• 제목/요약/키워드: Static Pressure Error

검색결과 41건 처리시간 0.024초

기압 고도의 정밀도 향상을 위한 정압 오차 모델에 관한 연구 (Study on Static Pressure Error Model for Pressure Altitude Correction)

  • 정석영;안창수
    • 한국항공우주학회지
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    • 제33권4호
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    • pp.47-56
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    • 2005
  • 무인기의 INS/GPS/기압고도계 결합항법 시스템에서 수직채널감쇠루프를 사용하여 고도 오차를 보정할 때 비행 고도의 오차를 감소시키기 위해서 기압고도계의 정밀도를 향상시켜야한다. 피토정압관을 사용하여 기압 고도를 측정할 때 비행 속도와 자세 등의 변화에 따라 피토정압관 주위의 압력이 변하여 정압 오차에 의한 기압 고도의 오차를 유발한다. 정압 오차를 보정하기 위하여 풍동 시험과 CFD, 비행 시험 등의 자료를 이용하여 피토정압관 측정 압력의 변화를 분석하고 받음각과 비행 속도에 따른 압력 오차의 모델을 수립하였다. 비행 속도 변화에 의한 오차를 보정하기 위하여 피토정압관의 차압과 차압/정압 비를 사용한 두 가지 오차 모델에 대하여 압력 섭동에 대한 민감도 해석을 하였고 비행 시험에 적용하여 차압/정압 비를 사용한 모델이 고고도 비행 특성이 우수하다는 결론을 얻었다.

3차원 소형축류홴의 공력특성에 대한 난류모델평가 (Evaluation of the Turbulence Models on the Aerodynamic Performance of Three-Dimensional Small-Size Axial Fan)

  • 김장권;오석형
    • 동력기계공학회지
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    • 제18권6호
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    • pp.13-20
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    • 2014
  • The steady-state, incompressible and three-dimensional numerical analysis was carried out to evaluate turbulent models on the aerodynamic performance of a small-size axial fan(SSAF). The prediction performance on the static pressure of all turbulent models is going downhill at the high static pressure and low flowrate region, but has improved at the axial flow region. In consequence, all turbulent models predict the static pressure coefficient with an error performance less than about 4% after the region of the flowrate coefficient of about 0.14. Especially, the turbulent model of SST $k-{\omega}$ shows the best prediction performance equivalent to an error performance less than about 2% on the static pressure.

소형 항공기 개발 동정압계통 오차 확인 비행시험 사례 (Study on Flight Test Practice of the Small Civil Airplane Development for Pitot-Static System's Error Identification)

  • 김찬조;서지한;이원중
    • 항공우주시스템공학회지
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    • 제7권3호
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    • pp.33-38
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    • 2013
  • The air data measured from the static pressure, the dynamic pressure and etc. of an airplane is used for calculation of many flight parameters(altitude and airspeed and so on) and these values applied to flight safety and navigation flight. The pitot-static system of the development airplane is calibrated by finding of pitot-static system's error using tower fly-by, trailing cone method and etc. This paper is describing for the introduction of the trailing cone method and major items for test planning, preparation, operation and results for air data calibration flight test performed, considering efficiency and safety during KC-100 development project.

서보밸브 스풀-슬리브 형상공차가 압력 정특성에 미치는 영향 연구 (Effect of Spool-Sleeve Geometry on Static Pressure Characteristics of Servo Valves)

  • 김성동;손성회;함영복
    • 드라이브 ㆍ 컨트롤
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    • 제13권1호
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    • pp.34-42
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    • 2016
  • This study studied how the clearance, overlap and mismatch errors of spool-sleeve affect the static pressure characteristics of a servo valve. A computer simulation model was established as a direct acting servo valve and a series of simulations was conducted for various values of clearance, overlap and mismatch errors. Pressure gain decreased as the clearance increased. The overlap also affects the pressure gain and was similar to the effect of clearance. Asymmetry of the pressure plot got worse and worse as the mismatch error increased.

점탄성유체의 압력측정용 벽공부근의 유동모양에 관한 실험적 연구 (An Experimental Study on the Flow Pattern in the Vicinity of Pressure Measuring Hole of the Viscoelasitc Fluids)

  • 김춘식
    • Journal of Advanced Marine Engineering and Technology
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    • 제4권1호
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    • pp.23-31
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    • 1980
  • The fluid static pressure has been generally measured by means of a small hole leading to a measuring instrument. In case of viscoelastic fluids, however, it has been shown experimentally that a systematic error exists in measuring the static pressure by means of the small hole becuase viscoelasitc fluids have many properties that can not be observed in Newtonian fluids. In this paper, in order to examine the mechanism of the errors in measuring the static pressure of viscoelasitc fluids, flow patterns in the vicinity of static pressure measuring hole were photographically taken and observed graphically. The experiments to take photographs of flow patterns were performed by a parallel plate channel with the steady two-dimensional shear flow of viscoelastic fluids. Results of the experiment are classified as following three regions; (1) Arched symmetrical flow pattern region. (2) Asymmetrical flow pattern region. (3) Rectilinear symmetricl flow pattern region.

