[0001] This invention relates to a corrosion reducing structure and a method of protecting
a surface from corrosion. The structure and method are particularly, but not exclusively,
useful for protecting metallic parts of a vacuum pump used for gas discharging from
a semiconductor producing apparatus, especially from a dry etching apparatus.
[0002] Since an intensively corrosive gas is used in some semiconductor producing apparatuses,
it is necessary to use an excellent anticorrosive material for construction of the
portions which are exposed to a corrosive gas including, not limitedly, the inside
of chambers, valves and pipings of such apparatuses, but even vacuum pumps for gas
discharging from the chambers.
[0003] In general, austenite type stainless steels typified by SUS304 are used as the anticorrosive
material of this kind.
[0004] That is, it is common practice to use an austenite type stainless steel for constructing
those areas exposed to a corrosive gas, but a high power aluminium alloy is used for
preparing those parts which rotate at a high speed such as rotating elements of vacuum
pumps since light weight and high strength are required.
[0005] In the case of such aluminium alloys, an oxide film is spontaneously formed on the
surfaces thereof and it functions as a passive state coating so that the surfaces
are endowed with a corrosion resisting property to a certain extent. However, since
the corrosion resisting property of aluminium alloys is considerably inferior to that
of the passive state coating on stainless steels, the oxide films on the surfaces
of aluminium alloy are broken when exposed to a corrosive gas as the exhaust gas to
cause corrosion thereon. Therefore, it is necessary to apply a corrosion preventing
treatment to the surface of aluminium alloys other than the spontaneously formed oxide
film.
[0006] In view of this, surfaces of aluminium alloys have hitherto been subjected to electroless
plating with a Ni-P type alloy or to anodic oxidation treatment (alumite process)
as the anticorrosion treatment.
[0007] The plating treatment with a Ni-P type alloy is carried out by applying the electroless
plating method which is distinctive from the usual electroplating. On the whole surface
of the parts made of an aluminium alloy a Ni-P type alloy such as Ni-P, Ni-W-P or
the like is deposited to form a film of 10 to 25 micrometer thickness by this method.
Also, the anodic oxidation treatment should be accompanied with the so called sealing
treatment for plugging the micropores of oxide film formed by the usual treatment.
[0008] However, in the apparatuses which use a chlorine type gas having intensively corrosive
action such as Cl
2, CCl
4, BCl
3, and the like such as the recently developed reactive ion etching apparatus (RIE)
for aluminium alloys, it is not possible to protect the aluminium alloys with the
traditional coating films formed by the treatment of electroless plating with a Ni-P
type alloy or alumite treatment bringing about a problem of corrosion of the aluminium
alloy. The mechanism of corrosion is as follows.
[0009] Etching of aluminium alloys is practised by ionisation of a chlorine type gas to
form chlorine ions which are crashed against the aluminium film on a silicon substrate.
At this time, the reaction product (AlCl
3) is generated in a large amount as a vapour and the vapour deposits in the course
of discharging on the sites where the temperature is low and the pressure is high,
namely the inner surface of exhaust pump. Such a deposited product (AlCl
3) sublimates at 178°C under 1 atm and at about 40°C under 0.3 Torr.
[0010] Therefore, the deposited product (AlCl
3) of this kind reacts with atmospheric moisture in the event of pump suspension, leaking
or the like to form HCl, namely chlorine ions. Also, chlorine ions may be formed by
the reaction with moisture at the time of periodical maintenance or washing elimination.
[0011] Chlorine ions readily break the passive state films on aluminium alloys and stainless
steels inducing corrosion of pit form (pitting corrosion). Once pitting corrosion
is induced, the sites act as local cells and corrosion advances acceleratively.
[0012] Further, in the apparatuses of such a type, since raw material gases having intensive
corrosiveness such as Cl
2, BCl
3 and the like are partly discharged as they are through the exhaust pump, such gases
are adsorbed by the inner surface of relevant exhaust pump intact and sometimes generate
chlorine ions similarly to the above.
