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Yuanchao Yang, Jin Yue
DETERMINATION OF THE DISTORTION COEFFICIENT OF A 500 MPA FREE-DEFORMATION PISTON GAUGE USING A CONTROLLED-CLEARANCE ONE UP TO 200 MPA

Cross-float experiments between a 500 MPa free-deformation (FD) piston gauge and a 200 MPa controlled-clearance (CC) one were carried out at a series of system pressures and jacket pressures. The two characteristics of the CC piston gauge, the zero clearance jacket pressure and the jacket pressure coefficient, were determined based on the Heydemann-Welch model. After that, the pressure dependence of the effective area for the FD piston was calculated using the cross-float data, from which the pressure distortion coefficient was determined to be 8.46 × 10-7 MPa-1. The result was about 19% larger than the one obtained by the Lame equation.

Wu Jian
REALISATION OF PRIMARY PRESSURE MEASUREMENT SYSTEM

NMC recently established the primary deadweight pressure standards in the range from 10 kPa to 1 MPa. The primary standard includes two piston-cylinder (PC) units, the diameters of which derive the pressure values. While two other of the PC units serve as the reference in the higher range of 24 kPa to 10 MPa are traceable to the primary PC units through cross-floating measurement method. Together with a primary laser manometer and a hydraulic deadweight pressure standard, NMC realises the pressure measurement system from 1 Pa to 400 MPa. This paper describes the method of realisation of the pressure unit at NMC.

W. Sabuga, R. Haines
DEVELOPMENT OF 1.6 GPA PRESSURE-MEASURING MULTIPLIERS

Two 1.6 GPa pressure-measuring multipliers were developed and built. Feasibility analysis of their operation up to 1.6 GPa, parameter optimisation and prediction of their behaviour were performed using Finite Element Analysis (FEA). Their performance and metrological properties were determined experimentally at pressures up to 500 MPa. The experimental and theoretical results are in reasonable agreement. With the results obtained so far, the relative standard uncertainty of the pressure measurement up to 1.6 GPa is expected to be not greater than 2·10-4. With this new development the range of the pressure calibration service in Europe can be extended up to 1.5 GPa.

Andreas Hebestreit
PROBLEMS OF DYNAMIC PRESSURE MEASUREMENT

Pressure sensor elements are in general able to swing. Some data sheets tell the damping constant and the natural frequency. These dynamic characteristics influence the measuring values in case the pressure alters very fast. If the pressure changes with frequencies which are in the near of the resonance frequency of the sensor large measuring deviations will occur. But we did not learned yet how much the damping constant and the natural frequency of the sensor will be, when it is mounted and has contact with the fluid.

Sung Soo Hong
AN ANALYSIS ON HIGH PRESSURE DYNAMIC CALIBRATORS USED IN THE DEFENSE AREAS

Up to now, there is no the international certified standard calibrator of dynamic pressure because the definition of dynamic pressure is not determined. Even though a few dynamic calibrators were designed, manufactured and used in a variety of industrial areas, they are not traceable to the international standards in practical. At present, the determination of response characteristics to pressure transducers is routinely limited to static calibration, while using a deadweight pressure standard. The deadweight device is a primary static pressure standard used to generate precise pressure under the assumption that the static and dynamic responses of the transducer in static calibration are equivalent. However, the differences in transducer response between static and dynamic events can lead to serious measurement errors. Dynamic techniques are required to calibrate pressure transducers to meet dynamic events in milliseconds In this paper, the calibration techniques are surveyed and classified in the area of dynamic pressure and finally analyzed in terms of the waveform, range, transition time and method of dynamic pressure so that its analysis result can be informative and helpful for those who are interested in dynamic pressure for better measurement.

J. Y. Lim, S. Y. In, S. K. Lim, W. Cheung
ESTABLISHMENT OF THE ENGINEERING RELIABILITY EVALUATION SYSTEM FOR THE DEVELOPMENT OF UHV PUMPS

Engineering reliability evaluation system has been under establishment for the development of ultrahigh (UHV) vacuum pumps such as 3,600 L/s cryo and 2,500 L/s turbo-molecular pumps (TMP). This paper briefly addresses the utilization of the characteristics evaluation system already developed in KRISS to design, characterize, and establish the reliability evaluation system through two project years ahead. The purpose ensured of the main national project is the completion of the commercialization of UHV pumps in recognition of international engineering reliability.

Suelí Fischer Beckert, Gustavo Domeneghetti, Danielle Bond
USE OF POOLED STANDA DATA IN CALCULATING

The specification of mechanical properties is essential for adequate choice of material, as well as for design and manufacturing of components and products. recognised that the present state of uncertainties in testing activities is not as comprehensive as in the calibration fields. This paper presents guidelines calculation of measurement uncertainty (tensile strength and percentage elongation after fracture making the type A evaluation from historical data. also demonstrated that the application of deviation has larger representativeness than the use of diameter and load standard deviations.

Hagyong Kihm, Ho-Soon Yang, Il-Kweon Moon, Yun-Woo Lee
ADJUSTABLE BIPOD FLEXURES FOR MOUNTING MIRRORS IN A SATELLITE TELESCOPE

A new mirror mounting technique applicable to the primary mirror in a space telescope is presented. Conventional bipod flexures for mounting mirror bosses are changed to have mechanical shims to adjust gravitational distortions at the mirror surface. Analytical results using finite element methods are compared with experimental results from an optical interferometer. Vibration tests qualified their use in space applications.

Il Kweon Moon, Sangon Lee, Juhee Lim, Joung Ung Lee, Ho-Soon Yang, Yun Woo Lee
ESTIMATION OF IMAGE MOTION FOR WIDE FIELD TELESCOPE UNDER WIND LOADS

To evaluate opto-mechanical performances under a certain level of windy environment, an estimation of the image motion is useful for a wide field telescope optical system. The wide field telescope is a Cassegrain telescope composed of two hyperbolic mirrors, a 0.5 m primary mirror and a 0.2 m secondary mirror, and correction lenses and then covers a 2° field of view. We performed the image motion analyses from the dynamic response based on the line of sight (LOS) sensitivity equations, which had been derived from the optical design program Code V, integrated in the finite element models by using NX NASTRAN.

A. Ho-Soon Yang, B. Hagyong Kihm, C. Il Kweon Moon, D. Gil-Jae Jung, E. Se-Chol Choi, F. Kyung- Joo Lee, G. Hong-Yeon Hwang, H. Sug-Whan Kim, I. Yun-Woo Lee
AN ATHERMALIZATION LENS BARREL STRUCTURE FOR IR OPTICAL SYSTEM

We have developed an athermalization barrel containing 4 IR lenses. It consists of two materials with different coefficients of thermal expansion (Invar and aluminum). A finite element analysis and the experiment data showed that this new athermalization barrel has a defocus error sensitivity of 8.1 nm/°C, which satisfies our requirement for high resolution camera.

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