• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2007년도 추계학술대회논문집
• /
• pp.281-286
• /
• 2007

Needs of fuel's performance evaluation for the dual-cooled fuel pellet (annular shape) necessitate the irradiation test in the test reactor. Irradiation test rig for the HARARO reactor, which is a special-purposed equipment used for material, irradiation and creep test, must satisfy the operational requirement on the hydraulic characteristics and structural integrity. In this paper, pressure drop and flow-induced vibration test for the newly developed non-instrumented test rig were carried out using FIVPET as a out-pile evaluation test. The test results show that the new test rig satisfy the HANARO operational requirement with sufficient margin. The spectral response characteristics of the flow-induced vibration of the test rid were also discussed.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
• /
• pp.1445-1449
• /
• 1996

To evaluate of active suspension, it is necessary for special equipment - so called Test Rig which can perfectly realize the road condition and the impact from the road. And most of the test rig systems controlling force accurately and rapidly consist of electro-hydraulic servo mechanism, and they need robust controller which can endure outer road change. But in the case of PID controller, we should choose its best gains by trial and error method, and once its gains are fixed, they cannot get changed, so we should reset PID controller gains respectively when the road is changed. Therefore based on the load pressure feedback compensation method, our aim at constructing electro-hydraulic test rig is not affected by various road disturbance.

• 대한기계학회논문집B
• /
• 제25권5호
• /
• pp.634-644
• /
• 2001

The test facility of a 1/60-scale model for train-tunnel systems has been recently developed to investigate the effects of tunnel portal shapes, hood shapes and air-shafts for reducing the micro-pressure waves radiating towards the surroundings from the tunnel exit. The present test rig has been advanced from a 1/70-scale facility at NLR in Netherlands. The NLR test rig has the two-wise guidance system that needs two ears attached on the external surface of a model train nose. Therefore, their train models have irregular nose shapes. The main characteristics of the present facility are that the train model is guided by only one wire from the compressed air launcher to the absorber parts of test facility and the wire guidance hole is located at the axial center of a train model. In the present test rig, after a train model is launched, the air jet from the launcher does not enter the tunnel model. Experimental results were compared with numerical predictions to prove the performance of the test facility.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2011년도 제37회 추계학술대회논문집
• /
• pp.977-980
• /
• 2011

본 논문에서는 항공우주연구원에서 개발중인 1단 저압 축류압축기 성능시험리그의 개발에 대한 내용을 소개하고자 한다. 성능시험리그는 유동 입구부, 동익단, 정익단, 축, 리그 하우징, 베어링 하우징 및 유동 출구부로 구성되어 있다. 로터와 회전축을 단순화하여 회전동역학 해석 결과를 바탕으로 회전축을 설계하고 입 출구 유로의 유동해석을 통해서 시험리그 형상설계를 최적화하였다.

• International Journal of Railway
• /
• 제2권2호
• /
• pp.93-97
• /
• 2009

The experiments for aerodynamic characteristics of railway acoustic screen are performed using 1/61 scaled-down moving model rig facility which employs an axis symmetry and one wire guidance method. The launching mechanism is an air-gun type. The train model for the experiment is the high speed train (Korea Train Express: KTX) and the tested speed is about 300 km/h. The tested train length is 61 em which is corresponding to two units of KTX train. The cross sectional area and weight of train model are 0.00264 $m^2$ and 287 g, respectively. The Reynolds number based on the model train length is $1.2{\times}10^7$. The strength of pressure wave is measured using piezo typed pressure sensor. The measured pick value of pressure was as high as 365 Pa in the shortest gap between the acoustic screen and model train. The measured pressure is well compared with the field test data of mc 779-1 [2] values. However, the experimental data were slightly lower than the mc 779-1 values. The results show the model test can be used as a substitute for the field test.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2000년도 춘계학술대회논문집B
• /
• pp.611-618
• /
• 2000

The test facility of the 1/60-scale models for the train-tunnel interactions was recently developed to investigate the effects of entry portal shapes, hood shapes and air-shafts for reducing the micro-pressure waves radiating to the surroundings of the tunnel exits by KRRI in Korea. The launching system of train model was chosen as air-gun type. In present test rig, after train model is launched, the blast wave by the driver did not enter to inside of the tunnel model. The train model is guided on the one-wire system from air-gun driver to the brake parts of test facility end. Some cases of the experiments were compared with numerical simulations to prove the test facility.