[0013] Through the above procedures a large amount of chlorine ions are generated. Confronting
the existence of such a large amount of chlorine ions, the electroless plating film
of a Ni-P type alloy of 20 micrometer thickness and the alumite processed coating
film having been hitherto applied as an anticorrosion treatment cannot completely
prevent corrosion.
[0014] That is to say, chlorine ions readily intrude through the micropores (pinholes) existing
in the plating films to reach the aluminium substrate where pitting corrosion is induced
and, once pitting corrosion is induced in this manner, the local cell function is
by far amplified standing on the relevance to the Ni alloy existing in the plating
films thereby to intensively advance pitting corrosion so that the corrosion product
forces up the plating films to induce exfoliation of the plating films.
[0015] The electroless plating treatment is preferable as a treatment to form the coating
films for corrosion prevention in respect of the capability of promoting growth of
the film even in the inside of concave areas and holes with a thickness equal to that
on the flat portions. Further, the Ni-P alloy per se is not attacked by chlorine ions.
[0016] However, with the electroless plating treatment, it is not possible for coating films
to completely get rid of pinholes in the coating films and some sites cannot be plated
particularly in the concave areas of machining processed surfaces and electric discharge
machined surfaces or the areas of nonhomogeneous aluminium texture. With respect to
this point, it is postulated that pinholes piercing from the surface of aluminium
to the surface of plating film are sometimes generated in the cases in which the object
of electroless plating is aluminium. It is difficult for the known plating technology
to completely eliminate such piercing pinholes and, when being intact, chlorine ions
reach the aluminium substrate by way of such pinholes starting from the plating surface
thereby to cause unavoidably corrosion of aluminium.
[0017] Prior art can be found in JP7080876 which discloses a mould having a composite film
layer 3, which is produced through the uniformly dispersed eutectoid of finely divided
polytetrafluoroethylene (PTFE) particle in electroless plating plated through ground
layer 2 on the surface 11 of the base of mould base material 1 such as aluminum alloy
or the like. At the formation of the composite film layer 3, the base material 1 is
buffed, cleansed with ethane and degreased and cleaned with weak alkali so as to form
the ground layer 2 for zinc film on the surface 11 of the base. Next, PTFE is dispersed
in electroless nickel plating solution having hypophosphate as reducer. After that,
composite film layer 3 is preferably formed by directly immersing the base material
1, on which the ground layer 2 is formed, in the mixed liquid just mentioned above
at normal temperature for 10-24 hours.
[0018] It is an object of the present invention to provide a corrosion preventing structure
which is suitable for metallic parts composed of an aluminium alloy, iron and the
like.
[0019] According to one aspect of the present invention, there is provided a corrosion reducing
structure applied to a surface to be protected, the structure comprising a first plating
film composed of Ni-P type alloy for application to the surface, characterised in
that a second plating film comprising fine particles in a Ni-P type alloy is provided
on said first plating film.
[0020] According to another aspect of the present invention, there is provided a method
of protecting a surface against corrosion, the method comprising applying a first
plating film composed of Ni-P type alloy to the surface, and characterised by applying
a second plating film comprising fine particles in a Ni-P type alloy over said first
plating film.
[0021] The surface may, for example, be an aluminium alloy or an iron type material.
[0022] In order to attain the above mentioned object, the present invention, in one aspect,
is featured by and has adopted a scheme that a primary plating film comprising a Ni-P
type alloy has been formed on the surfaces of metallic parts and a secondary plating
film of Ni-P type alloy containing dispersed and deposited fine particles has been
formed on the primary plating film.
[0023] Further, a primary plating film comprising a Ni-P type alloy may be formed at least
on the portion of aluminium alloy in the turbomolecular pump used for gas discharging
from a semiconductor producing apparatus and a secondary plating film of a Ni-P type
alloy prepared by dispersing and deposition of fine particles may be formed on this
primary plating film.
