WO2013117241A1 - Micro-torque material strengthening by fiber spot-pinning - Google Patents
Micro-torque material strengthening by fiber spot-pinning Download PDFInfo
- Publication number
- WO2013117241A1 WO2013117241A1 PCT/EP2012/052360 EP2012052360W WO2013117241A1 WO 2013117241 A1 WO2013117241 A1 WO 2013117241A1 EP 2012052360 W EP2012052360 W EP 2012052360W WO 2013117241 A1 WO2013117241 A1 WO 2013117241A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- nanotubes
- fibrils
- fibers
- matrix material
- matrix
- Prior art date
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/14—Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/08—Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/14—Making alloys containing metallic or non-metallic fibres or filaments by powder metallurgy, i.e. by processing mixtures of metal powder and fibres or filaments
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
- C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
- C22C49/04—Light metals
- C22C49/06—Aluminium
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K7/00—Use of ingredients characterised by shape
- C08K7/02—Fibres or whiskers
Definitions
- the invention relates to the mechanical strengthening of a material by spot-pinning tubular fibers, fibrils or nanotubes in a metallic, ceramic, or polymeric matrix material, forming a compound material.
- HNTs Halloysite nanotubes
- CNTs Carbon nanotubes
- Halloysite nanotubes are types of naturally occurring aluminosilicate clays with nanotubular structures, having the chemical composition Al 2 Si 2 O 5 (OH) 4 2H2O+SiO 2 .
- HNTs are a weathering product of volcanic rocks of rhyolitic or granitic composition and occur in vast natural deposits. Typical characteristics include low specific weight (2.53 g/cm 3 ), high length-to-diameter ratio (aspect ratio 10-200), and low hydroxyl group density on the surface.
- the unique crystal structure of HNTs resembles that of carbon nanotubes (CNTs) in terms of aspect ratio.
- Halloysite nanotubes are inexpensive, readily available in quantity, environmentally benign, and safe and easy to process. Their CAS registry number is 1332-58-7. Halloysite nanotubes do not agglomerate, making them ideal for dispersion in compound applications. Halloysite nanotubes are hollow tubes with outer diameters typically ranging from about 40nm to 150nm, inner diameters from about 10nm to 100nm with lengths typically ranging from about 100nm to over 2 ⁇ m. Halloysite nanotubes can be functionalized (coated) with metallic and other substances to achieve a wide variety of electrical, chemical, and physical properties including excellent interfacing to a metallic compound matrix. Chemically, the outer surface of a not functionalized Halloysite nanotube has properties similar to SiO 2 while the inner cylinder surface has an Al 2 O 3 - like structure, providing an excellent interface to an aluminum matrix.
- US4299628(A) describes 'A composition for compressing and sintering to produce high-wear resistant articles essentially includes between 2% and 10% by weight, preferably 5% by weight, basalt powder and the remainder being metallurgical powder.
- HNTs can be seen as a form of basalt we are referring to this invention.
- US4299628(A) describes an inhomogeneous distribution of basalt particles in the metal matrix, where the compound material is manufactured in such a way that the 'sintered metal powder [is] having the entire pore space filled with basalt'. In this context 'pore space' means the voids in the metallic preform to be sintered.
- US4299628(A) does neither refer to any hollow basalt structure nor to HNTs.
- US2006147690(A1) describes a 'Metallic layer material, reinforced with basalt fibers, as well as products made thereof'. As the title indicates this patent describes an inhomogeneous distribution of layered basalt fibers in a metal matrix, with the basalt fibers arranged in layers.
- US2008219084(A1) discloses 'Fabrication Methods of Metal/Polymer/Ceramic Matrix Compounds Containing Randomly Distributed or Directionally Aligned Nanofibers'.
- claim 1 of this patent describes an alignment of the nanofibers by specifying: 'imparting a directionality to the nanofibers via application of a mechanical mass flowing process to a compound material with the nanofibers uniformly dispersed in the metal, polymer or ceramic matrix.
- US2010068526(A1) discloses 'MATERIALS CONTAINING CARBON NANOTUBES, PROCESS FOR PRODUCING THEM AND USE OF THE MATERIALS'. However, according to the invention 'this is achieved by materials containing at least one metal and/or at least one polymer laminated in layers alternating with layers of CNT'. This means that the CNTs are not homogeneously distributed in the metal matrix but arranged in layers.
- a fiber preform is similar to a sponge made of the fibers that will later form the reinforcing structure in the compound. This 'sponge' is placed in a mold and infiltrated with the liquid matrix material.
- the preform also provides for the proper fiber orientation, volume fraction, and distribution in the compound. After consolidation of the matrix material the orientation of fibers in the matrix is as defined by the fiber preform.
- the main challenges to the use of preforms are the high pressures and temperatures used to infiltrate the matrix material in particular when the matrix material is a metal. The high pressures and temperatures can break or otherwise chemically destroy the preform.
- Fiber-matrix bonding is a key factor in the effective transmission of mechanical load from the matrix to the fiber. It is essential that this bond is strong for the compound to develop the desired increase in mechanical strength. Otherwise, on the onset of mechanical stress, the fibers could potentially slide within the matrix, and thus not carry any of the load. The result of this would be that the matrix, now effectively reduced in cross sectional area due to the volume occupied by the ineffective fibers, has to support the entire load which would result in a lower strength level.
- wetting of the fiber by the matrix material is essential.