• 대한기계학회논문집B
• /
• 제37권1호
• /
• pp.1-7
• /
• 2013

본 연구는 보조동력장치에 적용되는 구심터빈의 공력성능시험을 한국항공우주연구원의 고온 터빈 시험리그에서 수행한 결과이다. 리그시험을 위하여 터빈의 형상은 동일하되 팽창비, 마하수 및 유량계수는 실제 엔진과 동일한 값이 되도록 상사법칙을 적용하여 시험하였다. 설계 팽창비는 3.096이며, 상사된 설계회전수는 34909 rpm이고 상사된 터빈 입구온도는 $160^{\circ}C$이다. 터빈의 입구에는 익형 형상의 노즐이 설치되었으며 터빈 휠의 직경은 175.74mm이다. 시험을 통하여 터빈의 성능지도가 생성되었으며 터빈 입구에서의 상세 유동이 측정되었다. 노즐의 허브면에서 측정한 압력과 노즐의 쉬라우드 면과 터빈 휠 케이싱에서 측정한 압력 분포를 볼 때 터빈 내부에서의 팽창과정이 적절함을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2008년도 제31회 추계학술대회논문집
• /
• pp.149-152
• /
• 2008

초소형 터보제트엔진에 적용되는 슬링거연소기를 개발하고 리그시험을 수행하였다. 슬링거연소기에 적용하기 위하여 고속으로 회전하는 회전연료노즐을 설계, 제작하고 분무시험을 통해 연소에 적합한 액적크기와 분포를 얻었다. CFD를 이용해 연소기 내부 유동장을 해석하였으며, 연소리그시험을 통해 설계점에서 11.2%의 압력손실, 99.8%의 연소효율을 달성하였다.

• 한국가스학회지
• /
• 제11권4호
• /
• pp.12-16
• /
• 2007

천연가스 자동차에 탑재되어 있는 연료압력 레귤레이터는 연료분사시스템의 압력을 일정하게 유지하는 역할을 한다. 연료압력의 정확한 제어는 천연가스 자동차가 가지고 있는 높은 효율성과 청정성을 십분 활용하기 위해서 반드시 필요한 사항이다. 본 연구에서는 천연가스 레귤레이터의 성능을 정확하게 평가할 수 있는 고압실험장치를 구축하였으며, 이 장치를 이용하여 두 가지 방식의 천연가스 레귤레이터를 평가하고 상호 비교를 하였다. 레귤레이터 밸브시스템의 설계에 따라 여러 가지 레귤레이터 성능 특성 중 동적응답과 Creep특성이 영향을 많이 받는 것으로 나타났으며, 레귤레이터 입구 압력이 높을 경우 출구 가스의 온도가 급격히 감소하는 것으로 나타남으로써 아이싱문제를 효과적으로 방지할 수 있는 방안이 마련되어야 함을 확인할 수 있었다.

• 한국군사과학기술학회지
• /
• 제7권4호
• /
• pp.133-137
• /
• 2004

A simplified test rig to simulate high-altitude environments was designed by analyzing the AEDC (Arnolds Engineering Development Center) report regarding simulated altitude testing. The test rig consists of a vacuum chamber, a supersonic nozzle connected to a cold-gas supplier and a diffuser. The preliminary tests were conducted to validate the AEDC design concepts. The test results showed that sub-atmospheric pressure(1.0psia) environments were realized inside the vacuum chamber and the design concepts were confirmed.