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Publication numberUS20010041230 A1
Publication typeApplication
Application numberUS 09/543,477
Publication dateNov 15, 2001
Filing dateApr 6, 2000
Priority dateJan 25, 1996
Also published asUS6306225
Publication number09543477, 543477, US 2001/0041230 A1, US 2001/041230 A1, US 20010041230 A1, US 20010041230A1, US 2001041230 A1, US 2001041230A1, US-A1-20010041230, US-A1-2001041230, US2001/0041230A1, US2001/041230A1, US20010041230 A1, US20010041230A1, US2001041230 A1, US2001041230A1
InventorsHans-Jorg Hunger, Gunter Lobig, Gerhard Trute
Original AssigneeHans-Jorg Hunger, Gunter Lobig, Gerhard Trute
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Borating wing boron halide
US 20010041230 A1
Abstract
A process is provided for producing wear-resistant boride layers on metal material surfaces. The process is characterized in that a boron halide selected from the group comprising boron trifluoride, boron tribromide, boron triiodide and their mixtures is mixed with hydrogen and optionally argon and/or nitrogen, in order to produce a reaction gas containing between 0.1 and 30 vol % boron halide. The resultant mixture is activated by a plasma discharge whereby boron is transferred from the plasma to the metal surface.
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Claims(6)
What is claimed is:
1. A process for producing wear-resistant boride layers on metallic material surfaces, which comprises mixing at least one boron halide selected from the group consisting of boron trifluoride, boron tribromide and boron triiodide as boron source with hydrogen and possibly argon and/or nitrogen to generate a reaction gas containing from 1 to 35% by volume of boron halide and activating the resulting mixture by means of a plasma discharge so as to enable boron to be transferred from the plasma to the metal surface.
2. The process as claimed in
claim 1
, wherein the boron source used is boron trifluoride.
3. The process as claimed in
claim 1
or
2
, wherein the reaction gas contains 20-90% by volume of H2.
4. The process as claimed in one or more of
claims 1
to
3
, wherein the reaction gas is fed into the treatment space in an amount of from 0.5 to 2 l per minute.
5. The process as claimed in one or more of
claims 1
to
4
carried out at temperatures of from 400° C. to 1200° C.
6. The process as claimed in one or more of
claims 1
to
5
, wherein the treatment time is from 30 to 240 minutes.
Description

[0001] The invention relates to a process for producing wear-resistant boride layers on metallic material surfaces.

[0002] Wear-resistant boride layers are usually produced in practice using solid boriding agents, for example in the form of powders, pastes or granules.

[0003] A disadvantage of these processes is that they are labor-intensive in terms of packing, unpacking and cleaning the parts. Cleaning is carried out using a combination of washing and brushing or abrasive-blasting. Since the powders, pastes and granules can be used only once, problems also arise in disposing of the spent boriding agents.

[0004] In addition, the use of liquid boriding agents, for example in the form of salt melts, is also known. However, all these processes have not been able to become established owing to the problems generally associated with salt baths, viz. those relating to safety of handling, cleaning of the parts after treatment and disposal of the baths or their waste products.

[0005] In the past, there have been various attempts at boriding using gaseous boriding agents (CVD processes). When using organic boron compounds (trimethylboron, trialkylborons), carburization occured predominantly instead of boriding; when diborane is used, safety problems occur because of the extreme toxicity and the risk of explosion.

[0006] The use of boron trichloride as boron donor medium has not been able to become established because of process-inherent problems in layer formation. The cause of these problems is the hydrogen chloride formation which always occurs in boriding using BCl3/H2 mixtures.

[0007] In the boriding of ferrous materials using boron trichloride, the following fundamental reactions occur:

2BCl3+3H2+2Fe→2FeB+6HCl

2BCl3+3H2+4Fe→2Fe2B+6HCl

[0008] The hydrogen chloride gas formed in boriding using BCl3 reacts with the iron of the base material to form volatile iron chlorides:

2HCl+Fe→FeCl2

[0009] The iron chlorides have high vapor pressures at the treatment temperatures in the range 500° C.-1200° C. which are employed, resulting in substantial, ongoing evaporation of iron chloride. This leads to hole formation between boride layer and substrate, as is always criticized in the case of the BCl3 process. Suppression of the hole formation is only possible if one succeeds in generating an impermeable boride layer within a very short time at the beginning of boriding. This is technically difficult in that to the present time it cannot be achieved reliably and reproducibly.