- One method to obtain this wetting consists of subjecting the fiber within the liquid matrix to very high pressures produced by a squeeze casting process.
- squeeze casting has limitations because not all compounds can be produced at these high pressures and temperatures.
- the first method consisted in sintering the fibers together. With this approach, there was substantial degradation of the fibers due to grain growth which reduced fiber strength.
- the second method a series of binders based on phosphoric acid solutions with and without aluminum hydroxide were used, with the intent of forming an aluminum phosphate binder to bind the fibers together. When only the phosphoric acid solution was used it damaged and weakened the fibers due to chemical attack, while a mixture with aluminum hydroxide improved the properties of the preform.
- WO2011032791(A1) describes a mechanical method for functionalizing CNTs prior to dispersing them in the matrix material by high energy ball milling (here called mechanical alloying) .
- the functionalization is achieved by roughening the surface of at least some of the CNTs.
- CNT-agglomerates are submitted to a high pressure of 100 kg/cm ⁇ 2> (9.8 MPa). It was found that while the CNTs retain the same inner structure, the outermost layer or layers burst or break, thereby developing a rough surface. With the rough surface, the interlocking effect between CNTs and the metal matrix is increased, which in turn increases the nano-stabilization or strengthening effect.
- the present invention describes a method for increasing the mechanical strength of a matrix material characterized in that the embedded particles have a spot-wise mechanical connection to the surrounding matrix and can slide in the other areas relative to the matrix material. Because of that micro-torques acting at the embedded particles are generated when the compound material is exposed to external mechanical stress, which causes an increased mechanical strength of the compound material.
- a mixture of commercially available HNTs and a commercially available aluminum powder, in which at least a fraction of the powder particles have a size smaller than the inner (open) diameter (lumen) of the HNTs, are processed in a powder mixer such that the metal particles enter the HNTs, filling the inner tubular space of the HNTs completely or in part.
- Figure 1 shows a principle picture where the matrix material powder particles (a) enter the tubular fiber (b).
- step 2 the mixture produced in step 1 is compacted by hot isostatic pressing, such as to form a solid block of aluminum / HNT compound material where the filled HNTs are firmly embedded in the aluminum matrix.
- Figure 2 shows a principle cross section of a compacted material body (b) with embedded HNTs (a).
- the formation of a solid block of compound material can also be done by infiltrating a HNT preform with liquid aluminum and subsequent consolidation or by dispersion-stirring the HNTs in an aluminum melt and subsequent consolidation.
- the present invention now takes advantage of the fact that the outer surface of HNTs has similar chemical properties as SiO 2 , which does not have good bonding properties to the aluminum matrix, while the inner walls of a Halloysite nanotube have an Al 2 O 3 like structure which provides for an excellent bonding interface between the aluminum matrix and the inner walls of the HNTs.
- the outer layer of any aluminum part exposed to an oxygen containing environment contains always Al 2 O 3 , the aluminum matrix and the inner wall of the HNTs can essentially share the same surface. This in turn means, that the ends of the HNTs are much stronger mechanically attached to the aluminum matrix than the rest of the fiber, which can easily slide in the matrix because of the much weaker bonding between the outer hull of the fiber and the surrounding aluminum matrix.
- Figure 3 shows a schematic solid block of a matrix material (a) containing a fiber (b) which has been conditioned in the above described way.
- the fiber is spot-pinned to the surrounding matrix in the areas marked with concentric circles (b), while the outer hull (c) can slide in the matrix, symbolized by the opposing arrow rows.
- the present invention takes further advantage of the fact that, if a mechanical tensile or compression stress is applied to the compacted compound material, the mechanical stress is transferred from the metal matrix much stronger to the ends of the HNTs than to the fiber hull because of the different bonding interfaces. This in turn causes a torque force acting on the HNTs.
- Figures 4 shows schematically a sold block of matrix material (c), in which a tensile stress (a) causes a torque (b), which tries to align the fiber (d) parallel to the external force vector (a).
- Figures 5 shows schematically a sold block of matrix material (c), in which a compression stress (a) causes a torque (b), which tries to align the fiber (d) perpendicular to the external force vector (a).
- the stress induced torque is transferred back from the fiber to the matrix and dissipated as heat in the matrix material. This in turn leads to an increase in tensile and compression force necessary to cause any deformation of the compound material.
- the increment in force necessary to cause a deformation, or with other word the increment in mechanical strength, is proportional to the fraction of the applied stress which is converted into multiple internal micro-torque actions of the embedded HNTs and thus proportional to the heat generated in the material.
- FIG 1 The matrix material powder particles (a) enter the tubular fiber (b)
- Figure 2 Cross section of a compacted material body (b) with embedded HNTs (a).
- Figure 3 Schematic solid block of a matrix material (a) containing a fiber (b).
- the fiber is spot-pinned to the surrounding matrix in the areas marked with concentric circles (b), while the outer hull (c) can slide in the matrix, symbolized by the opposing arrow rows.
- Figure 4 Schematic picture of a sold block of matrix material (c), in which a tensile stress (a) causes a torque (b), which tries to align the fiber (d) parallel to the external force vector (a).
- Figure 5 Schematic picture of a sold block of matrix material (c), in which a compression stress (a) causes a torque (b), which tries to align the fiber (d) perpendicular to the external force vector (a).
- Figure 6 The particle size distribution of the HNTs as received.