[0024] Further, a primary plating film comprising a Ni-P type alloy may be formed on at
least aluminium alloy part of a dry pump used for gas discharging from a semiconductor
producing apparatus and a secondary plating film of a Ni-P type alloy prepared by
dispersing and deposition of fine particles may be formed on this primary plating
film.
[0025] Further, a primary plating film comprising a Ni-P type alloy may be formed at least
on an inner surface of a piping used for gas feeding of a semiconductor producing
apparatus or used for gas discharging from a semiconductor producing apparatus and
a secondary plating film of a Ni-P type alloy prepared by dispersing and deposition
of fine particles may be formed on this primary plating film.
[0026] Further, a primary plating film comprising a Ni-P type alloy may be formed at least
on a moving part of a valve used for gas feeding of a semiconductor producing apparatus
or used for gas discharging from a semiconductor producing apparatus and a secondary
plating film of Ni-P type alloy prepared by dispersing and deposition of fine particles
may be formed on this primary plating film.
[0027] Further, a primary plating film comprising a Ni-P type alloy may be formed at lest
on a moving part and a sliding part in a chamber of a semiconductor producing apparatus
and a secondary plating film of a Ni-P type alloy prepared by dispersing and deposition
of fine particles may be formed on this primary plating film.
[0028] Further, the metallic part may be composed of a material of aluminium alloy type
or of iron type.
[0029] Further, polytetrafluoroethylene may be used as the fine particles.
[0030] Further, the fine particles may be about 1 micrometer or less of the particle diameter.
[0031] Further, the primary and the secondary plating films may be respectively, 8 micrometers
or more of the film thickness.
[0032] Further, the Ni-P type alloy may be compounded with the fine particles in a ratio
of 20 vol% or more by volume ratio or 6 wt% or more by weight ratio.
[0033] The fine particles are of a size such that they fill the holes (micropores) which
are present in the primary plating film.
[0034] In this invention, metallic parts may be firmly protected against intrusion of chlorine
ions to the substrate thereof an occurrence of corrosion in a pit form can be prevented
or reduced. It is thought that such a phenomenon is due to pinholes having an opening
at the surface of the primary plating film being plugged by the fine particles, and
that if the pinholes begin to from during growth of the secondary plating film, the
pinholes are immediately plugged by the fine particles and growth of the pinholes
is disrupted by the fine particles preventing pinholes from straightforwardly piercing
toward the metallic parts.
[0035] For a better understanding of the invention, embodiments will now be described by
way of example, with reference to the accompanying drawings in which:
Fig. 1A and 1B are explanatory diagrams of the corrosion preventing structure according
to this invention;
Fig. 2 is a photograph showing a cross section of a product according to this invention;
Fig. 3 is a photograph showing another cross section of a product according to this
invention;
Fig. 4 is a photograph showing another cross section of a product according to this
invention;
Fig. 5 is a photograph showing a cross section of a prior art product A;
Fig. 6 is a photograph showing another cross section of a prior art product A;
Fig. 7 is a photograph showing a cross section of a prior art product B;
Fig. 8 is a photograph showing another cross section of a prior art product B;
Fig. 9 is a photograph showing a cross section of a comparative sample C;
Fig. 10 is a photograph showing another cross section of a comparative sample C;
Fig. 11 is a photograph showing another cross section of a comparative sample C;
Fig. 12 is a photograph showing a cross section of a comparative sample D;
Fig. 13 is a photograph showing another cross section of a comparative sample D;
Fig. 14 is a photograph showing another cross section of a comparative sample D.
[0036] A detailed description s given below on the corrosion preventing structure according
to this invention referring to Fig. 1 through Fig. 14.
[0037] This corrosion preventing structure has, as shown in Fig. 1, a primary plating film
2 comprising a Ni-P type alloy on the surface of metallic part 1 and is further provided
with a Ni-P/PTFE composite plating film as the secondary plating film 3 on the primary
plating film 2.
[0038] The Ni-P/PTFE composite plating film is formed with not solely a Ni-P alloy but by
dispersing and deposition of polytetrafluoroethylene in the form of fine particles
(hereinafter termed as "PTFE fine particles") in this Ni-P type alloy.
