STA-1: Special standard test rig for metrological analysis and certification of strain-gauge equipment

2010 ◽  
Vol 71 (11) ◽  
pp. 2447-2449
Author(s):  
A. I. Beklemishchev ◽  
G. V. Rodzevich ◽  
V. A. Sabrekov
2020 ◽  
Vol 1675 ◽  
pp. 012082
Author(s):  
I K Kabardin ◽  
V G Meledin ◽  
S V Dvoinishnikov ◽  
V A Pavlov ◽  
G V Bakakin ◽  
...  

2014 ◽  
Vol 29 (1) ◽  
pp. 15-22
Author(s):  
Jarosław Sarnecki

Abstract The article deals with laboratory test method for jet fuels thermal stability testing. Author described the reasons that led to test rig preparation, its construction and operation principles. Innovative test rig for jet fuels thermal stability testing enables research in wide thermal conditions and different pressures. Testing capabilities and advantages compared with currently used standard test method of jet fuels thermal stability testing according to ASTM D3241 have been also presented


2018 ◽  
Vol 880 ◽  
pp. 226-231 ◽  
Author(s):  
Adrian Sorin Rosca ◽  
Nicolae Craciunoiu ◽  
Ionut Geonea ◽  
Cristina Ploscaru

In this paper the design, experimental and numerical simulation of a test rig for stabilizer bars fatigue resistance study is presented. A virtual CAD of the test rig is developed, for design and simulation purposes. A dynamic simulation model is developed in ADAMS software, to study the stabilizer bar durability. Strain gauge transducers are used to measure the deformations of the stabilizer bar.


2010 ◽  
Vol 71 (11) ◽  
pp. 2483-2490 ◽  
Author(s):  
A. I. Samoilenko ◽  
V. K. Maskaev
Keyword(s):  
Air Flow ◽  

2010 ◽  
Vol 71 (11) ◽  
pp. 2450-2454
Author(s):  
A. I. Beklemishchev ◽  
G. V. Biryukov ◽  
Yu. K. Blokin-Mechtalin ◽  
V. M. Vlasenko ◽  
V. N. Chekrygin ◽  
...  

2012 ◽  
Vol 16 (suppl. 2) ◽  
pp. 605-615 ◽  
Author(s):  
Bozidar Bogdanovic ◽  
Zivan Spasic ◽  
Jasmina Bogdanovic-Jovanovic

Low-pressure axial fan impellers designed according to the principle of equal specific work of all elementary stages have blades whose profile near the fan hub is under a significantly larger inclination angle than at the impeller periphery. In order to minimize the spatial curvature of the fan blades and the fan hub length, impeller blades of low-pressure axial fans can be designed with different specific work of elementary stages, so that the specific work of elementary stages is smaller at the hub than at the periphery. This paper presents the operating characteristics of a low-pressure reversible axial fan with straight blade profiles, designed with different specific work of elementary stages. The fan was tested on a standard test rig, with air intake loading on the suction side of the fan.


2010 ◽  
Vol 4 (4) ◽  
pp. 389-393 ◽  
Author(s):  
Dilip C. Patel ◽  
◽  
Deepak P. Vakharia ◽  

A floating bush bearing is a kind of journal bearing in which the bushing will float between the journal and bearing. Knowing the frictional coefficient is important for the determination of wear loss and power loss conditions; an appropriate test rig is used to determine friction of floating bush bearings. The frictional coefficient of bearings in dry and lubricated conditions has been examined in experiments.


10.29007/lw5b ◽  
2018 ◽  
Author(s):  
Gaurav Patel ◽  
Akash Patel ◽  
Mukesh Makwana ◽  
Neeraj Chavda

Valves are widely used in numerous industries like Beverage, Food, Dairy, Cosmetic, Pharmaceutical and Biotech to serve various purposes. Hence, it is strongly needed that each valve must be tested thoroughly for proper functioning. The equipment used for testing of valves is known as test-rig. At present, no standard test-rig is available in the market for testing of valves. This study is a part of an attempt to develop a cost-effective customized test-rig for multiple valve testing. In present study, pressure-drop in various cross-sections of the proposed.


Author(s):  
Aravind Sivaraman ◽  
Sridhar Ranganathan ◽  
Shashank Tangirala ◽  
G. Lakshmi Narayana Rao

The objective of this work is to compare the quality of various diesel fuels using a normal engine and carrying out the test under the actual operating conditions of the engine, unlike the conventional test methods that uses standard test conditions. The standard test conditions involve the running of the diesel engine test rig at a speed of around 800 rpm, which is not the condition when the fuel is actually being used, as the operational speed of commercial engines is around 1500–2000 rpm. Also the non-engine based quality rating methods are not economically liable and are inaccurate as they depend too much on the chemical nature of the fuel. So, the objective of this work is to develop a generalized quality rating procedure with less number of parameters, with a simpler and cheaper method compared to other available methods. A single cylinder diesel engine was used to study the ignition quality of various reference fuels of known Cetane numbers. A relatively simple and compact setup was used, by modifying the existing test rig. The inlet manifold was incorporated with an airflow control valve so that the quantity of air let into the cylinder can be varied. The exhaust gas manifold was modified to enable easier observation of the exhaust gas. The single cylinder diesel engine was made to run at two distinct conditions, namely, the normal and white-puff / critical condition, with the reference fuels of known cetane numbers. The quantity of air available for the fuel to combust is the only difference between the two conditions. The air-fuel ratio of each fuel under both the conditions was continuously monitored. A correlation was developed between the critical air-fuel ratios and the corresponding Cetane numbers. From this correlation, a test fuel can be rated easily by finding the air-fuel ratio, by running it in the same engine at an identical load, at an instant when the “white puff” is observed.


Author(s):  
Paul Lyttek ◽  
Harald Roclawski ◽  
Martin Böhle ◽  
Marc Gugau

Standard test rigs for basic research on turbochargers usually do not provide the capability of periodically changing, instantaneous process values, which are characteristic for the real application of these turbines. The challenge of testing the performance potential of turbocharger turbines under pulsating inflow conditions is mainly originated by the complex compatibility of two main issues that need to be implemented at a test facility: Firstly, a special device is required that reproducibly provides real engine-like exhaust gas pulsations with some variability representing different engine operating conditions. Secondly, appropriate real time measurement techniques for all significant transient values are required to measure both, instantaneous turbine inflow conditions and turbine power output. This paper presents a new developed test rig that enables a preferably high overlap between the above mentioned supply of approximately real engine exhaust gas conditions and the fundamental and scientifically based attempt of unsteady gas flow examinations.


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