[0001] The present invention relates to a vane for a rotary type compressor, and more particularly
relates to such a compressor vane, made of a metallic material reinforced with short
fiber material, which is improved so as to be outstanding in its strength and durability.
[0002] As is per se known, a rotary type compressor that includes vanes typically is basically
composed of a hollow right cylindrical member that defines a compressor chamber with
its inner right cylindrical surface (which often, typically, may not be circular cylindrical),
a rotor member that rotates within said cylindrical compressor chamber about an axis
parallel to the generators thereof (said axis being located either at the axial center
of said compressor chamber, or not, depending upon constructional layout) and is formed
with a plurality of generally radially extending vane receiving slots, and a plurality
of vanes, each one of which is slidingly fitted in a one of said vane receiving slots
with its outer edge extending generally parallel to the generators of the inner cylindrical
surface defining the compressor chamber and in contact therewith. As the rotor member
is rotated within the compressor chamber, the vanes of course rotate along therewith,
and their outer edges, which stay in contact with said inner cylindrical surface defining
the compressor chamber by said vanes sliding to and fro along the rotor member vane
receiving slots in which they are fitted, define in cooperation with said cylindrical
surface and said rotor member a plurality of pumping chambers which expand and contract
in volume as the rotor member and the vanes thus rotate. In detail, considering a
one of said pumping chambers, it expands in volume as it passes a portion of said
cylindrical surface in which there is formed an intake port, and at this time said
pumping chamber sucks a fluid which is to be pumped and compressed into itself through
said intake port. Subsequently said one of said pumping chambers passes away from
said portion of said cylindrical surface with said intake port and becomes isolated,
and next said one of said pumping chambers contracts in volume and thereby compresses
the quantity of said fluid entrapped therein. Finally, said one of said pumping chambers
passes to a portion of said cylindrical surface in which there is formed an exhaust
port, and at this time said pumping chamber squirts the compressed fluid within itself
through said exhaust port. Thereby, as a whole, fluid is sucked into the compressor
through said intake port, is compressed, and is then expelled in compressed form through
said exhaust port; and thereby compression action for said fluid is maintained.
[0003] During the operation of such a vane type compressor, each of the vanes rotates at
high speed with its outer edge portion in sliding contact with the compressor chamber
inner cylindrical surface, which creates severe conditions of sliding friction; and
at the same time said vane slides to and fro in the generally radially direction along
the vane receiving slot in the rotor member in which it is fitted, and this sliding
contact motion similarly creates severe conditions of sliding friction. This means
that both the outer edges of the vanes and also the side surfaces thereof are all
subjected to high friction operational regimes, and are liable to severe wear. For
these reasons, conventional design practice has aimed at making such vanes light in
weight, and, with the objective of ensuring the adequacy of the anti seizure characteristics,
the anti scuffing characteristics, and the anti wear characteristics of the vanes,
they have been conventionally manufactured from a high silicon type aluminum alloy
such as the type AA standard A390. However, such aluminum alloy type vanes have been
decidedly deficient with regard to anti wear characteristics, anti scuffing characteristics,
and anti seizure characteristics, especially in view of the constantly more severe
demands in terms of operational conditions and performance and also operating life
made upon such a vane type compressor, and accordingly other solutions have been desired.
[0004] In order to meet this problem, in Japanese Patent Laying Open Publications Serial
Nos. 58-91141 (1983) and 59-3449b (1984), neither of which is it intended hereby to
admit as prior art to the present patent application except to the extent in any case
required by applicable law, there was described a fiber reinforced metal compressor
vane, in which the main or matrix metal was an alloy of aluminum and the reinforcing
material was short carbon fiber material, and the concepts were further discussed
that in such a compressor vane (a) the short carbon reinforcing fibers should be oriented
substantially randomly in three dimensions; and (b) said short carbon reinforcing
fibers should all be oriented substantially in the same direction, said direction
being substantially perpendicular to the surfaces of the vane.
[0005] However, in the course of enhancing the performance of such compressors and making
such compressors more and more compact, in the case of utilizing such high silicon
alloy compressor vanes, or such fiber reinforced metal compressor vanes, the performance
has been discovered to be currently inadequate with regard to anti wear characteristics
and anti scuffing characteristics. Moreover, in making such vane type compressors
more and more compact, the requirement has arisen for the vanes to be made extremely
thin, and a further problem has developed with regard to the bending strength of the
vanes. In detail, the outer edges and the inner edges of the vanes act as fulcrums
with regard to stresses imposed on the vanes, and it is accordingly necessary that
said outer edges and said inner edges of the vanes should be not only superior with
regard to anti wear characteristics and anti scuffing characteristics, but also should
be superior with regard to bending strength, in order to be able to withstand the
bending stress imposed by the rotor member and so on. These demands upon the characteristics
of such vanes for vane type compressors have become exceedingly severe, especially
when considered together as a whole rather than each in isolation.