[0039] Such stratified two layers of plating films 2, 3 can be formed through the following
procedures.
(1) The first stage of treatment
[0040] The known treatment of electroless plating with a Ni-P alloy is applied to the surfaces
of metallic parts 1 such as rotary wings, fixed wings and other well known as aluminium
alloy parts of turbomolecular pumps thereby to form the first layer of a Ni-P alloy
(the primary plating film 2).
[0041] That is to say, after applying the prescribed pretreatment to the metallic part 1,
this metallic part 1 is dipped in a plating bath having a specified bath composition
thereby for forming a Ni-P alloy plating film on the surface of metallic part 1.
[0042] The concentration of P in the Ni-P alloy plating film should be about 8 wt% and the
target value of thickness should be at lest 10 micrometer or more. In consideration
of the tolerance and scattering, the film thickness may also be set at 8 micrometers
or more.
[0043] The tendency of the above mentioned pinhole plugging becomes more prominent as the
thickness of deposited Ni-P alloy plating film is increased. That is, the number of
pinholes having the opening at the plated surface is decreased by forming a thick
plating film and the amount of chlorine ions intruded from the surface of plating
to the substrate is reduced to allow improvement of the character of corrosion resistance.
Accordingly, by taking also economy into consideration, it is preferable to provide
the Ni-P alloy plating film formed as the primary plating film 2 with a thickness
of about 20 micrometers.
(2) The second stage of treatment
[0044] After formation of the first layer (the primary plating film 2) in the above manner,
the Ni-P/PTFE composite plating film is further formed as the second layer (the secondary
plating film 3) on this first layer.
[0045] The Ni-P/PTFE composite plating film should have 10 micrometers of thickness as the
target value. The film thickness may also be 8 micrometers or more similarly in this
case from the same consideration of the tolerance and scattering as above.
[0046] The Ni-P/PTFE composite plating film is formed by using a bath prepared by mixing
fine powder of PTFE having about 1 micrometer or less of the particle diameter and
a surface active agent in a bath almost the same as that for Ni-P alloy plating treatment
and by depositing the plating from the bath in a state of being vigorously stirred.
That is, the PTFE fine particles are simultaneously dispersed and deposited in the
Ni-P alloy plating film.
[0047] The formulation should be adjusted to regulate the PTFE content in the Ni-P alloy
plating film to the level of 20 vol% or above but 40 vol% or lower by volume ratio
or 6 wt% or above but 12 wt% or lower by weight ratio.
[0048] That is to say, the corrosion preventing structure of this example is constructed
by forming the primary plating film 2 comprising a Ni-P type alloy on the metallic
part 1 and further forming thereon the secondary plating film 3 prepared by dispersing
and deposition of PTFE fine particles 4 in the Ni-P type alloy. By this structure,
as considered from the viewpoints of following (I) and (II), the structure of metallic
part can be securely protected from intrusion and reaching of chlorine ions, and pitting
corrosion is not brought about proving that it is a favourable corrosion preventing
structure for metallic parts.
(I) As shown in Figure 1A, even if pinholes H having an opening at the surface of
primary plating film 2 exist at the beginning of formation of the secondary plating
film, it is conjectured that such pinholes H are plugged by the PTFE fine particles
and intrusion of chlorine ions into such pinholes H is prevented. Also, growing up
of pinholes ceases at this point by being plugged in this manner. That is, the fine
particles of PTFE 4 impede growth of the pinholes H and prevent pinholes from piercing
through the primary plating film 2 to the base material.
(II) As shown in Figure 1B, even if appearance of pinholes begins during growth of
the secondary plating film 3, such pinholes are immediately plugged by the PTFE fine
particles and growth of the pinholes is disrupted by the PTFE fine particles so that
pinholes which pierce through the base material do not appear and consequently the
intruding sites of chlorine ions scatter over a broad range and localised intensive
pitting corrosion only occurs with difficulty.
[0049] In this corrosion preventing structure, the surface of secondary plating film 3 is
covered by PTFE of the amount of 20 to 40 vol% by volume ratio after the growth thereof.
