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Year 2007 No 2

Dubas L., Kulsiriwiwat T., Samneingjam K., Sritaveesinsub V., Wangyao P., Dubas S. T.
FORMATION OF SILVER-NANOPARTICLES COMPOSITE THIN FILMS
Keywords: layer-by-layer|silver|nanoparticles|film|
No 2 (2007), p. 147-155
  mag01.pdf (559 kB)
mag01_eng.txt (1 kB)  

Grosman F., Cyganek Z.
INFLUENCE OF MEFASS ROLLING PARAMETERS ON TEMPERATURE OF FORMED STRIP
Keywords: MEFASS process|rolling|change of the strain path|temperature|
No 2 (2007), p. 156-162
  mag02.pdf (2 MB)
mag02_eng.txt (2 kB)  

Marchewka Ł., Stobrawa J., Cwolek B., Hadasik E., Płachta A.
STUDY OF AN EFFECT OF TEMPERATURE, RATE AND DEGREE OF DEFORMATION ON THE STRUCTURE OF HARDLY DEFORMABLE CuPAg ALLOYS
Keywords: Cu-P alloys|brazing alloys|hardly-deformable alloys|dynamic recrystallisation|superplastic properties|plastometric tests|metallographic examination|
No 2 (2007), p. 163-172
  mag03.pdf (625 kB)
mag03_eng.txt (2 kB)  

Jabłońska M., Niewielski G.
PLASTIC DEFORMATION AND THE EFFECTS OF DYNAMIC RECRYSTALLIZATION IN AN ALLOY IN THE MATRIX OF ORDERED SOLID SOLUTION
Keywords: intermetallic alloys|dynamic recrystalization|hot compression tests|
No 2 (2007), p. 173-178
  mag04.pdf (2 MB)
mag04_eng.txt (1 kB)  

Niżnik B., Pietrzyk M.
RHEOLOGICAL MODEL FOR MICROALLOYED STEEL IN THE TWO-PHASE REGION OF TEMPERATURES, ACCOUNTING FOR THE INFLUENCE OF DEFORMATION AND PRECIPITATION ON THE
Keywords: niobium microalloyed steels|carbonitride precipitation process|dislocation density model|
No 2 (2007), p. 179-189
  mag05.pdf (1 MB)
mag05_eng.txt (2 kB)  

Horkavcová D., Rohanová D., Horváthová R.
PREPARATION OF CALCIUM PHOSPHATE COATING ON TITANIUM AND TITANIUM ALLOY AND STUDY OF ITS ADHESION TO SUBSTRATE
Keywords: titanium|titanium alloy|calcification|calcium phosphate layer|adhesion|tape and knife test|
No 2 (2007), p. 190-197
  mag06.pdf (2 MB)
mag06_eng.txt (1 kB)  

Petrík J., Javorčíková Z..
THE CAPABILITY OF HARDNESS MEASUREMENT PROCESS OF SUPERDURALUMINIUM
Abstract
The aim of the submitted work is to evaluate hardness measurement process capability of various qualitative standards of hardenable wrought aluminium alloy - superduraluminium. The standards were simulated by casting (two cooling rates, 4.5°C.s-1 and 20°C.s-1), heat treatment (cooling rate of casting 4.5°C.s-1: solution treatment 6 hours at 500°C ± 5°C with following quenching into water 40°C and natural age hardening 0, 48 and 96 hours at 20°C) and thermomechanical treatment (cooling rate of casting 20°C.s-1: solution treatment 6 hours at 490°C ± 5°C with following quenching into water 40°C and pressing with amount of deformation ??????? and natural age hardening 96 hours at 20°C).
The Al alloy „Superduraluminium“ (STN 42 4203) was used as an experimental material. This type of alloy although being practically the first heat treatable alloy to be discovered still finds wide application for many general engineering and aircraft structural purposes in the form of forgings, extruded bars and sections, sheet, plate, tube and rivets. The excellent properties of this material are exploited in automotive industry. The alloy has good fracture toughness , but shows signs of overheating at about 510°C.
The surface of samples was milled and ground by abrasive paper. Polished metallographic samples were etched with 25 % H2SO4 at 75°C and consequently with 0.5 % HF. The microstructure was evaluated according to STN 42 0491 and STN 42 0462. The average grain diameter was 41.65 ?m for cooling rate 4.5°C.s-1 and 21.55 ?m for cooling rate 20°C.s-1.
The quality of alloy was evaluated by Brinell (HBS5/250/30) hardness test according standard ISO 6506 (STN 42 0371). Hardness tester HPO 250, being up to standard STN EN ISO 6506 - 2 (42 0371) for maximum permissible error, was used as measuring instrument.
Because the Brinell ball makes the deepest and widest indentation and the test averages the hardness over a wider amount of material, which will more accurately account for multiple grain structures, and any irregularities in the uniformity of the alloy (typical for cast structure) and soft materials, the Brinell hardness test was applied.
Attempts to standardize the evaluation of the measurement processes capability can be observed for several years. The capability of measurement processes is searched by analogy with that of production processes. Process capability means the ability of the process to meet technological or other requirements. Measurement process capability is determined by total variation caused by random reasons influencing the process.
Measurement system analysis (MSA) is an experimental and mathematical method of determining how much the variation within the measurement process contributes to overall process capability. MSA involves gauge repeatability and reproducibility (GRR) studies to evaluate measurement systems. It is an interactive, multimedia, system designed to help engineers and quality professionals assess, monitor, and reduce measurement system variation. MSA helps us conform to ISO 9000 and ISO/TS 16 949:2002 requirements.
To make a GRR study, the same type of parts or samples (10 pieces), two appraisers (people who measure the parts, the appraiser A was “cadet”, the appraiser B “veteran”), one measurement instrument and 3 measurement trials, on each part, by each appraiser were used. The multiple trials were necessary to estimate repeatability %EV and multiple operators to estimate reproducibility %AV. Multiple parts allow to obtain better estimates of repeatability and reproducibility, as well as to estimate part variation %PV. Index %GRR represents the overall process capability and ndc (number of distinct product categories) is relative to resolution of measurement instrument.
As a general rule of thumb is the measurement system resolution ought to be at least one-tenth of the process variability. This demand is fulfilled, because the resolution is 0.22 HBS 5/250/30 and equivalent standard deviation is between 3.67 and 16.37 HBS 5/250/30.
As %GRR exceeds 3 0% (95.69 % cast state - cooling rate 4.5°C.s-1, 66.14 % cast state - cooling rate 20°C.s-1, 85.33 % quenched, 90.44 % natural age hardened 48 hours, 93.56 % natural age hardened 96 hours and 93.03 % thermomechanical treated) the used hardness measurement system was not capable. The number of categories (ndc) is less then 2, the measurement system is of no value in controlling the process. It is all noise and one part can not be said to be different from another. The inhomogeneity of tested material at cast state with low cooling rate and partial melting down of grain boundaries and formation of cracks and micro-voids at age hardened and thermomechanical treated states are the causal relation of low capability.