SUMMARY OF THE INVENTION
[0006] The inventors of the present invention have considered the various problems detailed
above in the case of a vane for a vane type compressor, from the point of view of
the desirability of increasing the operational performance of the compressor while
decreasing its size and making it more compact and light in weight.
[0007] Accordingly, it is the primary object of the present invention to provide a fiber
reinforced metal compressor vane, which avoids the problems detailed above.
[0008] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with superior frictional wear resistance characteristics.
[0009] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior frictional wear resistance
characteristics, in particular on its outer edge portion.
[0010] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior frictional wear resistance
characteristics in particular on its side surface portions, and especially upon the
parts of said side surface portions thereof which slide in vane receiving grooves
formed in the rotor member of the compressor.
[0011] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with superior scuffing resistance characteristics.
[0012] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior scuffing resistance characteristics,
in particular on its outer edge portion. ,
[0013] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior scuffing resistance characteristics
in particular on its side surface portions, and especially upon the parts of said
side surface portions thereof which slide in vane receiving grooves formed in the
rotor member of the compressor.
[0014] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with superior anti seizure characteristics.
[0015] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior anti seizure characteristics,
in particular on its outer edge portion.
[0016] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is endowed with such superior anti seizure characteristics
in particular on its side surface portions, especially upon the parts of said side
surface portions thereof which slide in vane receiving grooves formed in the rotor
member of the compressor.
[0017] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which has particularly good bending strength.
[0018] It is a further object of the present invention to provide such a fiber reinforced
metal compressor vane, which has such particularly good bending strength especially
at its portions which are subjected with high bending stress during use.
[0019] It is a yet further object of the present invention to provide such a fiber reinforced
metal compressor vane, which allows for a compressor incorporating it to have good
durability.
[0020] It is a yet further object of the present invention to provide such a fiber reinforced
metal compressor vane, which allows the compactness of a compressor incorporating
it to be enhanced.
[0021] It is a yet further object of the present invention to provide such a fiber reinforced
metal compressor vane, which allows the pumping capacity of a compressor incorporating
it to be enhanced, without particularly requiring said compressor to be increased
in size or weight.
[0022] It is a yet further object of the present invention to provide such a fiber reinforced
metal compressor vane, which is itself light in weight.
[0023] According to the most general aspect of the present invention, these and other objects
are attained by, for a vane type compressor comprising a rotor rotatably mounted about
a longitudinal axis within a hollow cylindrical housing member, and formed with a
generally radially extending slot: a compressor vane, formed generally in a slab shape,
having two opposite substantially mutually parallel side surfaces for sliding against
the surfaces of said slot in said rotor, and further having an edge portion, substantially
perpendicular to its said side surfaces, for sliding against the inner surface of
said hollow cylindrical compressor housing member; said vane being manufactured from
a matrix of metal reinforced with short fiber material, with the orientation of the
fibers of said reinforcing short fiber material being generally two dimensionally
random and isotropic in planes perpendicular both to said opposite side surfaces thereof
and to said edge portion thereof; or, according to an alternative form of expression,
by, for a vane type compressor comprising a rotor rotatably mounted about a longitudinal
axis within a hollow cylindrical housing member, and formed with a generally radially
extending slot: a compressor vane, formed generally in a rectangular parallelopipedal
slab shape, for being inserted in said generally radially extending slot of said rotor,
and having two opposite substantially mutually parallel side surfaces for, when said
vane is thus fitted to said rotor of said compressor, extending in planes substantially
radial and substantially longitudinal to said rotor and sliding against the surfaces
of said slot in said rotor, and further having a side edge portion, substantially
perpendicular to its said side surfaces and joining them, for, when said vane is thus
fitted to said rotor of said compressor, extending in a plane substantially circumferential
and substantially longitudinal of said rotor and for sliding against the inner surface
of said hollow cylindrical compressor housing member; said vane being manufactured
from a matrix of metal reinforced with short fiber material, with the orientation
of the fibers of said reinforcing short fiber material being generally two dimensionally
random and isotropic in planes perpendicular both to said opposite side surfaces thereof
and to said edge portion thereof and substantially perpendicular to the longitudinal
direction of said rotor, when said vane is fitted to said rotor of said compressor.