Accordingly, the surface of secondary plating film exhibits good water repellency
so that substances such as AlCl
3, Cl gases, chlorine ions and the like come to be adsorbed by the surface of secondary
plating film 3 only with difficulty and reaching and intrusion of chlorine ions to
the substrate of metallic part can be prevented also in this respect.
[0050] The effect of preventing intrusion of chlorine ions mentioned above cannot be sufficiently
exhibited if the content of PTFE in the secondary plating film 3 is low. For instance,
the protection against intrusion of chlorine ions is lowered in the event of the PTFE
content of about 5 to 15 vol% by volume ratio (1.5 to 5 wt% by weight ratio), though
protection against intrusion of chlorine ions does not become inefficacious. Accordingly,
the PTFE content is required to be 20 vol% or more but 40 vol% or less by volume ratio,
or 6 wt% or more but 12 wt% or less by weight ratio as mentioned above.
[0051] The above function and effect have been confirmed by an experiment. An explanation
will now be given of this experiment.
[0052] In this experiment, rotary wings (No. 2000 type high power aluminium alloy) of a
turbomolecular pump were used as the metallic part 1 and they were subjected to any
of the treatments (i) to (v) mentioned below for preparing a product according to
the present invention, prior art products A, B and comparative samples C, D. These
test samples are laid in a desiccator the bottom cavity of which was charged with
hydrochloric acid diluted with water. In this manner, the above test samples were
exposed to vapour of hydrochloric acid. The concentration of hydrochloric acid in
this case was at lowest 18 ppm and the time for exposure was 148 hours.
[0053] Samples were produced as follows:
(i) electroless plating wtih a Ni-P alloy (thickness 10 micrometers), then electroless
plating treatment with a Ni-P/PTFE (thickness 10 micrometers, PTFE content 10 wt%):
the product according to the present invention.
(ii) electroless plating treatment with a Ni-P alloy: prior art product A
(iii) alumite processing (thickness 8 micrometers): prior art product B.
(iv) electroless plating treatment with a Ni-P alloy (thickness 50 micrometers): comparative
sample C.
(v) electroless plating with a Ni-P alloy (thickness 10 micrometers), then electroless
plating treatment with a Ni-P/PTFE (thickness 10 micrometers, PTFE content 5 wt%):
comparative sample D.
[0054] A portion of each test sample, specifically the tip of rotary wing, was cut after
the experiment and the cross section was observed and photographed. In the case of
the product according to the present invention, Figure 2 to Figure 4 respectively
show that intrusion of chlorine ions has been completely prevented and no pitting
corrosion has been brought about.
[0055] In contrast, intensive pitting corrosion is observed in whole surfaces of prior art
product A shown in Figure 5 and Figure 6 as well as of the prior art product B shown
in Figure 7 and Figure 8.
[0056] As seen in Figure 9 to Figure 11, in the case of Ni-P alloy plating in which the
film thickness is 50 micrometer but not 20 micrometer like the case of comparative
sample C, the number of pitting corrosion slightly decreases owing to plugging of
the pinholes but pitting corrosion invariably occurs even in this case and complete
prevention of pitting corrosion is impossible. further, even in the case where 2-layer
plating is applied, intrusion of chlorine ions cannot be prevented as shown in Figure
12 to Figure 14 in the event of little amount of PTFE like in the case of comparative
sample D to allow occurrence of pitting corrosion.
[0057] That is, intrusion of chlorine ions cannot be prevented and occurrence of pitting
corrosion remains unavoidable only by increasing the thickness of Ni-P alloy plating
film from 20 micrometers to 50 micrometers or only by stratifying the Ni-P alloy plating
film in two layers without compounding PTFE.
[0058] Also, it can be conjectured that even if a Ni-P/PTFE plating (PTFE content 10 wt%)
is applied, use thereof as a sole layer is ineffective to avoid occurrence of pitting
corrosion.
