Welding and allied processes. Quality classification and dimensional tolerances of thermally cut (oxygen/fuel gas flame) surfaces

1995 ◽  
Author(s):  
M.A. Cole ◽  
R. Walker

Abstract Over the past 30 years, there has been considerable interest in the development of thermally sprayed thermal barrier coatings (TBCs) for aerospace and land based turbine applications. The use of TBCs enables higher operating temperatures, resulting in significant fuel efficiency savings. This paper reports on the development of dense Yttria Stabilised Zirconia (YSZ) thermal barrier coatings produced by High Velocity Oxygen Fuel (HVOF) spraying using acetylene as the fuel gas. The use of a high temperature gas erosion rig allowed the controlled evaluation of erodent size, velocity, impact angle, and temperature on coating performance. The work also covers the optimization of process parameters, including powder morphology, stand-off distance, oxygen to fuel ratio, gas pressures, and flowrates, and their effect on coating characteristics such as deposition efficiency, microhardness, and surface roughness.


2012 ◽  
Vol 188 ◽  
pp. 422-427 ◽  
Author(s):  
Iosif Hulka ◽  
Viorel Aurel Şerban ◽  
Kari Niemi ◽  
Petri Vuoristo ◽  
Johannes Wolf

The aim of the work was to study the microstructure and wear properties of fine-structured HVOF and HVAF sprayed WC-10Co-4Cr coatings prepared from powder having submicron-sized tungsten carbides. The coatings were deposited by HVOF (High Velocity Oxygen Fuel) and HVAF (High Velocity Air Fuel) using propane as a fuel gas in both processes, and using oxygen or air as oxidizing gas for combustion, respectively. Nitrogen was used as carrier gas for the powder. Commercially available agglomerated and sintered cermet powder with main carbide sizes under 500 nm was used in this study. Scanning electron microscopy (SEM) and X-ray diffraction were performed in order to characterize the powder and the microstructures formed during the spraying processes. The microhardness HV0.3 of the coatings was investigated and the pin on disk test was used to determine the sliding wear behaviour. The rubber wheel abrasion test was performed in order to determine the abrasion wear resistance of the coatings.


2020 ◽  
Vol 22 (2) ◽  
pp. 135-149
Author(s):  
O.G. Fawole ◽  
X.-M. Cai ◽  
I. Nikolova ◽  
A.R. MacKenzie

This study proposes an approach for estimating the emission of soot, carbon monoxide (CO) and carbondioxide (CO ) from a typical gas flare. The estimations depend on the quantity and varying composition of the 2 natural gas, flame dynamics (represented by the fire Froude number, Fr ) and the equivalence ratio, f, of the fuel- f air mixture. Soot emission estimates are presented as a function of fire Froude number for gases used in labbased  test in order to validate the scheme and for two real-world fuel gas compositions. The mass-weighted carbon-hydrogen ratio (C:H) of the fuel gas compositions are 0.25 and 0.29 which are two extreme cases in terms of density. The soot yield of the lab-based test case was scaled up to estimate the soot yield of a full scale flare using the Richardson number as the scaling parameter. When all other variables are held constant at values characteristics of real-world flares, a difference of 16 % in the fuel-gas density, as indicated by the carbonhydrogen ratio, results in an increase of the emission factors (EF) of soot, CO and CO by factors of ~3, ~1.4 2 3 and ~1.7, measured in g/m , respectively. For both fuel gas compositions, the ratio of EF to EF at the fuel- soot CO lean region f < 1) is higher. The ratio lies in the range 0.031 – 0.13 and 0.0012 – 0.0055 for the fuel-lean (f < 1) and fuel-rich (f > 1) regions, respectively. The approach proposed and results obtained may be adopted to generate emissions inventories of emission species associated with gas flaring on regional and global scales. Keywords: gas flaring; soot; natural gas; emission factor; black carbon; equivalence ratio


Author(s):  
E. Lugscheider ◽  
C. Herbst-Dederichs ◽  
L. Zhao

Abstract The paper deals with an analysis of particle behavior in a HVOF-jet as a function of process parameters. The experiments were carried out using a commercial HVOF gun with hydrogen as fuel gas. A commercial 316 L stainless steel powder was used for spray material. The experiments were conducted by using on-line particle diagnostics in order to simultaneously detect particle velocity, temperature and diameter. The results were correlated with caught spray powder and splats. The experiments released that among many parameters the oxygen/fuel gas ratio is the most important parameter. It was found, that fragmentation of partially melted particles in a supersonic jet is not a neglectable phenomenon. It may cause excessive oxidation inflight and therefore is to be avoided in the production of oxygen-poor coatings. Furthermore, it was found that velocity or temperature measurements of particles have to be interpreted very carefully in order to characterize the process. Without taking a possible change of the particle size due to inflight fragmentation into consideration either measurement value will lead to very limited information benefit.


2017 ◽  
Vol 58 (7) ◽  
Author(s):  
Sebastian Bürkle ◽  
Lukas G. Becker ◽  
Maria Angela Agizza ◽  
Andreas Dreizler ◽  
Volker Ebert ◽  
...  

Author(s):  
Margot Brundage ◽  
Robert F. Dunn
Keyword(s):  

Re-embedding of plastic impregnated tissue blocks is easily accomplished when a combination of carnuba and Tenax dental waxes is used. This method is particularly helpful when combined with capsule flat end embedding, because the entire orientation range of the microtome can be utilized for final exact positioning of the specimen. A demonstration of both techniques will be given.The advantages of re-embedding are: 1, complete freedom in orientation of the tissue, and 2, multiple segments of the same block can be used for various orientations. Re-embedding involves: 1, removal of a tissue block from the surrounding plastic (Fig. 1), and 2, orientation and embedding of the tissue into wax which has suitable support properties for sectioning.Equipment and materials needed for re-embedding include: dissecting microscope; wax mixture ( carnuba 35%, Tenax 65%); empty gelatine capsules; dental carvers; dissecting needles; #7 Dupont forceps; Pasteur pipettes; specimen holders; razor blades; and gas flame.


1888 ◽  
Vol 25 (635supp) ◽  
pp. 10139-10140
Author(s):  
Chas. M. Lungren
Keyword(s):  

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