[0024] According to such a fiber reinforced metal compressor vane as specified above, since
the orientation of the fibers of said reinforcing short fiber material, when said
vane is fitted to said rotor of said compressor, is generally two dimensionally random
and isotropic in planes perpendicular both to said opposite side surfaces thereof
and also to said edge portion thereof and thus substantially perpendicular to the
longitudinal direction of said rotor, thereby these reinforcing short fibers, where
they meet said opposite side surfaces and said edge portion of said rotor, are overall
on average angled at the maximum amount with respect to said surfaces of said vane,
which are the surfaces of said vane which particularly undergo sliding friction during
use of the compressor. By "overall" it is meant that other orientations for the reinforcing
short fibers might increase the average angle which said reinforcing short fibers
might make at one of these surfaces, but only at the expense of the average angle
which said reinforcing short fibers might make at the other of said surfaces; the
specified orientation for the reinforcing short fiber material is the one which maximizes
the minimum average angle which said reinforcing short fibers make at both of these
surfaces. Consequently, the anti wear characteristics and the anti scuffing and anti
seizure characteristics of this vane and the compressor incorporating it are significantly
enhanced. Further, since the reinforcing short fibers are generally oriented on planes
which are perpendicular to the direction (taken as a vector) of the bending stress
to which the vane is subjected by the rotor during use of the compressor, thereby
there is made possible a significant improvement in the bending strength of the vane,
which further increases its durability.
[0025] Thereby, as a whole, the durability of a compressor including this vane is notably
enhanced, and, further, since it becomes possible to reduce the thickness of the vane
in accordance with the improved characteristics thereof, thereby the swept volume
of the compression or pumping chambers of the compressor can be significantly increased,
without making the compressor as a whole more bulky or heavier. As a result, the pumping
capacity of the compressor can be desirably enhanced to a significant extent.
[0026] According to a particular specialization of the present invention, the above and
other objects may more particularly be accomplished by a fiber reinforced metal compressor
vane of either of the types specified above, wherein said matrix metal is magnesium
alloy, or alternatively is aluminum alloy. This facilitates making the vanes as light
as possible. Further, the reinforcing fiber material may be alumina short fiber material,
or alumina-silica short fiber material (possibly including a substantial crystalline
content, which may be mullite crystalline content), or silicon carbide whisker material,
or silicon nitride whisker material. And the volume proportion of said reinforcing
fiber material may be from about 5% to about 50%.
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] The present invention will now be described with respect to the preferred embodiments
thereof, and with reference to the illustrative drawings appended hereto, which however
are provided for the purposes of explanation and exemplification only, and are not
intended to be limitative of the scope of the present invention in any way, since
this scope is to be delimited solely by the accompanying claims. With relation to
the figures, spatial terms are to be understood as referring only to the orientation
on the drawing paper of the illustrations of the relevant elements, unless otherwise
specified; like reference numerals, unless otherwise so specified, denote the same
elements and so on in the various figures relating to one preferred embodiment, and
like elements and so on in figures relating to different preferred embodiments; and:
Fig. 1 is a schematic longitudinal skeleton view of a vane type compressor suitable
for incorporating any one of the preferred embodiments of the fiber reinforced metal
compressor vane of the present invention;
Fig. 2 is a schematic enlarged perspective view showing a fiber reinforced metal compressor
vane for said Fig. 1 compressor, said compressor vane being according to any one of
the preferred embodiments of the present invention;
Fig. 3 is a perspective view showing a preform made of short reinforcing fiber material,
suitable for being used for making a fiber reinforced metal compressor vane according
to the present invention, with the orientation of the short fibers of which said fiber
preform is composed being generally two dimensionally isotropically random in planes
perpendicular to the axis thereof designated as "Y";
Fig. 4 is similar to Fig. 3, being a perspective view showing a preform made of short
reinforcing fiber material, suitable for being used for making a first comparison
fiber reinforced metal compressor vane not according to the present invention, with
the orientation of the short fibers of which said fiber preform is composed being
generally two dimensionally isotropically random in planes perpendicular to the axis
thereof designated as "X";
Fig. 5 is similar to Figs. 3 and 4, being a perspective view showing a preform made
of short reinforcing fiber material, suitable for being used for making a second comparison
fiber reinforced metal compressor vane also not according to the present invention,
with the orientation of the short fibers of which said fiber preform is composed being
generally two dimensionally isotropically random in planes perpendicular to the axis
thereof designated as "Z"; and:
Fig. 6 is similar to Figs. 3 through 5, being a perspective view showing a preform
made of short reinforcing fiber material, suitable for being used for making a third
comparison fiber reinforced metal compressor vane also not according to the present
invention, with the orientation of the short fibers of which said fiber preform is
composed being generally isotropically random in three dimensions.
DESCRIPTION OF THE PREFERRED
EMBODIMENTS
[0028] The present invention will now be described with reference to the preferred embodiments
thereof, and with reference to the figures.