[0059] The corrosion preventing structure of this invention is favourable as a measure for
corrosion prevention of aluminium alloys by may further be applied to, for example,
a corrosion preventing structure of metallic parts constituted with an iron type material.
[0060] The corrosion preventing structure of this example can be applied to, for example,
the following metallic parts. As a matter of course, it can be applied to other metallic
parts.
(a) aluminium alloy parts of a turbomolecular pump useful for gas discharging from
semiconductor producing apparatuses;
(b) aluminium alloy parts, or aluminium alloy parts with parts of another metallic
material of dry pumps used for gas discharging from similar apparatuses;
(c) inner surface, or both inner and other surfaces, of pipings used for gas feeding
of similar apparatuses or for gas discharging from similar apparatuses;
(d) movable parts, at least, of valves for gas discharging from similar apparatuses;
(e) movable parts and sliding parts, at least, in the chamber of similar apparatuses.
[0061] Although PTFE is used as the fine particles in this Example, there is no need of
restriction thereto and any of fine particles can be applied as a replacement of PTFE
provided that it can exhibit functions and effects similar to those of PTFE, that
is, plugging of pinholes, inhibitio of growth thereof and the like. As the fine particles
which exhibit performance and effect equivalent to those of PTFE, fluorinated graphite,
ceramics and the like may be referred to, for examples.
[0062] The corrosion preventing structure is set up by forming a primary plating film composed
of a Ni-P type alloy on the surface of metallic parts and further forming a secondary
plating film prepared by dispersing and deposition of fine particles in a Ni-P type
alloy thereon. Therefore, from the viewpoints of under mentioned (A) and (B), it is
possible securely to prevent intrusion and reaching of chlorine ions to the substrate
of metallic parts so that pitting corrosion never occurs proving that is a favourable
corrosion preventing structure for metallic parts which will extend the life of metallic
parts.
(A) It is postulated that, even if the primary plating film includes pinholes having
the opening at the surface thereof at beginning of formation of the secondary plating
film, such pinholes are plugged by the fine particles and intrusion of chlorine ions
in the pinholes is prevented. Further, growth of the pinhole terminates by being plugged.
That is, the fine particles inhibit growth of pinholes and pinholes piercing straightforwardly
to the base material (metallic parts) disappear.
(B) Even if formation of pinholes begins in the course of growing up of the secondary
plating film, such pinholes are immediately plugged by the fine particles and growth
of pinholes is disrupted so that pinholes straightforwardly piercing toward the base
material (metallic parts) disappear consequently to scatter the intruding sites of
chlorine ions over a broad range and localised intensive pitting corrosion becomes
to be only difficulty brought about.
1. A corrosion reducing structure applied to a surface (1) to be protected, the structure
comprising a first plating film (2) composed of Ni-P type alloy for application to
the surface (1), characterised in that a second plating film (3) comprising fine particles in a Ni-P type alloy is provided
on said first plating film (2).
2. A method of protecting a surface (1) against corrosion, the method comprising applying
a first plating film (2) composed of Ni-P type alloy to the surface (1), and characterised by applying a second plating film (3) comprising fine particles in a Ni-P type alloy
over said first plating film (2).
3. Use of a composition of fine-particles in a Ni-P type alloy for improving the corrosion
resistance of a Ni-P type alloy coating.
4. The structure, method or use as claimed in claims 1, 2 or 3, wherein the fine particles
are of polytetrafluoroethylene (PTFE).
5. The structure, method or use as claimed in claims 1, 2, 3 or 4, wherein the particle
diameter of the fine particles is substantially 1 micrometer or less.
6. The structure or method as claimed in claim 1 or 2, wherein the first and second films
have, respectively, a thickness of substantially 8 micrometers or more, or the use
as claimed in claim 3, wherein the Ni-P type alloy coating and the composition of
fine particles in Ni-P alloy, respectively, have a thickness of substantially 8 micrometers
or more.
7. The structure, method or use as claimed in any preceding claim, wherein the content
of the fine particles in the Ni-P type alloy is 20% or more by volume ratio or 6%
or more by weight ratio.