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노인에서 임상적 균형평가 지수들의 유용성 : 힘판을 이용한 균형평가와의 상관관계 (The Usefulness of Clinical Balance Tests in Elderly : Correlation of Balance Evaluation using by Forceplate)

  • 우영근;황수진;이우형
    • PNF and Movement
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    • 제8권1호
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    • pp.67-77
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    • 2010
  • Purpose : The purpose of this study was to investigate the usefulness of clinical balance tests through the correlation of balance evaluation using by forceplate in elderly. Methods : Thirty nine healthy elderly subjects (14 males, 25 females) participated in the study. The subjects were evaluated with clinical balance tests [(Berg balance scale (BBS), Functional reach test (FRT), Tinetti's performance oriented mobility assessment (POMA), and one leg standing (OLS)]. Static balance evaluation was assessed by using forceplate. Center of pressure (COP) parameters were obtained using it as total path distance, total sway area, X mean frequency and Y mean frequency for 20 seconds in the following conditions: (1) comfortable standing with eyes opened and closed, (2) uncomfortable standing with eyes opened and closed. After static balance evaluation tested, dynamic balance evaluation was assessed. COP parameters were error distance and area during sine curve trace. COP parameters were movement time, error distance, and maintained time in the circle during COP movement task. Results : Clinical balance tests showed statistically significant correlation between static and dynamic balance evaluations. Among the clinical balance tests, the BBS, POMA, and OLS showed significant correlation with to assess the balance ability of elderly in clinical setting both evaluations. Conclusion : Clinical balance tests can be recommended in clinical setting because of low costs and simplicity.

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기능적 발목관절 불안정성의 등속성 근력과 균형 및 보행 중에 근활성도와 발바닥압의 평가 (Evaluation of Muscle Activity and Foot Pressure during Gait, and Isokinetic Strength and Balance in Persons with Functional Ankle Instability)

  • 이선아;김아람;유경태;이호성
    • 대한물리의학회지
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    • 제13권3호
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    • pp.27-37
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    • 2018
  • PURPOSE: The purpose of this study was to investigate and evaluate muscle activity and foot pressure during gait, and isokinetic strength and balance in persons with functional ankle instability (FAI). METHODS: Nine healthy subjects (CON, n=9) without FAI and 11 patients (FAI, n=11) with FAI participated in the study after having been screened with an ankle instability instrument and a balance error scoring system. In addition, FAI was classified as non-involved (FAI-N) or involved (FAI-I), and CON was classified as dominant or non-dominant. All subjects were evaluated for isokinetic strength (plantar flexion, dorsiflexion, inversion and eversion of $30^{\circ}/sec$ and $60^{\circ}/sec$), balance (static and dynamic), muscle activity (tibialis anterior, peroneus longus and gastrocnemius) and foot pressure (static and dynamic) during gait. RESULTS: Results showed that plantar flexion (p<.05), dorsiflexion (p<.05), inversion (p<.01) and eversion (p<.00) of $60^{\circ}/sec$ were significantly decreased in FAI-I compared to those in FAI-N and CON. C 90 of static balance with eyes open (p<.01) and closed (p<.00) were significantly increased in FAI compared to those in CON. Forward position of dynamic balance (p<.01) was significantly decreased in FAI compared to that in CON. Gastrocnemius and peroneus longus of dynamic muscle activity (p<.01), left and right weight distribution of static foot pressure (p<.00) and pressure distribution of dynamic foot pressure (p<.00) were significantly decreased in FAI-I compared to those in FAI-N. CONCLUSION: We demonstrated that ankle strength, balance, muscle activity and foot pressure were significantly correlated with FAI.

다공질 공기 베어링의 강성 특성에 관한 실험 연구 (An Experimental Study on Porous Air Bearing Stiffness Characteristics)

  • 정순철;이성혁;이재응;지홍규;이동진;류제형;최형길;김혁
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2005년도 추계학술대회논문집
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    • pp.75-78
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    • 2005
  • In this paper, an experimental study on porous air bearing stiffness for ultra precision positioning system was performed. In general manufacturer provide bearing stiffness under specific air pressure, but the air pressure used in the field is different. Therefore it is necessary to know the stiffness of air bearing under the pressure used in the field. In order to know that, experimental device which can realize actual operating conditions was made. Using this device, static and dynamic stiffness of air bearing can be obtained. As a result, displacement error occurred around 1 $\mu$m at recommended load.

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초음파간섭 수은주압력계와 정적법 중진공 국가표준기 상호비교 (Inter-comparison between ultrasonic interferometer manometer and medium vacuum standards by static expansion method)

  • 홍승수;임인태;신용현;정광화
    • 한국진공학회지
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    • 제14권3호
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    • pp.103-109
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    • 2005
  • 정적법을 이용하여 새로운 중진공 국가표준기를 개발하였다. 이 장치의 성능평가를 위해 측정범위가 각각 133pa과 1,333pa인 두 개의 용량혈 진공게이지를 전달표준기로 사용하여 초음파간섭 수은주압력계와 중진공 표준을 상호비교하였다. Error normalized (En) 값으로 분석한 결과 교정압력 $3pa\;\sim\;100pa$에서 두 표준기는 합성불확도 범위 내에서 잘 일치하고 있음을 알 수 있었다.

KTX용 터보팬 블레이드 개발 (The Development of Turbo-Fan Blade for KTX)

  • 장영민;권오운;김성준
    • 산업기술연구
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    • 제29권B호
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    • pp.41-45
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    • 2009
  • The new cooling fan for various parts & equipments of KTX is developed and evaluated to improve fan performance and durability. The characteristic curve of the developed fan is obtained according to KSB 6311 of performance test regulation. 70 degree of the installation angle of blade makes the fan to produce a maximum flow rate. This angle is found out through trial-error and is confirmed through the verification test. In order to improve the blade strength, the blade is produced by a draw forming. The adoption of AL50 reduces a fan weight by 6 kg. The new blade makes a static pressure 170 (mmAq), a discharge rate $140(m^3/min)$, a rotational speed 2886 (rpm) at the power 10 kw. which results 54% of the static pressure improvement relative to the original blade.

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