General Construction of a Vane Type Compressor
[0029] In Fig. 1, there is shown a schematic longitudinal skeleton view of a vane type compressor,
which is of the type discussed earlier in this specification, and which is suitable
for incorporating any one of the preferred embodiments of the fiber reinforced metal
compressor vane of the present invention which will be described hereinafter; and
Fig. 2 shows a vane incorporated therein in enlarged perspective view. Therefore,
before description of any of the preferred embodiment compressor vanes, a general
description of the construction and the functioning of such a vane type compressor
will be given, in order to place into context the requirements upon the fiber reinforced
metal compressor vane of the present invention with regard to bending strength, wear
resistance, scuffing resistance, and the like.
[0030] Referring to Fig. 1, the reference numeral 2 denotes a hollow cylinder member of
the compressor, and this hollow cylinder member 2 is received in the central cavity
of an outer casing member 4. This hollow cylinder member 2 is formed as a right cylindrical
body which has a right cylindrical inner surface 8 which defines within it a cylinder
chamber space. This inner surface 8, which extends in a direction perpendicular to
the drawing paper in Fig. 1, however is not a circular cylinder, but rather its cross
sectional shape is generally formed as approximately elliptical. The central axis
of symmetry 6 of the inner surface 8 of the hollow cylinder member 2 is denoted as
6 in the drawing, and this axis of symmetry 6 also extends in a direction perpendicular
to the drawing paper in Fig. 1, since the entire construction is right cylindrical.
[0031] Through the inner surface 8 of the hollow cylinder member 2, at diametrically opposite
sides thereof with respect to the axis of symmetry 6 of said cylindrical inner surface
8, there open a pair of inlet ports 10 and 12. The inlet port 10 communicates to an
inlet plenum 14, and similarly the other inlet port 12 communicates to another inlet
plenum 16. Although such arrangements are not particularly shown in the figure, the
two inlet plenums 14 and 16 may typically be communicated together and then may be
connected to an inlet side of the compressor as a whole, for sucking fluid to be compressed
from a source thereof. Similarly, through said inner surface 8 of the hollow cylinder
member 2, at diametrically opposite sides thereof with respect to said axis of symmetry
6 of said cylindrical inner surface 8, there open a pair of outlet ports 18 and 20.
The outlet port 18 communicates to an outlet plenum 22, and similarly the other outlet
port 20 communicates to another outlet plenum 24. Although such arrangements are not
particularly shown in the figure, the two outlet plenums 22 and 24 may typically be
communicated together and then may be connected to an outlet side of the compressor
as a whole, for expelling fluid which has been compressed towards a device for receipt
thereof. In fact, a pair of one way valves are provided, one to each of said outlet
ports 18 and 20, for allowing flow of fluid therethrough only in the direction from
the cylinder chamber space defined within the inner surface 8 of the hollow cylinder
member 2 towards the respective outlet plenums 22 and 24, and not in the reverse directions;
however, such arrangements also are not particularly shown in the figure.
[0032] A substantially circular cylindrical rotor member 26 is mounted within said cylinder
chamber space defined in said hollow cylinder member 2, so as to be rotatable about
the axis of symmetry 6 of the inner surface 8 of said hollow cylinder member 2. This.
rotor member 26 is formed with four vane receiving slots designated as 28a through
28d, each of which extends substantially longitudinally along the rotor member 26
and thus in a plane also substantially perpendicular to the drawing paper in Fig.
1 and substantially parallel to the axis of symmetry 6 of the construction although
in fact not actually including said axis of symmetry 6. The planes of the two vane
receiving slots 28a and 28c are parallel to one another and are set at an angle of
90
° with respect to the planes of the other two vane receiving slots 28b and 28d which
also are parallel to one another. Thus, the four vane receiving slots 28a through
28d extend in the longitudinal direction of the rotor member 26 and also generally
in the radial direction of said rotor member 26 although in fact somewhat offset therefrom.
In each of said four vane receiving slots 28a through 28d there is slidably fitted
a corresponding one of four vanes 36a through 36d, each of which is formed as a slab
member, i.e. generally as a rectangular parallelopiped or cuboid whose dimension in
the circumferential direction of the construction is relatively small, whose dimension
in the radial direction of the construction is intermediate, and whose dimension in
the longitudinal direction of the construction is relatively large. The outer edges
of these four vanes 36a through 36d are respectively denoted by the reference symbols
40a through 40d; the trailing sides (with respect to the preferred direction of rotation
of the rotor member 26 and the vanes 36a through 36d as shown by an arrow in Fig.
1) of the four vanes 36a through 36d are respectively denoted by, the reference symbols
42a through 42d; and the leading sides with respect to said preferred direction of
rotation of the four vanes 36a through 36d are respectively denoted by the reference
symbols 44a through 44d. This nomenclature and these relative dimensions are best
appreciated by consideration of Fig. 2, which shows such a vane, particularly one
according to the present invention as will be described later, in enlarged perspective
view.
