Articles and Publication Machine tools ELECTROSLAG WELDING OF SHIP DESIGNS
ELECTROSLAG WELDING OF SHIP DESIGNS
© Dmitry Ivanovich Korneev,
Doctor Ph. & Sci., Professor, Academician
General Director & Chairman of Academic Council of ISTR UAS
The Winner of Honorable Awards and Scientific Premiums of UAS
Nikolaev, Ukraine
Contact to authors:
fond-nauka@mksat.net
http://www.geocites.com/fond_nauka
Manufacturing of large ship details and units as integral
toilful and complex process. Complexity of ship designs, such as anchors, arms
and rudders obviously causes reception of the certain quantity of defective cast
preparations [1]. To avoid occurrence of spoilage at molding, dismember on some
fineer parts. However, in this case, there is a necessity of the further
connection separately parts in a single whole a product. Prior to the beginning
of 50th years to connection of separate parts were applied very expensive and
toilful connections. Manual multipass welding of parts appeared even less
effective. Despite of simplification of the form of products, expenses for
manufacturing of designs have not decreased. And if it was possible to reduce
ñòàíî÷íûå and metalwork works the volume of welding works immeasurably
grew.
Output from this impasse was creation in the USSR of a way of
electroslag welding (ESW) [2]. This way of connection has opened ample
opportunities for the decision of many problems connected to improvement of
quality of welded designs, decrease of their labour input, reduction of a cycle
of manufacturing.
Way of ESW at once has received application on Taganrog
factory, Barnaul boiler and Is new - Kramatorsk machine-building factories, and
then - at many enterprises of heavy mechanical engineering [3] and shipbuilding.
Use of this progressive method of connection of metals, has allowed to change
manufacture of large ship designs radically. Has disappeared necessity for
creation of unique shops on capacity and units for moulding, êîâêè and
machining of such large details in shipbuilding, as àõòåðøòåâíè,
ôîðøòåâíè, shaft of water-wheels, beds powerful mechanical engineering,
etc.
On Nikolaev the Black Sea ship-building factory, with
assistance of Institute of electric welding by E.O.Patona, electroslag welding
is introduced in 1956. For example, for electroslag welding an external covering
of a board of a vessel on a building berth, at thickness of sheets 14 - 30 mm.,
the device such as Ç-433 or the walking automatic device such as Ç-505, and
further and device A-835 was used. This way had been welded coverings of the
case of tankers, dry-cargo ships, whaling base “Soviet Ukraine” and other
courts.
Choice of an optimum mode of welding
From the point of view of reception of the maximal accuracy
of the sizes of welded products it is the most favourable to deal with high
speeds of welding. In this case, as have shown experiences, angular both forward
moving details and probability of a mistake considerably decreases at
indemnification of these kinds of deformations [4]. The sizes determining
process of welding [5] refer to as elements of a mode. Mode ÝØÑ is set by the
following basic elements:
-
a pressure{voltage} of welding- Uñ;
-
speed of submission of an electrode wire-Vý;
-
speed of welding--------------------------------Vñ;
-
quantity{amount} of electrodes-----------------------n;
-
width of a welding backlash--------------------bç;
-
Width of a plate---------------------------------bn;
-
Width of a mouthpiece-------------------------------bm;
-
depth of a slag bath---------------------hø;
-
diameter of a welding wire-------------dý;
-
Thickness of a plate--------------------------------δï;
-
Thickness of a fusing mouthpiece-----------δì.
Depth of a slag bath and diameter of an electrode or
thickness of a fusing mouthpiece can be neglected, as these sizes do not depend
on other elements of a mode of electroslag welding. Basic elements of ESW are
the voltage of welding, speed of submission of electrodes and quantity of
electrodes. Speed of submission of a welding wire-Vý and thickness
of a fusing mouthpiece - δì define
force of a welding current which together with a voltage of welding defines
capacity of a source of heat. For optimum it is possible to accept such mode of
welding in which all elements are picked up so, that with high quality
achievement of welding quality of welded seams and accuracy of the set sizes of
welded details is provided.