- Figure 7 Morphology and the tubular structure of the HNTs as received, showing the diameter of the tube openings (a) and the outer diameter (b) of the HNTs.
- Figure 10 Micrograph of the HNTs after the mixing showing that the HNTs (b) are at least partly filled with aluminum particles (a).
- the method for making the compound material according to the present invention comprises the following steps:
- HNTs Halloysite nanotubes
- HNTs Halloysite nanotubes
- FIG. 7 A SEM micrograph showing the morphology and the tubular structure of the HNTs as received is depicted in Figure 7.
- the aluminum powder was then milled for 24 hours using a high energy planetary ball mill (Fritsch, planetary micro mill PULVERISETTE 7). After the milling process the resulting powder had a much finer grain size than the starting powder.
- the particle size distribution of the smaller size end of the spectrum of the aluminum powder after high energy milling is shown in Figure 9. As can be seen, a substantial amount of particles has a size smaller than 50nm, which means, that they fit into the inner tubes of the HNTs described in the previous paragraph.
- FIG. 10 shows a high resolution micrograph of a sample of the HNTs after the mixing. It is clearly visible that the HNTs (b) are at least partly filled with aluminum particles (a) sitting inside the inner tubes of the HNTs.
- the mixed powder material manufactured in steps 1-3 can now be used as a source material for forming semi-finished or finished articles by powder metallurgical methods.
- the mixed powder material of the invention can advantageously be further processed by cold isostatic pressing (CIP) and hot isostatic pressing (HIP).
- the compound material can be further processed by hot working, powder milling or powder extrusion at high temperatures up to the melting temperature of some of the metal phases.
- the powder can be directly processed by continuous powder rolling or powder extrusion.
- Table 1 shows exemplary tensile test results of the compound material manufactured according to steps 1-3 after hot isostatic pressing (HIP).
- the tensile strength was increased by more than a factor of five at a concentration of 10 weight % of HNTs in the aluminum matrix.
- concentrations of HNTs in the matrix were lower but still at least a factor of two higher than that of the pure matrix material.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Powder Metallurgy (AREA)
Abstract
The invention discloses a method for strengthening a material by stress induced micro-torques; a method for making a compound material which is strengthened by stress induced micro-torques acting at spot-pinned fibers, fibrils or nanotubes; and a compound material consisting of a metallic, ceramic, or polymeric matrix material which is mechanically strengthened by embedding tubular fibers, fibrils or nanotubes in the matrix material, characterized in that the bonding strength between the matrix material and the inner tube walls of the fibers, fibrils or nanotubes is stronger than the bonding strength between the matrix material and the outer hull of the tubular fibers, fibrils or nanotubes, which causes stress induced micro-torques acting at the embedded fibers, fibrils or nanotubes, when the compound material is exposed to external mechanical stress, which in turn causes an increased mechanical strength of the compound material in comparison to the pure matrix material.
Description
The invention relates to the mechanical
strengthening of a material by spot-pinning tubular fibers, fibrils or
nanotubes in a metallic, ceramic, or polymeric matrix material, forming a
compound material.
Strengthening of a material by embedding high aspect
ratio fibers has been done in the past. In particular Halloysite nanotubes
(HNTs) and Carbon nanotubes (CNTs) have been used for that purpose.
Halloysite nanotubes (HNTs) are types of naturally
occurring aluminosilicate clays with nanotubular structures, having the
chemical composition
Al2Si2O5(OH)42H2O+SiO2 .
HNTs are a weathering product of volcanic rocks of rhyolitic or granitic
composition and occur in vast natural deposits. Typical characteristics include
low specific weight (2.53 g/cm3), high length-to-diameter ratio
(aspect ratio 10-200), and low hydroxyl group density on the surface. The
unique crystal structure of HNTs resembles that of carbon nanotubes (CNTs) in
terms of aspect ratio. But unlike carbon nanotubes, naturally occurring
Halloysite nanotubes are inexpensive, readily available in quantity,
environmentally benign, and safe and easy to process. Their CAS registry number
is 1332-58-7. Halloysite nanotubes do not agglomerate, making them ideal for
dispersion in compound applications. Halloysite nanotubes are hollow tubes with
outer diameters typically ranging from about 40nm to 150nm, inner diameters
from about 10nm to 100nm with lengths typically ranging from about 100nm to
over 2 μm. Halloysite nanotubes can be functionalized (coated) with metallic
and other substances to achieve a wide variety of electrical, chemical, and
physical properties including excellent interfacing to a metallic compound
matrix. Chemically, the outer surface of a not functionalized Halloysite
nanotube has properties similar to SiO2 while the inner cylinder
surface has an Al2O3 - like structure, providing an
excellent interface to an aluminum matrix.
There are different methods for dispersing HNTs and
other tubular fibers, fibrils or nanotubes in a matrix. In particular methods
for the dispersion of carbon nanotubes in a metal matrix by high energy milling
have been disclosed before.
Recently a high energy ball milling method for making
an aluminum compound material consisting of Al6061 as the matrix material and
HNTs as reinforcing particles has been described (L.A. Dobrzański, B. Tomiczek,
M. Adamiak, Manufacturing of EN AW6061 matrix compounds reinforced by
Halloysite nanotubes, Journal of Achievements in Materials and Manufacturing
Engineering 49/1 (2011) 82-89). For the experiments described in this article a
standard high energy laboratory ball mill (manufacturer: Fritsch) was used.
