. Methods: The entrapped periorbital tissues in the ethmoid sinus were completely reduced endoscopically, and the bone defect of medial orbital wall was reconstructed with $Medpor^{(R)}$ insertion via subciliary approach. This technique was applied to 13 patients who had medial orbital wall fracture. Results: The patients were followed-up for 3 to 24 months with an average of 9 months. The postoperative courses were satisfactory in all cases. Conclusion: The conjunction of endoscopic transnasal and subciliary approach technique seems to produce good results in medial orbital wall fracture.

오비탈 연삭시스템의 연삭가공 열변형 오차 해석 (Thermal Deformation Analysis of an Orbital Grinding System Grinding Process)

  • 이현민;최우천;조창래;조순주
    • 한국정밀공학회지
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    • 제33권7호
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    • pp.595-600
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    • 2016
  • An orbital grinding system uses a special motion to machine crankshafts in ships. When a crankshaft is operated, eccentric pins rotate and a grinding wheel moves in order to grind the pins. Thermal error caused by heat generated in the grinding process decreases the quality of the final product. In this study, the thermal error of an orbital grinding system caused by heat generation was investigated in order to predict the extent of thermal error that can occur during the grinding process. Since the machine position changes during orbital grinding, the pin part is divided into 30 degree intervals and heat is generated. Total thermal error was measured by summing the thermal errors associated with the pin and the grinding wheel. Total thermal error was found to reach a maximum at 60 degrees and a minimum at 210 degrees because of the shape of the crankshaft.

NMR for magnetite

  • Lee, Soonchil
    • 한국자기공명학회논문지
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    • 제22권4호
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    • pp.101-106
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    • 2018
  • Magnetite is the oldest magnet material known to mankind. It is getting attention again from solid state physics researchers now a days because it is one of the most strongly correlated electron systems. Spin, charge, and orbital orders are interplaying with lattice and involved in the Verwey transition where magnetization, conductivity, and structure changes suddenly. The peculiar ordering states above and below the transition temperature mainly originate from the coexistence of $Fe^{2+}$ and $Fe^{3+}$ ions in the B site of the inverse spinel structure. In particular, the state of the charge and orbital order was the oldest and most intriguing problem. NMR has made significant contribution to the investigation of this question. A. Abragam stated that there is no doubt that NMR is a very powerful tool for the study of ferromagnetic and antiferromagnetic materials. In this mini-review, a short history of NMR investigation of magnetite is presented, providing a support to Abragam's claim.

A Wrapping Method for Inserting Titanium Micro-Mesh Implants in the Reconstruction of Blowout Fractures

  • Choi, Tae Joon;Burm, Jin Sik;Yang, Won Yong;Kang, Sang Yoon
    • Archives of Plastic Surgery
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    • 제43권1호
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    • pp.84-87
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    • 2016
  • Titanium micro-mesh implants are widely used in orbital wall reconstructions because they have several advantageous characteristics. However, the rough and irregular marginal spurs of the cut edges of the titanium mesh sheet impede the efficacious and minimally traumatic insertion of the implant, because these spurs may catch or hook the orbital soft tissue, skin, or conjunctiva during the insertion procedure. In order to prevent this problem, we developed an easy method of inserting a titanium micro-mesh, in which it is wrapped with the aseptic transparent plastic film that is used to pack surgical instruments or is attached to one side of the inner suture package. Fifty-four patients underwent orbital wall reconstruction using a transconjunctival or transcutaneous approach. The wrapped implant was easily inserted without catching or injuring the orbital soft tissue, skin, or conjunctiva. In most cases, the implant was inserted in one attempt. Postoperative computed tomographic scans showed excellent placement of the titanium micro-mesh and adequate anatomic reconstruction of the orbital walls. This wrapping insertion method may be useful for making the insertion of titanium micro-mesh implants in the reconstruction of orbital wall fractures easier and less traumatic.

최악의 대기 조건 하의 공기조력 비행선 운전 (Aeroassisted Orbital Maneuvering in a Worst-Case Atmosphere)

  • 이병수
    • 제어로봇시스템학회논문지
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    • 제6권10호
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    • pp.936-941
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    • 2000
  • Advanced space transportation systems, such as the National Aerospace Plane or an Orbital Transfer Vehicle, have atmospheric maneuvering capabilities. For such vehicles the use of aeroassisted orbital transfer from a high Earth orbit to a low Earth orbit, with unpowered flight in the atmosphere, has the potential for significant fuel savings compared to exoatmospheric Hohmann transfer. However, to exploit the fuel savings that can be achieved by using the Earths atmosphere to reduce the vehicles energy, a guidance law is required, and it must be able to handle large unpredictable fluctuations in atmospheric density, on the order of ${\pm}$50% relative to the 1962 US Standard Atmosphere. In this paper aeroassisted orbital transfer is considered as a differential game, with Nature controlling the atmosphere density to yield a worst case (min-max fuel required) atmosphere, from which the guaranteed playable set boundary are achieved. Inside the playable set, it is guaranteed that the vehicle achieves the optimal atmospheric exit condition for the minimum fuel consumption regardless of the atmospheric density variations.

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3층 구조를 가지는 광 집적회로용 2차 궤도 각운동량 광 도파로 (A Three-layered Optical Waveguide of Second-order Orbital Angular Momentum Mode Guiding for Photonic Integrated Circuit)

  • 이인준;김상인
    • 한국전자통신학회논문지
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    • 제14권4호
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    • pp.645-650
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    • 2019
  • 본 논문에서는 기존의 l=1 궤도 각운동량 모드에 대해서만 연구가 이루어지던 광 도파로 구조를 개선하여 반도체 박막 공정으로 제작이 가능하고, l=1 및 l=2 궤도 각운동량 모드를 전송할 수 있는 광 집적회로용 실리콘 광 도파로를 유한차분법을 통하여 설계하였다. 설계된 광 도파로는 여러 층의 실리콘과 실리콘 산화막으로 이루어져 있으며, 두 고유 모드의 합성을 통하여 궤도 각운동량을 가지는 모드를 구현한다. 제안된 광 도파로의 2차 궤도 각운동량 모드의 전기장 분포를 통한 궤도 각운동량 계산 결과, 궤도 각운동량 양자수가 1차 및 2차 각각 l= 0.9642, 1.8766으로 이론치에 매우 근접한 값을 보였다.