The further increase in speed of welding can result in
occurrence in seams cracks [6]. As have shown the experiences which have been
lead by experts [7], speed of submission depends on many factors, including from
conditions of fastening of details.
We shall take advantage of Table 1. In the table skilled
given influences of speed of submission of a wire and sizes
ïðîòèâîäåéñòâóþùåãî the moment of M on occurrence
cracks are resulted. Welding by a fusing mouthpiece of Steel by 30 thicknesses
of 200 mm. The analysis of the data shows that with reduction of speed of
submission of a wire, a crack in a seam appears that later, than it is less
moment. And it means that with other things being equal, occurrence of cracks
depends and on length of a welded seam as the seam is resistance for the angular
movings, welded parts.
Table ¹1 Skilled given influences of speed of submission of
a wire and sizes of the moment on occurrence cracks
|
¹ |
V(c),
km/h |
V(a),
km/h |
U(c),
In |
d(m),
mm |
M(0),
kg/sm |
Distance of cracks from the beginning of a seam mm |
The note |
|
1. |
0,9 |
198 |
46-47 |
65 |
35 |
190 |
Height |
|
2. |
0,8 |
175 |
46-47 |
65 |
0 |
300 |
sample |
|
3. |
0,7 |
152 |
46-47 |
65 |
120 |
150 |
(length of a seam) |
|
4. |
0,7 |
153 |
46-47 |
65 |
60 |
390 |
made |
|
5. |
0,6 |
132 |
46-47 |
65 |
75 |
780 |
950 mm |
|
6. |
0,55 |
120 |
46-47 |
65 |
125 |
No |
- |
|
7. |
0,5 |
110 |
46-47 |
65 |
125 |
No |
- |
The note: M(0) –
specific moment.
Welding of business products with length of a joint up to 4 meters has shown,
that at this speed of submission of a crack in a seam are not formed (speed of
welding did not exceed 0,5 km/h). Generalizing these skilled data, for
precomputations of metal by thickness 150 - 500 mm a fusing mouthpiece, are
possible to recommend critical speed of submission within the limits of 120 -
140 km/h.
The size of deformations depends, with other things being equal, not only on
force of a current, but also from speed of welding. At electroslag welding these
sizes are connected by the following dependence:
Vc = ,
(1)
Where: Fí - the area of a welding backlash, sm2;
Fì - the area of a fusing mouthpiece, sm2;
Fý - total section electrode ïðîâîëîê, sm2.
For a wire in diameter of 3,0 mm it is equal 0,071 n. The quantity of
electrodes n gets out of the following parity{ratio} and is approximated
to an integer:
,
(2)
Where: In - thickness of metal, mm. For definition of capacity of a
source of heat we can to take advantage to the formula found by practical
consideration:
I = (0,022 Vý + 90) n + 1,2 (Vñ
+0,48 Vn) δï
bn, (3)
Where Vn - speed of submission of a plate. Under the formula (3) it is
possible to define force of a current for welding by a wire, a fusing mouthpiece
and a plate. In particular, for a fusing mouthpiece (Vn = 0),
the formula gets the following kind:
I = (0,022 Vý + 90) n + 1,2
Vc δm bm. (4)
At definition of force of a current for the wire variant, the second composed
addresses in zero, and for welding by a lamellar electrode - the first composed.
Capacity of a source of heat of a slag bath, gets out proportionally to
thickness of welded edges and speed of welding:
W = W0 Vc,
Where W0-the specific capacity of welding equal of 0,0575 kw ·
÷/sm2 (specific thermal energy qo = 50,0 kcal / sm2).
Capacity of a source of heat and determine basically a temperature field of a
product. Knowing a temperature field and the sizes of details, it is possible to
define in the settlement way deformations of welded parts.