Operation of this Vane type Compressor
[0033] Thus, as the rotor member 26 rotates, it naturally carries the four vanes 36a through
36d around with it, since they are slidably fitted into the four vane receiving slots
28a through 28d formed in said rotor member 26. The action of centrifugal force therefore
keeps said four vanes 36a through 36d biased in the respective radially outward directions,
so that their outer edges 40a through 40d are kept pressed against the inner surface
8 of the hollow cylinder member 2 and form relatively good seals thereagainst, while
said one of said four vanes 36a through 36d slides to and fro in its one of the four
vane receiving slots 28a through 28d, its sides 42 and 44 at this time performing
rubbing action each on its side of said one of said four vane receiving slots 28a
through 28d. Thus, four variable volume pumping chambers 38 are defined around the
rotor member 26 between adjacent pairs of said four vanes 36a through 36d, the rotor
member 26, and said inner surface 8 of said hollow cylinder member 2. To consider
the action in detail, as the rotor member 26 and the four vanes 36a through 36d rotate,
and considering an exemplary one of these variable volume pumping chambers 38: said
variable volume pumping chamber 38 moves around the inner surface 8 of the hollow
cylinder member 2 in the counterclockwise direction as seen in the figure, and first
at the start of its pumping cycle its leading edge portion comes to correspond to
one of the inlet ports 10 and 12 - here let us assume that that one is the inlet port
10 - and thereafter said variable volume pumping chamber 38 expands in volume as it
passes past said inlet port 10, to reach a substantially maximum volume as its trailing
edge portion comes to pass said inlet port 10; thereby a quantity of fluid to be compressed
is sucked into said variable volume pumping chamber 38 through the inlet plenum 14
and said inlet port 10. Next, this variable volume pumping chamber 38 is reduced in
volume, thus compressing the fluid just inducted thereinto, and then the leading edge
portion thereof comes to correspond to one of the outlet ports 18 and 20 - actually
the outlet port 20 in this case - and thereafter said variable volume pumping chamber
38 further reduces in volume as it passes past said outlet port 20. At an appropriate
time point the one way valve not shown in the figure for said outlet port 20 is opened
by an appropriate means therefor, so as to allow the compressed fluid in the variable
volume pumping chamber 38 to be expelled therefrom through said outlet port 20 and
the outlet plenum 24. And the variable volume pumping chamber 38 reaches a substantially
minimum volume as its trailing edge portion comes to pass said outlet port 20. And
then this cycle is repeated.
[0034] Thereby, fluid is sucked in from the inlet plenums 14 and 16, is compressed, and
is expelled at relatively high pressure via the outlet plenums 22 and 24.
[0035] During this action, the four vanes 36a through 36d are subjected to very severe conditions
of frictional wear, both due to the rubbing of their outer edges 40a through 40d against
the inner surface 8 of the hollow cylinder member 2, and also due to the sliding of
their sides 42a through 42d and 44a through 44d against the sides of the four vane
receiving slots 28a through 28d. Such severe frictional wear conditions can cause
scuffing of the relevant surfaces against one another, or, in the worst case, mutual
seizure thereof. And, furthermore, the outer and inner edges of each such vane 36a
through 36d function as fulcrums to receive the bending stress imparted from the outer
edge of the respective one of the four vane receiving slots 28a through 28d, and this
subjects the four vanes 36a through 36d to very severe conditions of bending strain.
Because of these various severe conditions to which the four vanes 36a through 36d
are subjected, the requirements for their endurance have been made more and more demanding,
which has given rise to the particular composition for said four vanes 36a through
36d according to the present invention, now to be explained.
The Vane of the Present Invention
[0036] Fig. 2 is a schematic enlarged perspective view showing a fiber reinforced metal
compressor vane for said Fig. 1 compressor, said compressor vane being according to
any one of the preferred embodiments of the present invention. This vane, denoted
as 36, is manufactured from a composite material which is made up from a matrix of
metal such as for example aluminum alloy or magnesium alloy, reinforced by short fiber
material such as for example alumina-silica fibers or the like, with the particular
feature, according to the concept of the present invention, that the orientation of
the short fibers (denoted by the reference symbol 46) of said reinforcing short fiber
material is such that they are oriented substantially randomly and isotropically in
two dimensions, and substantially lie in planes perpendicular to the axial line 6
of the compressor to which they are to be fitted. In other words, according to the
nomenclature shown in the figure, the outer edge portion of the vane 36 which slides
against the inner surface 8 of the hollow cylinder member 2 is designated as 40 and
the two sides of said vane 36 which slide against the sides of the vane receiving
slot 28 formed in the rotor member 26 for this vane 36 are designated as 42 and 44,
and the axes as shown in the figure are as follows: the X axis is in the direction
perpendicular to said two sides 42 and 44 of said vane 36, i.e. is in the direction
circumferential to the rotor member 26 of the compressor when this vane 36 is fitted
to said compressor; the Y axis is in the direction parallel to said outer edge 40
of said vane 36, i.e. is in the direction longitudinal to the rotor member 26 of the
compressor when this vane 36 is fitted to said compressor; and the Z axis is in the
direction parallel to said two sides 42 and 44 and perpendicular to said outer edge
40 of said vane 36, i.e. is in the direction radial to the rotor member 26 of the
compressor when this vane 36 is fitted to said compressor. And, according to the particular
concept of the present invention, the orientation of the short fibers 46 of the reinforcing
short fiber material is such that they are oriented substantially two dimensionally
randomly and isotropically in planes parallel to the X-Z plane, and however substantially
all extend perpendicular to the Y axis.
