[0001] The invention relates to a shell or tubular object, especially having a complicated
configuration, and a method to manufacture the same.
[0002] The background of the invention is a desire to make it possible to operate internal
combustion engines at a higher working temperature, whereby an increased efficiency
and a more complete combustion can be achieved. Thus, it is a well-known problem to
accomplish temperature and corrosion resistance of the materials, especially in combustion
chambers and exhaust channels, in case the working temperature is to be raised above
what is normal in today's engines.
[0003] In fact, ceramic materials are high-temperature and corrosion resistant, but it is
complicated and expensive to combine ceramics with other, metallic construction materials,
such as iron and nickel alloys. Tensions are caused by different temperature coefficients.
Certain ceramics will also be subjected to phase transformations in temperature intervals
within or very close to the working temperatures in question. Moreover, the subsequent
treatment, e.g. the boring of holes, becomes more difficult, if ceramics are used.
[0004] Furthermore, experiments have been made to coat especially exposed motor parts with
plates or surface layers of some kind of heat and corrosion resistant metal alloy,
e.g. of a FeCrAl-type, which however causes problems in case inside cavities, in particular
of a complicated geometry, are to be coated.
[0005] It has also been suggested to manufacture tubular surface bodies, which have been
thermally sprayed in advance, with a remaining mandrel or core. In using this known
method, however, only very simple, especially cylindrical or conical tube forms can
be used, since it must be possible to take out the mandrel or core after molding.
[0006] Furthermore, the published Swedish Patent Application SE-A-8300603-1 discloses a
method of manufacturing a machine part, including a heat insulated inlet gas channel,
by thermally spraying a very thin first layer, having a thickness of 0.1-0.2 mm, of
a soft metal material, such as zinc, tin, lead, copper or aluminium, onto a sand core.
A second layer, having a thickness of 0.5-2.5 mm, of a metal material, such as carbon
steel, is thermally sprayed onto the first layer, and thereafter a third layer, serving
as a heat barrier and consisting of a ceramic material is applied, e.g. by thermal
spraying. Then, the sand core with the three layers applied thereon is placed in a
mold for molding the machine part in a conventional manner. Upon molding, the sand
core is removed, so that the three layers form an internal surface of a channel in
the machine part.
[0007] However, in this known method, there might be a risk of cracking when thermally spraying
the various layers having different expansion characteristics. Furthermore, the innermost
layer, forming the internal surface layer of the machine part, is not corrosion resistant
and is not suitable e.g. for exhaust channels. Also, the melting point of the soft
metal material is far too low to permit the use in an exhaust channel of a combustion
engine. Thus, a typical temperature of the exhaust gases is about 850°C, whereas the
melting point of Zn is about 420°C.
[0008] The object of the invention is to eliminate the disadvantages and restrictions of
the known methods and to enable a simple manufacture of shell or tubular objects,
even with a complicated geometry, by thermal spraying of a heat and corrosion resistant
metal alloy so as to form a relatively thick, first surface layer and a second layer
serving as a heat barrier, without any risk of cracking during the spraying process.
A further object is to enable the molding of such an object into a molded body having
one or several channels or cavities constituted by the molded shell or tubular object
according to the invention.
[0009] The main object is achieved in that the first layer consists of a high temperature
and corrosion resistant alloy with a thickness of 0.5-1.5 mm and in that the second
layer likewise consists of a high temperature and corrosion resistant metal alloy,
which contains more oxides and/or pores than the first layer and thereby serves as
a heat barrier, the second layer being sprayed onto the first layer upon removal of
the core body, whereby cracking is avoided.
[0010] Other suitable features are stated in the appended claims 2 - 9.
[0011] Thus, when manufacturing such an object it is essential that the core body, onto
which a first layer is sprayed, will be removed before additional material is applied
by spraying. It is particularly suitable to make the core body of molding sand which
can loose its form stability and be discharged from the tube or shell, e.g. upon heating.
Without risk of cracking due to tensions, which would unavoidably arise if the core
body were to remain, continuous spraying may thereafter be effected up to a desired
thickness.
[0012] The thermal spraying of the second layer should be controlled in such a way that
the second layer contains more oxides and/or pores than the first layer, whereby the
desired qualities, especially a lower thermal conductivity, are obtained in the second
layer. Naturally, it is also possible to apply a third layer, either between the two
other layers or as a separate layer sprayed onto the second layer. Preferably, such
a relatively thin third layer may e.g. be used as a diffusion barrier for carbon or
nickel. Also, it can be used to increase the mechanical qualities at higher temperatures.
[0013] The invention will be explained further below with reference to the appended drawings
illustrating an embodiment.
[0014]
Fig. 1 shows schematically a sand core;
Fig. 2 shows said sand core with a first layer sprayed thereupon;
Fig. 3 shows the dessired tubular object after removing the sand core and spraying
a relatively thick second layer onto the first layer.