Assembly of ship designs and reception of the exact sizes
Deviations of the sizes of a product from set will consist of the errors
admitted at assembly and errors at welding. If errors from welding not always
manage to be removed, errors of assembly should be shown up to a minimum [5].
First of all, it concerns a choice of base of gauging of deformations, i.e.
distance between two points located on a lateral surface of welded details on
both sides from a joint. Experiences have shown [8], which the size
deformation’s depends on distance between points from base of gauging.
Therefore, at the indication of size of movings of welded details it is
necessary to specify also and size of base of gauging. Further we shall consider,
that if at the indication of size of moving the base is not underlined, the
given moving has been received on the basis of 300 mm. Errors at assembly arise
more often not at installation of a detail on support which arrangement defines
size set of moment, and at creation of disorder of details. That is, at
formation a backlash with the set corner, for indemnification of turn of details
at welding [6].
For formation of a required assembly backlash [5], details usually move apart
on size bç.í (with parallel edges of a welded joint), and
then make disorder of details on a corner
γ that at the top of a joint the
backlash made size bç.â. However turn of details
(as a rule, welded details have the various sizes and weight) changes position
of edges in the bottom of a joint, i.e. size bç.í.. It
demands corrective action that complicates assembly. At limited preparatory time
under production conditions, even with application of special welding stands,
such system of assembly usually gives an error or demands excessive unproductive
expenses of time for corrective action. That assembly of details to make more
productive, without damage to accuracy of the received sizes of a welded product,
it is necessary to adhere to the following rules:
1.
At disorder of details with the various geometrical sizes it is
necessary, that edges of a bottom of a joint laid at one height. For an
arrangement of edges at one height the condition should be sustained:
γ 1à1
= γ2
à2; γ
1+ γ2=
γ; γ
1= à2 (à1 + à2);
γ2 =
γ à1
(à1 + à2). (5)
In case of welding a massive detail with a small part (see fig. 2) a support
1 and 2 it is necessary to have below bottom plane of a massive
detail on size: ∆h1 =
γà1 And
∆h2 = γà2
Or is higher (á) started a joint.
2.
At the task of disorder it is necessary to bring in size of an
assembly backlash some indemnification which is taking into account an
arrangement of support (fig. 3). If support are flush with the bottom edges of
welded details or is lower than them at disorder of details of an edge will miss
below, increasing size bç.í.. Vertical ∆h and
horizontal ∆L making movings of a considered point at turn of
details can be found from formulas (for both welded parts):
a1
∆h1 =
cos α1 γ1
cos α1 =
α1
γ1
a2
∆h2= cos α2
γ2
cos α2 =
α2
γ2
a1
∆L= cos α1
γ1
sin α1 =
α1
γ1 tq
a1 ( 6 )
a2
∆L= cos α2
γ2
sin α2=
α2
γ2 tq
a2
For observance of conditions on ∆h1 = ∆h2
corners γ1
and γ2
are
Under the formula (2). Thus, the size of an assembly backlash bç.ô.
In the bottom of a joint makes:
bç.ô. = bç.ô
+ ∆L, (7)
Where ∆L = ∆L + ∆L Values ∆L and
∆L take with marks plus at increase in a backlash, and a minus at
reduction of a backlash.
At formation of an external surface of a seam by copper water-cooled linings
to their fastening usually apply Ã-figurative ñêîáû. These
ñêîáû strongly enough press a lining to edges of a welded product, not
interfering with rapproachement of details at welding. At welding long seams
(two meters and more) when lining ïðèæàòû wedges on all height of a joint
the size of the effort necessary on overcoming of forces of friction between a
lining and a welded surface can reach{achieve} significant size. These efforts,
concerning the beginning of a seam, create ïðîòèâîäåéñòâóþùèé
the moment. Size of this moment which deforms size of expected deformations to
take into account very difficultly.
To avoid influence ïðîòèâîäåéñòâóþùåãî the moment from
friction, wedges it is recommended to hammer in the beginning of welding only in
the bottom of a joint at height of 300-400 mm. Other wedges hammer on a measure
of tea leaves of a welded seam.