[0010] Apart from the purely thermal variant of CVD boriding, work on plasma-aided boriding (PACVD boriding) is also known. Hitherto, only diborane and boron trichloride have been used in this process variant, accompanied by the disadvantages which are already known from thermal CVD. An overview of the processes mentioned may be found in the review “Engineering the Surface with Boron Based Materials”, Surface Engineering 1985, Vol. 1, No. 3, pp. 203-217.

[0011] It is an object of the invention to provide a process for producing wear-resistant boride layers on metallic materials, which process does not suffer from the abovementioned disadvantages.

[0012] According to the invention, this object is achieved by a process which comprises mixing at least one boron halide selected from the group consisting of boron trifluoride, boron tribromide and boron triiodide as boron source with hydrogen and possibly argon and/or nitrogen to generate a reaction gas containing from 1 to 35% by volume of boron halide and activating the resulting mixture by means of a plasma discharge so as to enable boron to be transferred from the plasma to the metal surface.

[0013] The reaction gas can further comprise boron trichloride as boron source.

[0014] The reaction gas preferably contains from 5 to 20% by volume of boron halide, particularly preferably from 5 to 15% by volume of boron halide.

[0015] The reaction gas preferably contains from 20 to 90% by volume of H2, particularly preferably from 20 to 50% by volume of H2.

[0016] The reaction gas preferably comprises boron trifluoride.

[0017] Boron trifluoride is particularly preferably used as boron halide.

[0018] The reaction gas is fed to the treatment space in an amount of preferably from 0.5 to 2 l per minute, particularly preferably about 1 l/min.

[0019] Boriding is preferably carried out in the pressure range of 1-10 mbar under the action of a plasma discharge as is known, for example, from plasma coating units. The plasma discharge can be pulsed or unpulsed.

[0020] The required treatment temperatures of preferably from 400° C. to 1200° C., particularly preferably from 850 to 950° C., are generated by the plasma itself or, especially in the high-temperature range above 900° C., with the aid of additional heating.

[0021] The treatment time is preferably from 30 to 240 min, particularly preferably from 30 to 120 min.

[0022] The thickness of the boride layers is usually controlled via the treatment time, with the thicknesses of the layers increasing with increasing treatment time.

[0023] As further gases, the reaction gas can additionally comprise argon and/or nitrogen. They enable the activity of boron transfer to be controlled and sufficient heating of the specimens by the plasma to be achieved. The composition of the reaction gas can thus vary within wide limits depending on the treatment conditions and the material to be borided.

[0024] The process of the invention is particularly suitable for boriding ferrous materials.

[0025] In the process of the invention, molecular hydrogen present in the reaction gas is converted into atomic hydrogen by means of a plasma discharge. The atomic hydrogen reduces the boron halide (BY3) and thus enables boron to be transferred to the workpiece surface.

BY3+3H→B+3 HY

B+x ME→MexB

[0026] However, conversion of BY3 into BY2 by the plasma can also occur, in which case the following reactions can then proceed:

3BY2→B+2 BY3

B+x ME→MexB

[0027] Subsequent to boriding, the borided material can be subjected to an aftertreatment to convert any FeB formed into Fe2B. This can be achieved, for example, by a heat-treatment process subsequent to the boriding treatment by stopping the supply of boron halide and holding the workpiece at the treatment temperature for a further time. The duration of this diffusion treatment depends on the amount of FeB present and is usually 20-60 min.

[0028] The process can be carried out, for example, in a unit which is suitable for plasma coating and is known per se. This consists essentially of the following components:

[0029] The vacuum vessel (reactor) for accommodating the parts to be treated. The reactor should be heatable and allow operation in the temperature range from 400° C. to 1200° C.