8. The structure, method or use as claimed in claim 7, wherein the content of the fine
particles in the Ni-P type alloy is 40% or less by volume or 12% or less by weight
ratio.
9. The structure, method or use as claimed in claim 1, 2, 3 or claims 5 to 8, wherein
the fine particles are of fluorinated graphite or ceramics.
10. Use of a structure as claimed in claim 1 for reducing corrosion of:
an aluminium alloy part of a turbomolecular pump used for gas discharging from a semiconductor
producing apparatus;
an aluminium alloy part of a dry pump used for gas discharging from a semiconductor
producing apparatus;
an inner surface of a pipe used for gas feeding of a semiconductor producing apparatus;
a movable part of a valve used for gas feeding of a semiconductor producing apparatus
or used for gas discharging from a semiconductor producing apparatus; and/or
a movable part and a sliding part in a chamber of a semiconductor producing apparatus.
1. Korrosionsvermindernde Struktur, aufgebracht auf eine Oberfläche (1), die geschützt
werden soll, wobei die Struktur einen ersten Beschichtungsfilm (2) aus einer Ni-P-Typ-Legierung
zum Aufbringen an die Oberfläche (1) umfasst, dadurch gekennzeichnet, dass ein zweiter Beschichtungsfilm (3), umfassend feine Teilchen in einer Ni-P-Typ-Legierung,
auf dem ersten Beschichtungsfilm (2) bereitgestellt ist.
2. Verfahren zum Schutz einer Oberfläche (1) gegen Korrosion, wobei das Verfahren das
Aufbringen eines ersten Beschichtungsfilms (2) aus einer Ni-P-Typ-Legierung auf die
Oberfläche (1) umfasst, und dadurch gekennzeichnet ist, dass ein zweiter Beschichtungsfilm (3), der feine Teilchen in einer Ni-P-Typ-Legierung
umfasst, über den ersten Beschichtungsfilm (2) aufgebracht wird.
3. Verwendung einer Zusammensetzung feiner Teilchen in einer Ni-P-Typ-Legierung zur Verbesserung
der Korrosionsbeständigkeit einer Ni-P-Typ-Legierungs-Beschichtung.
4. Struktur, Verfahren oder Verwendung nach den Ansprüchen 1, 2 oder 3, worin die feinen
Teilchen aus Polytetrafluorethylen (PTFE) bestehen.
5. Struktur, Verfahren oder Verwendung nach den Ansprüchen 1, 2, 3 oder 4, worin der
Teilchendurchmesser der feinen Teilchen im Wesentlichen 1 Mikrometer oder weniger
beträgt.
6. Struktur oder Verfahren nach den Ansprüchen 1 oder 2, worin der erste bzw. der zweite
Film eine Dicke von im Wesentlichen 8 Mikrometer oder mehr hat, oder Verwendung nach
Anspruch 3, worin die Ni-P-Typ-Legierungs-Beschichtung bzw. die Zusammensetzung feiner
Teilchen in der Ni-P-Legierung eine Dicke von im Wesentlichen 8 Mikrometer oder mehr
hat.
7. Struktur, Verfahren oder Verwendung nach einem der vorhergehenden Ansprüche, worin
der Gehalt der feinen Teilchen in der Ni-P-Typ-Legierung 20 % oder mehr in Volumenprozent
oder 6 % oder mehr in Gewichtsprozent ist.
8. Struktur, Verfahren oder Verwendung nach Anspruch 7, worin der Gehalt der feinen Teilchen
in der Ni-P-Typ-Legierung 40 % oder weniger in Volumenprozent, oder 12 % oder weniger
in Gewichtsprozent ist.
9. Struktur, Verfahren oder Verwendung nach den Ansprüchen 1, 2, 3 oder 5 bis 8, worin
die feinen Teilchen aus fluoriertem Graphit oder Keramiken bestehen.