At welding it is necessary to create identical conditions of a seam forming
devices. If cooling not identical and óñàäêà welded connection with both
sides of a joint will be different. There, where cooling will be smaller, there
óñàäêà welded connection will be the greater. The difference óñàäêè
can It quite enough that welded parts have turned in a horizontal plane, having
bended the general axis of a product.
The size of a corner of turn in a horizontal plane is usually insignificant
and on the average makes 0,001 - 0,002 radiuses. However at welding such long
details as àõòåðøòåâåíü, turn of welded parts even on such corner,
can cause a significant deviation{rejection} of the ends of a product from the
general{common} axis.
Welding of steel cartridges pipes.
For cartridges from steel thickness 25 - 70 mm, have been adapted the
submitting mechanism of semiautomatic device PS-5 supplied with a special
mouthpiece. A feed was carried out by a direct current. Assembly was made on
technological employees also for fastening forming linings. Welding was carried
out by an electrode wire under flux. In the beginning of process the arch was
raised on a metal shaving. After the beginning swimming trunks of a metal
shaving and excitation of an arch, the flux was fallen asleep.
Assembly backlashes and modes of welding of cartridges are resulted in Table
2 and Table 3. After the radiographic control, over removal of voltage of the
cartridge were exposed to holiday. Metal has structure of cast steel. The zone
structure with a point of a grain 4 - 6. Then there is a structure with a point
of a grain 5 - 6. Hardness on all sites is identical.
Table 2. Assembly backlashes at cartridges
|
¹ |
Length pipes [mm] |
Assembly backlashes [mm] |
|
In the bottom of a pipe
|
At the top of a pipe |
|
1. |
up to 1500 |
18 |
28 |
|
2. |
up to 2500 |
20 |
30 |
|
3. |
up to 4000 |
20 |
32 |
The note. Backlashes can change depending on diameter and
thickness welded product.
Table 3. Modes of cartridges
|
¹ |
Diameter of a wire, [mm] |
V, [m / hour] |
I, And |
U, IN |
Depth of a bath, [mm] |
|
1. |
2,5 |
250 |
380-420 |
38-42 |
40-50 |
|
2. |
2,5 |
306 |
460-500 |
42-44 |
40-50 |
|
3. |
2,5 |
372 |
500-550 |
44-48 |
40-50 |
Welded large courts.
For welding ship-building details by thickness up to 250 mm, device A-372r
with transformer TSHS-600-3 and a wire in diameter d = 3 mm was used. For
welding metal by thickness up to 500 mm the welding automatic device also was
above used.
Now by electroslag welding are made ship øòåâíè for tankers, dry-cargo
courts, the big freezing trawlers and for military shipbuilding. Productivity of
electroslag welding rather high. For example, a product section 400 õ 400 mm
and height 500 mm. It was welded for 50 minutes, and section 450 õ 700 mm. -
for 1, 5 hours. After performance of process all joints should be without fail
subjected to local high-temperature thermal processing (to normalization and
holiday) in electric furnaces.
After high-temperature thermal processing mechanical properties of welded
connection meet the requirements, showed to the basic metal. However the limit
of fluidity is reduced up to 30 kg/mm^2 at welded connection from steel and up
to 25 kg from special steels.
The used adaptations providing qualitative welding represent copper figured
linings cooled by water. Such adaptations allow carrying out welding of products
by thickness up to 1000 mm and are higher. It is necessary to stop on
technological sequence of tea leaves of joints closed contour. These apertures
are muffled by the fuses scalded on a contour that creates additional
concentration of voltage. During distance of external technological inflow with
the help gas are sharp on one of joints close, in the central part of welded
connection, after the common thermal processing øòåâíÿ the crack which has
left on a surface has appeared.