With 10w% of HNTs in the Al6061 matrix a maximum increase of compression yield
strength from 276 MPa to 481.6 MPa (about 175%) was realized according to the
article.
US4299628(A) describes 'A composition for compressing
and sintering to produce high-wear resistant articles essentially includes
between 2% and 10% by weight, preferably 5% by weight, basalt powder and the
remainder being metallurgical powder.' Since HNTs can be seen as a form of
basalt we are referring to this invention. However, US4299628(A) describes an
inhomogeneous distribution of basalt particles in the metal matrix, where the
compound material is manufactured in such a way that the 'sintered metal powder
[is] having the entire pore space filled with basalt'. In this context 'pore
space' means the voids in the metallic preform to be sintered. US4299628(A)
does neither refer to any hollow basalt structure nor to HNTs.
US2006147690(A1) describes a 'Metallic layer
material, reinforced with basalt fibers, as well as products made thereof'. As
the title indicates this patent describes an inhomogeneous distribution of
layered basalt fibers in a metal matrix, with the basalt fibers arranged in
layers.
US2008219084(A1) discloses 'Fabrication Methods of
Metal/Polymer/Ceramic Matrix Compounds Containing Randomly Distributed or
Directionally Aligned Nanofibers'. However, claim 1 of this patent describes an
alignment of the nanofibers by specifying: 'imparting a directionality to the
nanofibers via application of a mechanical mass flowing process to a compound
material with the nanofibers uniformly dispersed in the metal, polymer or
ceramic matrix.'
US2010068526(A1) discloses 'MATERIALS CONTAINING
CARBON NANOTUBES, PROCESS FOR PRODUCING THEM AND USE OF THE MATERIALS'.
However, according to the invention 'this is achieved by materials containing
at least one metal and/or at least one polymer laminated in layers alternating
with layers of CNT'. This means that the CNTs are not homogeneously distributed
in the metal matrix but arranged in layers.
Another method for embedding a fiber structure in a
matrix material is the infiltration of fiber preforms with liquid matrix
material. Essentially, a fiber preform is similar to a sponge made of the
fibers that will later form the reinforcing structure in the compound. This
'sponge' is placed in a mold and infiltrated with the liquid matrix material.
The preform also provides for the proper fiber orientation, volume fraction,
and distribution in the compound. After consolidation of the matrix material
the orientation of fibers in the matrix is as defined by the fiber preform. The
main challenges to the use of preforms are the high pressures and temperatures
used to infiltrate the matrix material in particular when the matrix material
is a metal. The high pressures and temperatures can break or otherwise
chemically destroy the preform.
Whether the infiltration of a liquid matrix material
into a preform, conventional powder mixing technology or a ball milling
technology at various energies is used to disperse nanoparticles homogeneously
in a polymeric, ceramic or metal matrix there is always the additional
necessity to create a good bonding (interfacing) between the embedded
nanoparticles and the surrounding matrix in order to improve the mechanical
strength properties of the compound material in comparison to the pure matrix
material.
Fiber-matrix bonding is a key factor in the
effective transmission of mechanical load from the matrix to the fiber. It is
essential that this bond is strong for the compound to develop the desired
increase in mechanical strength. Otherwise, on the onset of mechanical stress,
the fibers could potentially slide within the matrix, and thus not carry any of
the load. The result of this would be that the matrix, now effectively reduced
in cross sectional area due to the volume occupied by the ineffective fibers,
has to support the entire load which would result in a lower strength
level.
In order to obtain proper bonding, wetting of the
fiber by the matrix material is essential. One method to obtain this wetting
consists of subjecting the fiber within the liquid matrix to very high
pressures produced by a squeeze casting process. However, squeeze casting has
limitations because not all compounds can be produced at these high pressures
and temperatures.
There are several chemical ways to condition the
reinforcing particles in order to ensure good interfacing with the matrix.
Usually these methods try to diminish the pullout potential of fibers from the
matrix by bonding the fibers together, in a manner similar to a net. Then,
there is a mechanical restriction to fiber sliding as the matrix material is
restricted due to the bonds between the fiber strands. Peng et al. have bonded
alumina fibers in preforms together (Peng, H. X., Fan, Z., Mudher, D. S., and
Evans, J. R. G. (2002). 'Microstructures and mechanical properties of
engineered short fiber reinforced aluminum matrix compounds'. Materials Science
and Engineering A, 335: 207-216).
They used two different methods: The first method
consisted in sintering the fibers together. With this approach, there was
substantial degradation of the fibers due to grain growth which reduced fiber
strength. In the second method a series of binders based on phosphoric acid
solutions with and without aluminum hydroxide were used, with the intent of
forming an aluminum phosphate binder to bind the fibers together. When only the
phosphoric acid solution was used it damaged and weakened the fibers due to
chemical attack, while a mixture with aluminum hydroxide improved the
properties of the preform.
WO2011032791(A1) describes a mechanical method for
functionalizing CNTs prior to dispersing them in the matrix material by high
energy ball milling (here called mechanical alloying) . The functionalization
is achieved by roughening the surface of at least some of the CNTs. In the
described method CNT-agglomerates are submitted to a high pressure of 100
kg/cm<2> (9.8 MPa). It was found that while the CNTs retain the same
inner structure, the outermost layer or layers burst or break, thereby
developing a rough surface. With the rough surface, the interlocking effect
between CNTs and the metal matrix is increased, which in turn increases the
nano-stabilization or strengthening effect.