Keywords: capability|superduraluminium|Brinell hardness|
No 2 (2007), p. 198-207
  mag07.pdf (555 kB)
mag07_eng.txt (5 kB)  

Demeter J., Kijac J., Velgos J.
EVOLUTION OF THICKNESS OF REMAINING MgO-C REFRACTORY LINING IN BOF DURING CAMPAIGN
Keywords: magnesium-carbon refractory lining|basic oxygen furnace|skulls|gunning mixes|trunnions area|slag line area|
No 2 (2007), p. 208-213
  mag08.pdf (246 kB)
mag08_eng.txt (1 kB)  

Hyrcza-Michalska M., Lisok J., Sikorski Sz.
THE ANALYSIS OF PLASTIC FLOW OF LASER WELDED TUBES IN THE PROCESS OF HYDROMECHANICAL FORMING
Keywords: laser welded blanks|tubular welded blanks|formability|hydroforming|hydromechanical forming|hydro-bulging|strain analysis|
No 2 (2007), p. 214-220
  mag09.pdf (1 MB)
mag09_eng.txt (2 kB)  

Tkocz M., Kusiak J., Grosman F.
RECOMMENDATIONS FOR SELECTION OF PARAMETERS OF COGGING IN V-DIES
Keywords: open-die forging|cogging|drawing out|V-dies|state of stress|
No 2 (2007), p. 221-228
  mag10.pdf (1 MB)
mag10_eng.txt (2 kB)  

Szkliniarz W.
EFFECT OF INITIAL MICROSTRUCTURE ON Ti-48Al-2Cr-2Nb ALLOY PLASTICITY
Keywords: TiAl-intermetallic phase based alloys, heat treatment, deformation, compression test, microstructure
No 2 (2007), p. 229-235
  mag11.pdf (516 kB)
mag11_eng.txt (2 kB)  

Špánik J., Krochmal K.
PARAMETERS OF HOT EXTRUSION PRESSING OF ALPHA BRASS
Keywords: hot extrusion pressing|alpha brass|surface cracks|brass CuZn30|deformation rate|extrusion ratio|extrusion speed|
No 2 (2007), p. 236-243
  mag12.pdf (367 kB)
mag12_eng.txt (2 kB)  

Wangyao P., Polsilapa S., Sopon P., Panich N., Chuankrerkkul N.
RE-HEAT TREATMENTED MICROSTRUCTURES AND GAMMA PRIME PARTICLE COARSENING BEHAVIOR AT 1000˚C OF CAST NICKEL BASE SUPERALLOY, IN-738
Keywords: rejuvenation|re-heat treatment|microstructural repair|gamma prime particle coarsening|nickel base superalloy|
No 2 (2007), p. 244-252
  mag13.pdf (842 kB)
mag13_eng.txt (2 kB)  

Valíček J., Hloch S., Ohlídal M.
SURFACE MICROTOPOGRAPHY OPTICAL DETECTION CREATED AT ABRASIVE WATERJET MACHINING
Keywords: abrasive waterjet|shadow method|cutting mechanism|
No 2 (2007), p. 253-261
  mag14.pdf (642 kB)
mag14_eng.txt (1 kB)  

Boryca J.
THE EFFECT OF LOSS OF STEEL AND THICKNESS OF SCALE LAYER ON THE SCALE ADHESION FOR CONSTANT VALUE EXCESS COMBUSTION RATIO
Keywords: scale|scale adhesion|loss of steel for scale|heating charge|heating technology|
No 2 (2007), p. 262-268
  mag15.pdf (300 kB)
mag15_eng.txt (757 B)  

Vadász P., Rabatin Ľ.
THE CORROSION OF BASIC CARBON REFRACTORY MATERIALS BY OXIDIZING SLAG
Keywords: refractory material|carbon|slag|corrosion tests|
No 2 (2007), p. 269-275
  mag16.pdf (475 kB)
mag16_eng.txt (1 kB)  

Rákoš J.
SUBATOMIC NANO-LAYER OF STANNUM DIOXIDE AS A MASER PART OF SOLAR RADIATION
Keywords: Subatomary stannumdioxide layer|nanomaser|spectral gravitation prism. PACS: 02.70.Ns|34.50.Ez|42.50.Gy|61.46.Hk|78.20.Ek|
No 2 (2007), p. 276-285
  mag17.pdf (1 MB)
mag17_eng.txt (955 B)