Carried out together with Institute of electric welding researches, have
allowed to develop technology which provides reception of welded connections the
closed high quality contour and without cracks. Before welding of last joint
heating in the electric furnace of an opposite site, up to increase in a
backlash in a joint on 4 - 5 mm (size usual óñàäêè a joint of the given
section) is made. After welding a furnace it was disconnected, and the welded
joint was cooled simultaneously with the heated up site. This technological
reception provided decrease of additional voltage.
Very important at manufacturing, before foundry apertures to execute on small
through apertures. Absence of such apertures on resulted one in its destruction
on a site between welded joints during the common thermal processing in the
furnace. Assembly backlashes and modes of welding are resulted in Table 4 and
Table 5.
Table 4. Assembly backlashes
|
¹ |
Thickness of welded details [mm] |
Length of a seam [mm] |
Assembly backlash [mm] |
|
1. |
100-150 |
300-350 |
22+2 |
|
2. |
200-250 |
400-500 |
25+2 |
|
3. |
300-400 |
500-650 |
30-2 |
|
4. |
300-400 |
700-800 |
30,0 |
|
5. |
350-400 |
800-1000 |
30+2 |
|
6. |
350-400 |
1000-1500 |
32+2 |
|
7. |
400-450 |
1500-2000 |
35+2 |
|
8. |
450-500 |
800-1000 |
32+2 |
The note. Backlashes
can change depending on diameter and thickness of a welded product.
The partition on the greater number of details has allowed lowering spoilage
at casting preparations. Details prepare under welding only on one machine tool,
also "apple" here is pierced. Details have on the ends rectangular
technological inflow in length on 100 mm. replacing introduction plates. From
welded connection near to the technological inflow leaving for working section,
samples for mechanical tests are cut out. From the bottom side
"pocket" becomes isolated a steel rod.
Forged welded rudders.
Before application, rudders were made from preparations. At machining
preparation in a shaving left up to 40 - 50 % of metal. Now technology combined
rudders from steel at which the cast part is cast in the pure size is applied,
and rod is made with the minimal allowances. At connected end faces of a detail
have technological inflow from which samples for mechanical undertake Tests. At
manufacturing áàëëåðîâ in welded variant in a shaving leaves no more
than 10 - 15 % of metal.
Table 5. Modes of electroslag welding
|
¹ |
Thickness of metal [mm] |
U, IN |
I |
N
electrodes |
Speed of fluctuation of electrodes [m/hour] |
Endurance |
|
1. |
100-150 |
45 |
450 |
2 |
39,0 |
3 |
|
2. |
200 |
50 |
450 |
2 |
31,7 |
4 |
|
3. |
220 |
50 |
500 |
2 |
31,7 |
4 |
|
4. |
250 |
50 |
500 |
3 |
31,7 |
4 |
|
5. |
300 |
50 |
500 |
3 |
25,0 |
5 |
|
6. |
350 |
55 |
550 |
3 |
25,0 |
5 |
|
7. |
400 |
55 |
550 |
3 |
25,0 |
6 |
|
8. |
450 |
55 |
650 |
3 |
25,0 |
6 |
|
9. |
500 |
55 |
600 |
3 |
25,0 |
6 |
The note. Depth of the fused bath
within the limits of 50-:-60 mm.
Welded by an electroslag way rudders are rather responsible designs working
in very complex conditions at sign-variable loadings, high and low temperatures.
While in service on courts of the various tonnage and the purpose, floating in
tropical and Arctic conditions, and also in conditions of the Antarctic
breadthes, these products have shown reliability and serviceability.
HIGH-TEMPERATURE THERMAL PROCESSING
After process of electroslag welding all joints, together with
ïðèõâà÷åííûìè to them inflow, are exposed to local thermal
processing (to normalization and holiday) in electric furnaces. Electric
furnaces will consist of two mobile and independent sliding parts. Capacity of
furnaces from 35 up to 70 kw. The temperature necessary for heat treatment (in
position “ on a joint ”) is established by a furnace for four - five
hours. Normalization is carried out at temperature t = 940 … 960Ñ, and
holiday at tî = 640 … 660Ñ [8]. In case of the big dimensions of a design
and impossibility of carrying out of local thermal processing what or a welded
joint - all design is exposed to thermal processing. Local thermal processing is
made in portable furnaces. For registration and automatic control of process of
thermal processing, portable furnaces are equipped with recording devices.