[0030] The pumping system for evacuating the reactor and setting the working pressure.

[0031] The gas supply unit for mixing and metering in the reaction mixture.

[0032] The pulsed plasma power supply for generating and maintaining the plasma discharge in the vacuum vessel, such that the power introduced can be varied within a wide range by means of the pulse frequency or pulse width.

[0033] The system for neutralizing and disposing of the gas and the system for controlling and monitoring the operating parameters: the latter system controls and monitors the course of the process.

EXAMPLE 1

[0034] After introducing a 100Cr6 steel specimen into the reactor, it is heated in the plasma of a DC glow discharge having a constant pulse frequency (4 kHz) at a pressure of 10 mbar. The specimen is additionally heated by means of the heating of the reactor, thereby shortening the heating time. The heating and cooling of the specimen is carried out in a 1:1 mixture of argon and hydrogen. After the treatment temperature of 850° C. is reached, the boron source boron trifluoride is added at such a rate that a reaction gas mixture composed of 45% by volume of hydrogen, 40% by volume of argon and 15% by volume of boron trifluoride is formed. The gas mixture is fed to the vessel in an amount of 1 l/min. The duration of the plasma treatment is 200 min.

[0035] A metallographic section shows a boride layer having a mean thickness of 42 μm. The microhardness is 1800 HV0.05. The layer is free of FeB.

EXAMPLE 2

[0036] After introducing a Hastelloy B specimen into the reactor, it is heated in the plasma of a DC glow discharge having a constant pulse frequency (4 kHz). The specimen is heated to a temperature of 850° C. by means of the plasma discharge at 10 mbar. The power density is controlled via the pulse width. The specimen is heated exclusively by means of the glow discharge. The heating and cooling of the specimen is carried-out in a 1:1 mixture of argon and hydrogen. After the treatment temperature is reached, the boron source boron trifluoride is added in such an amount that a reaction mixture composed of 45% by volume of hydrogen, 45% by volume of argon and 10% by volume of boron trifluoride is formed. The gas mixture is fed to the vessel in an amount of 1 l/min. The treatment time is 240 min.

[0037] A metallographic section shows a boride layer having a mean thickness of 50 ∞m.

[0038] The micro hardness is 2400 HV0.05.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US6783794 *Jun 15, 2000Aug 31, 2004Volkswagen AgProducing a boride layer on a surface by plasma boronizing in which a gas mixture containing a boron-releasing gas is supplied to a reactor in which a glow discharge is generated
US7264682May 3, 2005Sep 4, 2007University Of Utah Research FoundationContacting a surface of a titanium mass with a particulate boron source containing activator, and filler to provide growth of titanium monoboride whiskers and heating to coat the mass with the whiskers; a TiB2 layer may be formed adjacent the TiB coating opposite opposite the mass
US7459105Jul 7, 2005Dec 2, 2008University Of Utah Research FoundationFlexural strength of 600-950 MPa; formed by high temperature processing of a powder precursor having carefully selected weight and size distributions of titanium and titanium diboride powders; can be cut by electro-discharge machining; nozzles, armor, metal refining electrodes, extrusion die inserts
US7501081Jan 25, 2007Mar 10, 2009University Of Utah Research FoundationFormed by growing TiB2-free titanium monoboride whiskers from a powder mixture of titanium, titanium diboride and densifier such as Fe and Mo at 1100 to 1400 degrees C.; network of interconnected titanium monoboride whiskers affords very high strength and wear resistance; electrodischarge machining
Classifications
U.S. Classification427/569, 427/255.4, 427/255.26
International ClassificationC23C16/28
Cooperative ClassificationC23C16/28
European ClassificationC23C16/28
Legal Events
DateCodeEventDescription
Dec 15, 2009FPExpired due to failure to pay maintenance fee
Effective date: 20091023
Oct 23, 2009LAPSLapse for failure to pay maintenance fees
May 4, 2009REMIMaintenance fee reminder mailed
Apr 18, 2005FPAYFee payment
Year of fee payment: 4