[0037] As a result of this orientation of the short fibers 46, the average orientation of
said short fibers 46 where they reach the surface of the vane 36, both at the outer
edge 40 of said vane 36 and at the two side surfaces 42 and 44 of said vane 36, is
maximized: i.e. the average angle at which said short fibers 46 meet said various
surfaces 40, 42, and 44 is maximized. Thereby, the anti wear characteristics of saie-
outer edge 40 and said two side surfaces 42 and 44 of said vane 36 are as a whole
maximized, as are their anti scuffing characteristics and their anti seizure characteristics.
Further, according to this orientation of the short fibers 46 of the fiber reinforcing
material according to the present invention, since said short fibers are substantially
oriented to lie in planes which are extended in the direction of the bending stress
which the vane 36 receives from the rotor member 26, the bending strength characteristics
of this vane 36 are also notably excellent. That is to say, speaking in vector and/or
tensor terms, the twisting stress to which the vane 36 is subjected as the compressor
rotor member 26 rotates can be represented by a vector field whose elements all extend
substantially longitudinally to said rotor member 26, i.e. in the direction of the
Y axis as seen in Fig. 2, and therefore, because the short fibers 46 of the reinforcing
short fiber material all lie so as to extend perpendicular to the Y axis, i.e. all
extend substantially two dimensionally randomly and isotropically in planes parallel
to the X-Z plane, therefore the resistance which they offer to said bending stress
is substantially maximal.
The First Preferred Embodiment, and Comparison Examples
[0038] Now, the first preferred embodiment of the fiber reinforced metal compressor vane
of the present invention will be described in concrete terms, along with comparison
examples, with reference to Figs. 3 through 6.
[0039] First, a quantity of crystalline alumina-silica short fiber material was prepared
in the following manner. The starting material was a quantity of non-crystalline (amorphous)
short fiber material of the type "Kaowool" (this is a trade mark) made by Isolite
Babcock Taika K.K., which had average fiber length of approximately 1 mm and average
fiber diameter of approximately 3 microns, and which was composed of approximately
48% by weight Al
2O
3 and balance substantially 5i0
2. This starting material was then subjected to heat treatment, so that approximately
60% by weight of it was converted to the mullite crystalline form.
[0040] Then, from this crystalline alumina-silica short fiber material, there were prepared,
using colloidal silica as a binder, four different short fiber material preforms,
shown in Figs. 3 through 6 and designated as 50, 52, 54, and 56. Each of these preforms
50, 52, 54, and 56 had approximate dimensions 98 mm x 50 mm x 200 mm, and had fiber
volume proportion of approximately 15%, and the orientations of the short fibers in
each preform were as will now be described, taking the X axis as the 50 mm axis, the
Y axis as the 98 mm axis, and the Z axis as the 200 mm axis (these axes correspond
to the axes of the finished vanes made from these preforms as shown in Fig. 2). The
first such preform 50 had the short fibers 46 of the short fiber reinforcing material
thereof lying generally two dimensionally randomly and isotropically in planes perpendicular
to the Y axis, i.e. extending parallel to the X-Z plane (hereinafter referred to as
orientation A); the second such preform 52 had the short fibers 46 of the short fiber
reinforcing material thereof lying generally two dimensionally randomly and isotropically
in planes perpendicular to the X axis, i.e. extending parallel to the Y-Z plane (hereinafter
referred to as orientation B); the third such preform 54 had the short fibers 46 of
the short fiber reinforcing material thereof lying generally two dimensionally randomly
and isotropically in planes perpendicular to the Z axis, i.e. extending parallel to
the X-Y plane (hereinafter referred to as orientation C); and the fourth such preform
56 had the short fibers 46 of the short fiber reinforcing material thereof lying generally
three dimensionally randomly and completely isotropically in all directions (hereinafter
referred to as orientation D). These preforms were manufactured by per se conventional
methods which will not be particularly discussed herein.