Table ¹6 Backlashes at welding wire an electrode
|
¹ |
Welded section: [thickness õ height]
in mm. |
Backlash after processing an end face
|
Backlash at processing under welding
|
The note |
|
In the bottom of a pocket |
At the top of a pocket |
|
1 |
2 |
3 |
4 |
5 |
6 |
|
1. |
200 õ 400 |
21+1 |
25+1 |
27+1 |
|
|
2. |
300 õ 300 |
22+1 |
27+1 |
30±1 |
|
|
3. |
900 õ 1400 |
22+1 |
28±1 |
32±1 |
|
|
4. |
400 õ 1600 |
21+1 |
28±1 |
33±1 |
|
|
5. |
400 õ 600 |
23+1 |
29±1 |
32±1 |
|
|
6. |
450 õ 700 |
24+1 |
30±1 |
33±1 |
|
|
7. |
500 õ 800 |
24+1 |
31±1 |
34±1 |
|
|
8. |
700 õ 700 |
28+1 |
36±1 |
39±1 |
Welding for 2-pass |
|
9. |
700 õ 700 |
28+1 |
36±1 |
39±1 |
Welding by two devices |
The note: It is supposed the lateral faces lying in one plane, in limits ±
1, 5 mm. On all length.
Mechanical properties should correspond to the norms resulted in tab. ¹ 7.
Table ¹7. Mechanical properties of samples
|
The name of a product
|
Mark of steel
|
G,
kg/mm2
|
δ, %
|
Ψ, %
|
Ak – 400Ñ
kg/sm2
|
|
not less |
|
Baller |
08ÃÄÍÔ + |
30,0 |
20,0 |
40,0 |
3,0 |
|
|
08ÃÄÍÔË |
|
|
|
|
|
Baller |
08ÃÄÍË + |
|
|
|
|
|
|
08ÃÄÍ |
25,0 |
20,0 |
40,0 |
3,0 |
|
Welded design |
08ÃÄÍÔË + |
30,0 |
20,0 |
40,0 |
3,0 |
|
|
08ÃÄÍÔË |
|
|
|
|
|
Welded design |
08ÃÄÍË + |
25,0 |
20,0 |
40,0 |
3,0 |
|
|
08ÃÄÍË |
|
|
|
|
|
Welded design |
25Ë + 25Ë |
24,0 |
19,0 |
30,0 |
Àê+20îÑ 4,0 |
Samples for tests, are cut out from the inflow past thermal processing
together with joints from which they have been cut off. At failure of automatic
control of temperature, it is necessary to make the subsequent tests of
mechanical properties of welded connection. Samples for test are cut out from
the inflow last thermal processing together with joints from which they have
been cut out.
Modes of local thermal processing.
The given modes of local thermal processing of a welded joint
áàëëåðîâ are valid only for a combination of steels; and an arm. Local
thermal processing will consist of normalization and holiday.
-
NORMALIZATION
The temperature of heating of the furnace at normalization of joints
of welded designs is equal 940 - 970Ñ. Time of endurance in the furnace
at temperature 940 - 970Ñ is equal to three - five hours from the
moment of achievement by both thermocouples of the set temperature.
Cooling on air before full dimness at moved apart furnaces. After that
additional cooling by the compressed air is supposed.
-
HOLIDAY
At holiday of a furnace it is heated up to temperature 640 - 670Ñ. Time of
endurance at temperature 640 - 670îÑ usually makes six - seven hours. Cooling
on air furnaces move apart so that the distance of cooled joint was not less
than 1,5 - 2,0 meters. Time of endurance of designs at normalization and holiday
depending on section can be presented in a tabulated kind (Tab. ¹ 8).