10. Verwendung einer Struktur nach Anspruch 1 zur Korrosionsverminderung bei:
einem Aluminiumlegierungs-Teil einer Turbomolekularpumpe, verwendet zum Gasauslass
aus einer Halbleiter-Herstellungsvorrichtung;
einem Aluminiumlegierungs-Teil einer Trockenpumpe, verwendet zum Gasauslass aus einer
Halbleiter-Herstellungsvorrichtung;
einer Innenoberfläche eines Rohrs, das zur Gaszufuhr einer Halbleiter-Herstellungsvorrichtung
verwendet wird;
einem beweglichen Teil eines Ventils, das zur Gaszufuhr einer Halbleiter-Herstellungsvorrichtung
verwendet wird, oder das zum Gasauslass aus einer Halbleiter-Herstellungsvorrichtung
verwendet wird; und/oder
einem beweglichen Teil und einem Schiebeteil in einer Kammer einer Halbleiter-Herstellungsvorrichtung.
1. Structure réduisant la corrosion appliquée à une surface (1) devant être protégée,
la structure comprenant un premier film de placage (2) composé d'alliage de type Ni-P
pour application à la surface (1), caractérisée en ce qu'un deuxième film de placage (3) comprenant de fines particules dans un alliage de
type Ni-P est disposé sur ledit premier film de placage (2).
2. Procédé de protection d'une surface (1) contre la corrosion, le procédé comprenant
l'application d'un premier film de placage (2) composé d'alliage de type Ni-P à la
surface (1), et caractérisé par l'application d'un deuxième film de placage (3) comprenant de fines particules en
un alliage de type Ni-P sur ledit premier film de placage (2).
3. Utilisation d'une composition de fines particules en un alliage de type Ni-P pour
améliorer la résistance à la corrosion d'un revêtement en alliage de type Ni-P.
4. Structure, procédé ou utilisation selon la revendication 1, 2 ou 3, dans lequel les
fines particules sont en polytétrafluoroéthylène (PTFE).
5. Structure, procédé ou utilisation selon la revendication 1, 2, 3 ou 4, dans lequel
le diamètre des fines particules est sensiblement de 1 micromètre ou moins.
6. Structure ou procédé selon la revendication 1 ou 2, dans lequel les premier et deuxième
films ont respectivement une épaisseur de sensiblement 8 micromètres ou plus, ou utilisation
selon la revendication 3, dans laquelle le revêtement en alliage de type Ni-P et la
composition de fines particules dans l'alliage de Ni-P, respectivement, ont une épaisseur
de sensiblement 8 micromètres ou plus.
7. Structure, procédé ou utilisation selon l'une quelconque des revendications précédentes,
dans lequel la teneur en les fines particules dans l'alliage de type Ni-P est de 20
% ou plus en proportion volumique ou de 6 % ou plus en proportion pondérale.
8. Structure, procédé ou utilisation selon la revendication 7, dans lequel la teneur
en les fines particules dans l'alliage de type Ni-P est de 40 % ou moins en volume
ou de 12 % ou moins en proportion pondérale.
9. Structure, procédé ou utilisation selon la revendication 1, 2, 3 ou l'une des revendications
5 à 8, dans lequel les fines particules sont en céramique ou en graphite fluoré.
10. Utilisation d'une structure selon la revendication 1 pour réduire la corrosion de
:
une pièce en alliage d'aluminium d'une pompe turbomoléculaire utilisée pour décharger
un gaz depuis un dispositif produisant des semi-conducteurs ;
une pièce en alliage d'aluminium d'une pompe à sec utilisée pour décharger un gaz
depuis un dispositif produisant des semi-conducteurs ;
une surface interne d'un tuyau utilisé pour l'alimentation en gaz d'un dispositif
produisant des semi-conducteurs ;
une pièce mobile d'une valve utilisée pour l'alimentation en gaz d'un dispositif produisant
des semi-conducteurs ou utilisée pour décharger un gaz depuis un dispositif produisant
des semi-conducteurs ; et/ou
une pièce mobile et une pièce coulissante dans une chambre d'un dispositif produisant
des semi-conducteurs.