[0041] Next, each of these four preforms 50, 52, 54, and 56 was subjected to a high pressure
casting process, which is not shown in any illustration because it is also per se
conventionally known, as follows. First, the preform was heated up to a temperature
of approximately 600
°C, and then it was placed in a cavity of a casting mold, which itself was maintained
at a temperature of approximately 250°C. Then a quantity of molten aluminum alloy
of type JIS standard ACIA, at a temperature of approximately 710°C, for serving as
a matrix metal, was poured into said mold cavity over and around the preform, to substantially
completely cover it, and then a pressure plunger, itself heated up to a temperature
of approximately 200
°C, was slidingly inserted into said mold cavity so as closely to cooperate therewith,
and was pressed strongly downwards on the surface of the molten aluminum alloy, so
as to pressurize said molten aluminum alloy matrix metal to a pressure of approximately
1000 kg/cm
2. Thereby the molten aluminum alloy matrix metal was pressed into the interstices
of the preform, so as thoroughly to infiltrate between all of the short fibers 46
thereof. And the pressure plunger was maintained in this condition until the aluminum
alloy matrix metal had completely solidified. After said aluminum alloy matrix metal
had thus completely solidified, the resultant cast form was removed from the casting
mold, and was cut down so as to produce a piece of composite material, with the peripheral
portions consisting substantially only of the original aluminum alloy matrix material
without any admixture of reinforcing fibers having been machined away.
[0042] Next, each of these pieces of composite material was processed, first by liquidization
processing for a time period of approximately six hours at a temperature of approximately
500
*C, and then by artificial aging processing for a time period of approximately six
hours at a temperature of approximately 180°C. Then, the resulting material pieces
were machined using per se conventional processes such as shaving and the like, so
as to form a set of four vanes such as shown in Fig. 2, and particularly each with
X, Y, and Z axes as shown in Fig. 2 corresponding to the X, Y, and Z axes respectively
of the preform used as shown in the appropriate one of Figs. 3 through 6. In fact,
as will be easily understood based upon the above explanations and the claims of the
present patent application, the one of these vanes, the reinforcing fibers of which
had orientation A, was an embodiment - the first preferred embodiment - of the present
invention, while on the other hand the other three of these vanes, the reinforcing
fibers of which had orientations B, C, and D respectively, were not embodiments of
the present invention, but on the contrary were comparison samples.
[0043] Each of these vanes 36 in turn was fitted to a compressor of the general type shown
in Fig. 1, and assessment tests were conducted to evaluate the bending strength characteristic,
the wear resistance characteristic, and the scuffing and seizure resistance characteristics
thereof. In detail, the material which was used for the rotor member 26 and for the
hollow cylinder member 2 of the compressor was a high silicon type aluminum alloy
of type JIS A390, and the assessment of the bending strength characteristic of each
of the vanes 36 was performed by rapidly compressing a liquidized coolant substance
and thus conducting liquid compression tests to establish the durability of the vanes
36 under these conditions. Further, the assessment of the wear resistance characteristic
of each of the vanes 36 was performed by operating the compressor for a prescribed
relatively long time period at a prescribed relatively high rotational speed, and
by under these operational conditions checking the wear amount of the outer edge portion
40 of the vane 36 which had slid against the inner cylindrical surface 8 of the cylinder
member 2 of the compressor, thus establishing the wear resistance characteristics
of the vanes 36 under these conditions. Moreover, in these same tests, the sides 42
and 44 of the vanes 36, which had slid against the sides of the vane receiving grooves
28 in which said vanes 36 were fitted, were also checked, thereby not only further
to establish the wear resistance characteristics of the vanes 36 under these conditions,
but also to evaluate the anti scuffing characteristics and the anti seizure characteristics
of said vanes 36.
[0044] The results of these tests are shown in the following Table. In this Table, the columns
"Anti wear characteristic I" and "Anti wear characteristic II" refer to the anti wear
characteristics of the two sides 42 and 44 of the vanes 36, and to the anti wear characteristics
of the edge portions 40 of the vanes 36, respectively; and an "O" indicates that the
corresponding characteristic was at an outstanding and acceptable level, while on
the other hand an "X" indicates that the corresponding characteristic was at an unsatisfactory
level.

[0045] As will be clear from the above Table, the vane whose constituent short reinforcing
fibers had fiber orientation A, i.e. the first preferred embodiment of the fiber reinforced
metal compressor vane of the present invention, was clearly superior in overall characteristics
to the other three vanes, whose constituent short reinforcing fibers had fiber orientations
B, C, and D, i.e. the first through the third comparison example vanes. In other words,
each of these first through third comparison example vanes was deficient in one or
more required performance characteristics, and only the first preferred embodiment
of the fiber reinforced metal compressor vane of the present invention was satisfactory
with regard to all of: bending strength characteristic, anti wear characteristics
of its two sides 42 and 44, and anti wear characteristic of its edge portion 40, as
well as being satisfactory with regard to the scuffing and seizure resistance characteristics
thereof.