The present invention describes a method for
increasing the mechanical strength of a matrix material characterized in that
the embedded particles have a spot-wise mechanical connection to the
surrounding matrix and can slide in the other areas relative to the matrix
material. Because of that micro-torques acting at the embedded particles are
generated when the compound material is exposed to external mechanical stress,
which causes an increased mechanical strength of the compound material.
Both chemical treatment of the nanoparticles and
mechanical functionalization methods of the reinforcing particles are
additional steps in the production of a compound material. Desirable is a
solution in which no functionalization is necessary but still good reinforcing
effects can be achieved by embedding reinforcing particles in a matrix.
So far, all strengthening methods using particles
for the strengthening of a matrix material rely on a good mechanical interface
between the matrix and an area as large as possible of the outer surface of the
particle, and in particular try to avoid any sliding of the particle in the
matrix. Desirable is a solution in which a spot-like mechanical pinning of the
reinforcing particle in the matrix is sufficient. Desirable is further a
solution in which a sliding of the reinforcing particle in the matrix does not
reduce the reinforcing effect.
So far, all strengthening methods using fiber
shaped particles rely on the tensile strength of the fiber and try to transfer
the largest possible portion of this tensile strength from the fiber to the
matrix through a good mechanical interface between the matrix and an area as
large as possible of the outer surface of the particle. Desirable is a solution
in which the geometrical properties and the bending strength of the reinforcing
particle contribute to the strengthening effect.
For the purposes of clear understanding of the
principles of the invention, reference will now be made to the preferred
embodiment illustrated in the drawings and specific language will be used to
describe the same. It will, nevertheless, be understood that no limitation of
the scope of the invention is thereby intended. In particular, alterations and
further modifications in the illustrated product, method, use, and further
applications of the principles of the invention as illustrated therein, are
contemplated as would normally occur now or in the future to one skilled in the
art to which the invention relates.
For the purposes of clear understanding of the
principles of the invention, reference will also be made to the preferred
embodiment of a method for making the compound material according to the
present invention, comprising aluminum as a representation of the matrix
material and Halloysite nanotubes (HNTs) as a representation of the reinforcing
tubular fibers, fibrils or nanotubes.
In a first step, a mixture of commercially
available HNTs and a commercially available aluminum powder, in which at least
a fraction of the powder particles have a size smaller than the inner (open)
diameter (lumen) of the HNTs, are processed in a powder mixer such that the
metal particles enter the HNTs, filling the inner tubular space of the HNTs
completely or in part. Figure 1 shows a principle picture where the matrix
material powder particles (a) enter the tubular fiber (b).
In a second step the mixture produced in step 1 is
compacted by hot isostatic pressing, such as to form a solid block of aluminum
/ HNT compound material where the filled HNTs are firmly embedded in the
aluminum matrix. Figure 2 shows a principle cross section of a compacted
material body (b) with embedded HNTs (a).
The formation of a solid block of compound
material can also be done by infiltrating a HNT preform with liquid aluminum
and subsequent consolidation or by dispersion-stirring the HNTs in an aluminum
melt and subsequent consolidation.
The present invention now takes advantage of the
fact that the outer surface of HNTs has similar chemical properties as
SiO2, which does not have good bonding properties to the aluminum
matrix, while the inner walls of a Halloysite nanotube have an
Al2O3 like structure which provides for an excellent
bonding interface between the aluminum matrix and the inner walls of the HNTs.
In simple terms, since the outer layer of any aluminum part exposed to an
oxygen containing environment contains always Al2O3 , the
aluminum matrix and the inner wall of the HNTs can essentially share the same
surface. This in turn means, that the ends of the HNTs are much stronger
mechanically attached to the aluminum matrix than the rest of the fiber, which
can easily slide in the matrix because of the much weaker bonding between the
outer hull of the fiber and the surrounding aluminum matrix. Figure 3 shows a
schematic solid block of a matrix material (a) containing a fiber (b) which has
been conditioned in the above described way. The fiber is spot-pinned to the
surrounding matrix in the areas marked with concentric circles (b), while the
outer hull (c) can slide in the matrix, symbolized by the opposing arrow
rows.
The present invention takes further advantage of
the fact that, if a mechanical tensile or compression stress is applied to the
compacted compound material, the mechanical stress is transferred from the
metal matrix much stronger to the ends of the HNTs than to the fiber hull
because of the different bonding interfaces. This in turn causes a torque force
acting on the HNTs.
Figures 4 shows schematically a sold block of
matrix material (c), in which a tensile stress (a) causes a torque (b), which
tries to align the fiber (d) parallel to the external force vector (a).
Figures 5 shows schematically a sold block of
matrix material (c), in which a compression stress (a) causes a torque (b),
which tries to align the fiber (d) perpendicular to the external force vector
(a).
However, since the HNTs are completely enclosed by
the aluminum matrix the stress induced torque is transferred back from the
fiber to the matrix and dissipated as heat in the matrix material. This in turn
leads to an increase in tensile and compression force necessary to cause any
deformation of the compound material. The increment in force necessary to cause
a deformation, or with other word the increment in mechanical strength, is
proportional to the fraction of the applied stress which is converted into
multiple internal micro-torque actions of the embedded HNTs and thus
proportional to the heat generated in the material.