The table ¹ 8 Time of endurance at normalization and holiday
|
¹
|
SECTION
in mm
|
Time of endurance(quotation) in (hours) |
|
At normalization |
At holiday |
|
1. |
Equally or more ≥ 400 |
3 |
6 |
|
2. |
▬ ≥
400-500 |
4 |
6 |
|
3. |
▬ more>
500 |
5 |
7 |
Process of thermal processing is fixed in magazine. As a rule, such data as
enter the name: the name and number of the drawing of a design; numbers of
swimming trunks of the welded preparations. Numbers of joints and the set modes
of heat treatment. Date and time of carrying out of heat treatment, actual modes
of processing with fixing through everyone 10 - 15 minutes, or according to
technological process.
At all obvious advantages of electroslag welding, this way of connection of
metals has also essential lack. This obligatory application of high-temperature
thermal processing. Despite of high efficiency, from the point of view of the
decision of practical problems connected with improvement of structure and
mechanical properties of metal of a seam zones, high-temperature heat treatment
has a lot of essential lacks [7]. To them concern: high cost of heating
furnaces, significant lengthening of a cycle of manufacturing of a welded
design, danger of gross infringement of geometry of a processable product, etc.
Therefore interest to this problem, and also to a problem of creation of such
advanced technology which will allow simplifying is clear or even completely to
exclude all operations connected with high-temperature thermal processing.
REFERENCES
1. Feygin O.O. Action
of high-energy electroimpulses on metal melts // Sciteclibrary
(2003). - http://www.sciteclibrary.ru/eng/catalog/pages/5294.html
2. Korneev D.I., Feygin O.O. Paradoxical physics of super-power impulsing
discharges // Ibid.
- http://www.sciteclibrary.ru/eng/catalog/pages/5347.html
3. Korneev D.I., Feygin O.O.
Phenomenological thermodynamics of super-energy electroimpulses in metal melt //
Ibid. -
http: //
www.sciteclibrary.ru/eng/catalog/pages/5422.html
4. Korneev
D.I., Feygin O.O. Thermodynamics of fluid metals at ultrahigs energies of
electrocurrent action // Ibid. - http:
// www.sciteclibrary.ru/eng/catalog/pages/5454.html
5. Petrenko S.S., Feygin O.O.
Nonequilibrium crystallization of metal melts // Ibid. -
http: //
www.sciteclibrary.ru/eng/catalog/pages/5687.html
6. Korneev D.I., Feygin O.O. Quasicrystallization of metals at ultrahigh
energy of action // Ibid. -
http: //
www.sciteclibrary.ru/eng/catalog/pages/6078.html
7. Korneev D.I., Feygin
O.O. Electrophysical methods of control by
the crystallization of welded metal // Ibid. - http:
// www.sciteclibrary.ru/eng/catalog/pages/6302.html
8. Korneev D.I., Feygin O.O. Theoretical
explorations of processes high-energy electrophysical treatments of metal’s
melts // Ibid. -
http://www.sciteclibrary.ru/eng/catalog/pages/6436.html
9. Korneev D.I., Feygin O.O. Mechanisms of the operation of electroimpulses
channels in the metal's melts // Ibid.
- http: // www.sciteclibrary.ru/eng/catalog/pages/6586.html
10. Korneev D.I., Feygin O.O. Superhigh - energy electroimpulses in the
metal's melt // Ibid.
-
http://www.sciteclibrary.ru/eng/catalog/pages/6649.html
11. Petrenko S.S., Feygin O.O. Macro - nonequilibrium model of the
quasicyclic solidification of metal – alloys // Ibid. -
http://www.sciteclibrary.ru/eng/catalog/pages/6651.html
12. Korneev D.I., Feygin O.O. Superenergy
electropulsing treatment of weld joints // Ibid. -
http://www.sciteclibrary.ru/eng/catalog/pages/6669.html
Publishing date: July 7, 2004
Source: SciTecLibrary.ru
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