[0015] Thus, in a way known per se, a core body 1 is made of molding sand and a phenol resin
as a binding agent. As shown in Fig. 1, the core body 1 has an external configuration
corresponding to the desired internal configuration of the tubular object and, in
addition thereto, holding portions la, 1b at each end for holding the core body. In
the embodiment, the desired object comprises an exhaust channel in a cylinder head
of a combustion engine.
[0016] In accordance with Fig. 2, a relatively thin and essentially pore-free layer 2 of
a metal alloy containing about 5% Al, 22X Cr and the rest mainly Fe (the contents
are by weight) is sprayed onto the core body 1. Porosity, if any, must consist of
closed pores. When the layer thickness is at least 0,5 mm, preferably about 1 mm,
the spraying operation is interrupted, whereupon the sand core 1 is removed in that
the sand core and the layer sprayed thereon is heated in a furnace at about 600°C
for 2-3 hours, and thereafter the sand is discharged from the tubular metal alloy
layer 2.
[0017] Thereafter, a second layer 3 is sprayed onto the first, self-supporting layer 2.
In absence of a core body, the first layer is permitted to expand and shrink freely
due to variations of temperature, without any risk of tensions and accompanying cracking.
The thickness of the second layer may be at least 1 mm. The spraying process can be
performed without interruption for cooling.
[0018] Different methods of spraying are possible. Preferably, the first, relatively thin
layer 2 is sprayed by means of a wire-fed flame sprayer so as to form a dense layer.
In case a surface layer of great purity is desired (small quantities of oxides and
pores), the layer may be applied by plasma spraying. The second layer 3 may preferably
be applied by means of a powder-fed flame sprayer in order to obtain a suitable quantity
of pores and oxides. In this case, a quantity of 5-25Z, preferably about 15X, pores
and oxides is desired.
[0019] However, the second layer 3 does not have to be of the same material composition
as the first layer 2, but may e.g. consist of another metal alloy of high heat resistance.
[0020] With regard to the heat tensions which may appear in the material, it is certainly
an advantage if the layer consists of the same material and differs only in porosity
and oxide contents. Moreover, a thin third layer may be applied either between or
on top of the two above-mentioned layers. The third layer may i.a. function as an
adhesive layer or diffusion barrier.
[0021] The object and the manufacturing method according to the invention have several advantages.
The geometric shape as well as the materials and the thickness thereof can be chosen
at will. Thus, very thick layers (the second layer 3) may be applied after the removal
of the core body. Moreover, the manufacturing method is relatively quick (metal can
be sprayed onto a red hot substrate) and the handling rather simple. The cassation
is very low because of the eliminated risk of cracking. Even the subsequent operations,
e.g. molding, are facilitated and can therefore be performed with great accuracy.
Moreover, by avoiding ceramic materials, the recircling of scrap is made easier.
i. A shell or tubular object, especially having a complicated configuration, said
object being intended to be incorporated in a machine or the like, particularly in
a combustion engine, and comprising a first, internal, layer (2) of a metal alloy
thermally sprayed onto a core body (1) and a second, thicker layer consisting of a
metal alloy thermally sprayed onto the external surface of said first layer, characterized
in that said first layer (2) consists of a high temperature and corrosion resistant
alloy with a thickness of 0.5 - 1.5 mm and in that said second layer (3) likewise
consists of a high temperature and corrosion resistant metal alloy, which contains
more oxides and/or pores than the first layer (2) and thereby serves as a heat barrier,
said second layer (3) being sprayed onto the first layer (2) upon removal of said
core body (1), whereby cracking is avoided.
2. An object according to claim 1, characterized in that the second layer (3) has
essentially the same material composition as the first layer (2).
3. An object according to claim 1 or 2, characterized in that the porosity of the
first layer (2) consists of closed pores, whereas the porosity and oxide contents
of the second layer (3) exceeds 10%.
4. An object according to anyone of claims 1-3, characterized in that at least the
first layer (2) consists of 1-12X A1, 10-30X Cr, possibly small quantities of one
or several elements in the group Si, Mn, Co, Y, Hf, possibly small quantities of oxides
and nitrides and the rest Fe.
5. An object according to anyone of claims 1-4, characterized in that the thickness
of said second layer (3) is greater than 1 mm, preferably about 2,5 mm.
6. An object according to anyone of the preceding claims, characterized by a third
layer between or on top of the two other layers and substantially thinner than said
other layers.
7. A method to manufacture a shell or tubular object according to anyone of the preceding
claims, said object being manufactured by thermal spraying of a high temperature and
corrosioin resistant metal alloy, characterized in that a first, relatively thin and
essentially porefree layer (2) is formed by thermal spraying onto a core body (11),
the external dimensions of which correspond to the internal dimensions of the finished
object, whereupon the core body (1) is removed and a second, relatively thick layer
(3) is applied by thermal spraying onto the external surface of the first layer (2),
so that the internal surface of said finished object is constituted by the first layer
(2).
8. A method according to claim 7, characterized in that the core body (1) is made
of molding sand.
9. A method according to claim 7 or 8 characterized in that the thermal spraying is
controlled in such a way that said second layer (3) contains more oxides and/or pores
than the first layer (2).