Figure 1: The matrix material powder particles (a)
enter the tubular fiber (b)
Figure 2: Cross section of a compacted material body
(b) with embedded HNTs (a).
Figure 3: Schematic solid block of a matrix material
(a) containing a fiber (b). The fiber is spot-pinned to the surrounding matrix
in the areas marked with concentric circles (b), while the outer hull (c) can
slide in the matrix, symbolized by the opposing arrow rows.
Figure 4: Schematic picture of a sold block of
matrix material (c), in which a tensile stress (a) causes a torque (b), which
tries to align the fiber (d) parallel to the external force vector (a).
Figure 5: Schematic picture of a sold block of
matrix material (c), in which a compression stress (a) causes a torque (b),
which tries to align the fiber (d) perpendicular to the external force vector
(a).
Figure 6: The particle size distribution of the HNTs
as received.
Figure 7: Morphology and the tubular structure of
the HNTs as received, showing the diameter of the tube openings (a) and the
outer diameter (b) of the HNTs.
Figure 8: Particle size distribution of aluminum
powder as received
Figure 9: Particle size distribution of aluminum
powder after high energy milling
Figure 10: Micrograph of the HNTs after the mixing
showing that the HNTs (b) are at least partly filled with aluminum particles
(a).
For the purposes of clear understanding of the
principles of the invention, reference will now be made to the preferred
embodiment illustrated in the drawings and specific language will be used to
describe the same. It will, nevertheless, be understood that no limitation of
the scope of the invention is thereby intended. In particular, alterations and
further modifications in the illustrated product, method, use, and further
applications of the principles of the invention as illustrated therein, are
contemplated as would normally occur now or in the future to one skilled in the
art to which the invention relates.
In the following, a processing strategy for
producing a compound material according to the invention from exemplary
constituent materials will be explained. Also, exemplary use of the compound
material in different ways of compacting will be discussed.
In the preferred embodiment, the method for making
the compound material according to the present invention comprises the
following steps:
1. Procurement of Halloysite nanotubes (HNTs)
2. Preparation of fine grain aluminum powder
3. Filling the HNTs with aluminum powder
4. Compacting the aluminum powder / HNT mixture
It is to be understood that these steps represent an
embodiment of the production method, in which a compound material according to
an embodiment of the invention is obtained.
1. PROCUREMENT OF HNTs
In a preferred embodiment, commercially available
Halloysite nanotubes (HNTs) are used, provided by NaturalNano Inc. (Rochester,
NY, USA). The particle size distribution of the HNTs as received is shown in
Figure 6.
A SEM micrograph showing the morphology and the
tubular structure of the HNTs as received is depicted in Figure 7. By a
geometrical analysis of the tube openings (a) visible in the picture, and the
outer diameter (b) of the HNTs, it was found that the outer diameter of the
HNTs was in the range of about 100-150nm, while the inner tube diameter of the
HNTs was in the range of about 50-100nm.
2. PREPARATION OF FINE GRAIN ALUMINUM POWDER
Commercially available, air atomized, fine grain
aluminum powder (EN AW2024) from ECKA (Germany) was used as matrix material.
The particle size distribution of the aluminum powder as received is shown in
Figure 8.
The aluminum powder was then milled for 24 hours
using a high energy planetary ball mill (Fritsch, planetary micro mill
PULVERISETTE 7). After the milling process the resulting powder had a much
finer grain size than the starting powder. The particle size distribution of
the smaller size end of the spectrum of the aluminum powder after high energy
milling is shown in Figure 9. As can be seen, a substantial amount of particles
has a size smaller than 50nm, which means, that they fit into the inner tubes
of the HNTs described in the previous paragraph.
- FILLING OF THE HNTs WITH ALUMINUM POWDER
The HNTs were then added to the pre-milled aluminum
powder containing the increased fraction of particles having a diameter smaller
than the inner tube diameter of the HNTs, and the mixture was mixed for 1 hour
at low energies. Figure 10 shows a high resolution micrograph of a sample of
the HNTs after the mixing. It is clearly visible that the HNTs (b) are at least
partly filled with aluminum particles (a) sitting inside the inner tubes of the
HNTs.
4. COMPACTING OF THE ALUMINUM POWDER / HNT
MIXTURE
The mixed powder material manufactured in steps 1-3
can now be used as a source material for forming semi-finished or finished
articles by powder metallurgical methods. In particular, it has been found that
the mixed powder material of the invention can advantageously be further
processed by cold isostatic pressing (CIP) and hot isostatic pressing (HIP).
Alternatively, the compound material can be further processed by hot working,
powder milling or powder extrusion at high temperatures up to the melting
temperature of some of the metal phases. Also, the powder can be directly
processed by continuous powder rolling or powder extrusion.
Table 1 shows exemplary tensile test results of the
compound material manufactured according to steps 1-3 after hot isostatic
pressing (HIP). The tensile strength was increased by more than a factor of
five at a concentration of 10 weight % of HNTs in the aluminum matrix. At lower
(5w%) and higher (15w%) concentrations of HNTs in the matrix the achieved
strength levels were lower but still at least a factor of two higher than that
of the pure matrix material.
Although a preferred exemplary embodiment is shown
and specified in detail in the drawings and the preceding specification, these
should be viewed as purely exemplary and not as limiting the invention. It is
noted in this regard that only the preferred exemplary embodiment is shown and
specified, and all variations and modifications should be protected that
presently or in the future lie within the scope of protection of the appending
claims. It is also noted that the term 'compound' can also be read as
'composite' in the context of the present invention.
TABLE 1
Aluminum powder type | HNT content [%] | Yield strength [MPa] | Increase [%] |
| 0 | 95 | 0 |
| 5 | 262 | 276 |
| 10 | 515 | 542 |
EN AW2024 | 15 | 485 | 510 |
Claims (15)
- Method for strengthening a material by generating stress induced micro-torques in the material, which convert mechanical energy into heat.
- Compound material with embedded fibers, fibrils or nanotubes in a matrix material, wherein the bonding strength between the matrix material and limited sections of the fiber surfaces, fibrils or nanotubes is stronger than the bonding strength between the matrix material and the rest of the surfaces of the tubular fibers, fibrils or nanotubes.
- Compound material according to claim 2 with embedded tubular fibers, fibrils or nanotubes in a matrix material, wherein the bonding strength between the matrix material and the inner tube walls of the fibers, fibrils or nanotubes is stronger than the bonding strength between the matrix material and the outer hull of the tubular fibers, fibrils or nanotubes.
- Compound material according to claim 2, wherein the matrix material is a metal, or a ceramic, or a polymer.
- Compound material according to claim 2, wherein the difference in bonding strengths is caused by inhomogeneous chemical or mechanical properties of the surfaces of the fibers, fibrils or nanotubes.
- Compound material according to claim 2, wherein stress-induced micro-torques are generated at the embedded tubular fibers, fibrils or nanotubes when the compound material is exposed to external mechanical stress.
- Compound material according to claim 2, wherein the mechanical transfer of the stress-induced micro-torques to the surrounding matrix causes an increase in mechanical strength of the compound material in comparison to the strength of the pure matrix material.
- Method for making a compound material according to claim 3 characterized in that a filling process is used which fills the inner tubular space of the fibers, fibrils or nanotubes completely or in part with the matrix material and in that a subsequent solidification process is used to form a solid material body from the fiber, fibril or nanotube / matrix material mixture.
- Method according to claim 8 wherein the filling process is infiltration of liquid matrix material into the fibers, fibrils or nanotubes.
- Method according to claim 8 wherein the filling process is dispersion of the fibers, fibrils or nanotubes in a matrix material.
- Method according to claim 8 wherein the filling process is powder mixing of a mixture containing the matrix material in a powder form and the fibers, fibrils or nanotubes.
- Method according to claim 8 wherein the filling process is mechanical powder milling of a mixture containing the matrix material in a powder form and the fibers, fibrils or nanotubes.
- Method according to claim 8 wherein the solidification process is compacting of a powder material.
- Method according to claim 8 wherein the solidification process is solidification of a melt.
- Method according to claim 8 wherein the solidification process is curing of a polymer.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/EP2012/052360 WO2013117241A1 (en) | 2012-02-10 | 2012-02-10 | Micro-torque material strengthening by fiber spot-pinning |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/EP2012/052360 WO2013117241A1 (en) | 2012-02-10 | 2012-02-10 | Micro-torque material strengthening by fiber spot-pinning |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2013117241A1 true WO2013117241A1 (en) | 2013-08-15 |
Family
ID=46085887
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2012/052360 WO2013117241A1 (en) | 2012-02-10 | 2012-02-10 | Micro-torque material strengthening by fiber spot-pinning |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2013117241A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116786816A (en) * | 2023-08-18 | 2023-09-22 | 山东瑞斯卡诺轴承科技有限公司 | Alloy material for bearing rolling bodies and preparation method thereof |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4299628A (en) | 1978-06-29 | 1981-11-10 | Bleistahl G.M.B.H. | Metal powder composition and article made therefrom |
US20060147690A1 (en) | 2005-01-04 | 2006-07-06 | Airbus Deutschland Gmbh | Metallic layer material, reinforced with basalt fibers, as well as products made thereof |
WO2006134405A1 (en) * | 2005-06-16 | 2006-12-21 | Paata Gogoladze | Method of manufacturing aluminium-based composite material |
US20080219084A1 (en) | 2005-05-17 | 2008-09-11 | Dong-Hyun Bae | Fabrication Methods of Metal/Polymer/Ceramic Matrix Composites Containing Randomly Distributed or Directionally Aligned Nanofibers |
US20100068526A1 (en) | 2006-10-31 | 2010-03-18 | Horst Adams | Materials containing carbon nanotubes, process for producing them and use of the materials |
WO2011032791A1 (en) | 2009-09-17 | 2011-03-24 | Bayer International Sa, Ftb | A compound material comprising a metal and nanoparticles |
-
2012
- 2012-02-10 WO PCT/EP2012/052360 patent/WO2013117241A1/en active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4299628A (en) | 1978-06-29 | 1981-11-10 | Bleistahl G.M.B.H. | Metal powder composition and article made therefrom |
US20060147690A1 (en) | 2005-01-04 | 2006-07-06 | Airbus Deutschland Gmbh | Metallic layer material, reinforced with basalt fibers, as well as products made thereof |
US20080219084A1 (en) | 2005-05-17 | 2008-09-11 | Dong-Hyun Bae | Fabrication Methods of Metal/Polymer/Ceramic Matrix Composites Containing Randomly Distributed or Directionally Aligned Nanofibers |
WO2006134405A1 (en) * | 2005-06-16 | 2006-12-21 | Paata Gogoladze | Method of manufacturing aluminium-based composite material |
US20100068526A1 (en) | 2006-10-31 | 2010-03-18 | Horst Adams | Materials containing carbon nanotubes, process for producing them and use of the materials |
WO2011032791A1 (en) | 2009-09-17 | 2011-03-24 | Bayer International Sa, Ftb | A compound material comprising a metal and nanoparticles |
Non-Patent Citations (4)
Title |
---|
ISMAIL H ET AL: "Curing characteristics, tensile properties and morphology of palm ash/halloysite nanotubes/ethylene-propylene-diene monomer (EPDM) hybrid composites", POLYMER TESTING, ELSEVIER, AMSTERDAM, NL, vol. 29, no. 7, 1 October 2010 (2010-10-01), pages 872 - 878, XP027247213, ISSN: 0142-9418, [retrieved on 20100702] * |
L.A. DOBRZANSKI; B. TOMICZEK; M. ADAMIAK: "Manufacturing of EN AW6061 matrix compounds reinforced by Halloysite nanotubes", JOURNAL OF ACHIEVEMENTS IN MATERIALS AND MANUFACTURING ENGINEERING, 2011, pages 82 - 89, XP002686120 |
PASBAKHSH P ET AL: "Influence of maleic anhydride grafted ethylene propylene diene monomer (MAH-g-EPDM) on the properties of EPDM nanocomposites reinforced by halloysite nanotubes", POLYMER TESTING, ELSEVIER, AMSTERDAM, NL, vol. 28, no. 5, 1 August 2009 (2009-08-01), pages 548 - 559, XP026155473, ISSN: 0142-9418, [retrieved on 20090423], DOI: 10.1016/J.POLYMERTESTING.2009.04.004 * |
PENG, H. X.; FAN, Z.; MUDHER, D. S.; EVANS, J. R. G.: "Microstructures and mechanical properties of engineered short fiber reinforced aluminum matrix compounds", MATERIALS SCIENCE AND ENGINEERING A, vol. 335, 2002, pages 207 - 216 |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116786816A (en) * | 2023-08-18 | 2023-09-22 | 山东瑞斯卡诺轴承科技有限公司 | Alloy material for bearing rolling bodies and preparation method thereof |
CN116786816B (en) * | 2023-08-18 | 2024-01-26 | 山东瑞斯卡诺轴承科技有限公司 | Alloy material for bearing rolling bodies and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8889065B2 (en) | Micron size powders having nano size reinforcement | |
DE60125798T2 (en) | COMPOSITE MATERIALS WITH CERAMIC MATRIX ON BORCARBID BASIS | |
Boccaccini et al. | Borosilicate glass matrix composites containing multi-wall carbon nanotubes | |
CN109338167B (en) | Preparation method of carbon nano tube composite material | |
US7862897B2 (en) | Biphasic nanoporous vitreous carbon material and method of making the same | |
US20020068164A1 (en) | Friction body of silicon-infiltrated, carbon fiber-reinforced porous carbon and method for making same | |
US20050181209A1 (en) | Nanotube-containing composite bodies, and methods for making same | |
CA2402377A1 (en) | Improved golf club and other structures, and novel methods for making such structures | |
DE2648459A1 (en) | METHOD FOR MANUFACTURING SILICON CARBIDE FIBER-REINFORCED COMPOSITE MATERIAL | |
JPH0365527A (en) | Silicon oxicarbide glass and its article | |
Chen et al. | Mechanical and thermal properties of attapulgite clay reinforced polymethylmethacrylate nanocomposites | |
JP2002356381A (en) | METHOD OF MANUFACTURING SiC COMPOSITE MATERIAL OF SiC REINFORCED TYPE | |
Deng et al. | Floating catalyst chemical vapor infiltration of nanofilamentous carbon reinforced carbon/carbon composites–Tribological behavior and wear mechanism | |
Zhang et al. | Scalable manufacturing of mechanical robust bioinspired ceramic–resin composites with locally tunable heterogeneous structures | |
WO2013117241A1 (en) | Micro-torque material strengthening by fiber spot-pinning | |
CN106191719B (en) | A kind of high-performance ceramic braking composite material and preparation method thereof | |
CN109652679B (en) | Carbon nanotube and endogenous nano TiC particle mixed reinforced aluminum-based composite material and preparation method thereof | |
CN116573952A (en) | Adhesive jet printing silicon carbide-aluminum composite material and preparation method thereof | |
Tijjani et al. | Manufacturing and mechanical characterization of multiwalled carbon nanotubes/quartz nanocomposite | |
Lephuthing et al. | Exploring the sintering and densification behaviour of multiwalled carbon nanotube reinforced TiO2–MnO2 composites developed by spark plasma sintering | |
EP0672637B1 (en) | Fibre composite material having a ceramic matrix and method of making it | |
Xiao et al. | Oxidation behavior of carbon/carbon-boron nitride composites fabricated by additives and chemical vapor infiltration | |
JP2579854B2 (en) | Inorganic fiber sintered body and method for producing the same | |
Tijjani et al. | Effect of Carbon nanotubes addition on the foundry physical properties of Silica refractory nanocomposite: PART A | |
JP2792595B2 (en) | Inorganic fiber sintered body and method for producing the same |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 12721420 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 12721420 Country of ref document: EP Kind code of ref document: A1 |