The Second preferred Embodiment, and Comparison Examples
[0046] Now, the second preferred embodiment of the fiber reinforced metal compressor vane
of the present invention will be described in concrete terms, along with other comparison
examples. In this second preferred embodiment and its comparison samples, the reinforcing
material used was a quantity of alumina short fiber material of a type made by ICI
K.K., which had average fiber length of approximately 1 mm and average fiber diameter
of approximately 3 microns, and which was composed of approximately 95% by weight
A1
20
3 and balance substantially SiO
2. From this alumina short fiber material there were prepared, substantially as before
except that the fiber volume proportions were now approximately 7% in each case, four
different short fiber material preforms, again as shown in Figs. 3 through 6 with
the same approximate dimensions as before, and with the same orientations of the short
fibers in each preform. Again, these four preforms were manufactured by per se conventional
methods which will not be particularly discussed herein.
[0047] Next, each of these four preforms 50, 52, 54, and 56 was subjected to a high pressure
casting process, substantially as before except that the matrix metal utilized was
a magnesium alloy of type JIS standard MC2. The particular details of this casting
process, and of the subsequent processing steps for the resultant pieces of composite
material, will not be particularly discussed herein, since they are similar or identical
to those practiced for the first preferred embodiment and for its comparison samples,
and in any case are per se conventional. The resulting material pieces were, as before,
machined using per se conventional processes such as shaving and the like, so as to
form four vanes such as shown in Fig. 2, corresponding to the preforms as shown in
the appropriate ones of Figs. 3 through 6. Again, the one of these vanes, the reinforcing
fibers of which had orientation A, was an embodiment - the second preferred embodiment
- of the present invention, while on the other hand the other three of these vanes,
the reinforcing fibers of which had orientations B, C, and D respectively, were not
embodiments of the present invention, but on the contrary were a second set of comparison
samples.
[0048] Each of these vanes 36 in turn was subjected to assessment tests to evaluate the
bending strength characteristic, the wear resistance characteristic, and the scuffing
and seizure resistance characteristics thereof, of the same general nature as in the
case of the first preferred embodiment and of its comparison examples, detailed above.
In this case, the materials which were used for the rotor member 26 and for the hollow
cylinder member 2 of the compressor were, respectively, a high silicon type aluminum
alloy of type JIS A390, and a tempered chromium steel of type JIS standard SCr20.
[0049] The results of these tests will not be detailed at length herein, in view of the
desirability of conciseness of disclosure; suffice it to say as a summary that the
vane whose constituent short reinforcing fibers had fiber orientation A, i.e. the
second preferred embodiment of the. fiber reinforced metal compressor vane of the
present invention, was clearly superior in overall characteristics to the other three
vanes, whose constituent short reinforcing fibers had fiber orientations B, C, and
D, i.e. these first through third comparison example vanes. In other words, each of
these first through third comparison example vanes was deficient in one or more required
performance characteristics, and only the second preferred embodiment of the fiber
reinforced metal compressor vane of the present invention was satisfactory with regard
to all of: bending strength characteristic, anti wear characteristics of its two sides
42 and 44, and anti wear characteristic of its edge portion 40, as well as being satisfactory
with regard to the scuffing and seizure resistance characteristics thereof.
The Third preferred Embodiment, and Comparison Examples
[0050] Now, the third preferred embodiment of the fiber reinforced metal compressor vane
of the present invention will be described in concrete terms, along with other comparison
examples. In this third preferred embodiment and its comparison samples, the reinforcing
material used was a quantity of silicon carbide whisker material of a type made by
Tokai Carbon K.K., which had average fiber length of approximately 100 microns and
average fiber diameter of approximately 0.3 microns. From this silicon carbide whisker
material there were prepared, substantially as before except that the fiber volume
proportions were now approximately 25% in each case, four different whisker material
preforms, again as shown in Figs. 3 through 6 with the same approximate dimensions
as before, and with the same orientations of the whiskers in each preform. Again,
these four preforms were manufactured by per se conventional methods which will not
be particularly discussed herein.
[0051] Next, each of these four preforms 50, 52, 54, and 56 was subjected to a high pressure
casting process, substantially as before except that the matrix metal utilized was
now an aluminum alloy of type JIS standard AC7A. The particular details of this casting
process, and of the subsequent processing steps for the resultant pieces of composite
material, will not be particularly discussed herein, since they are similar or identical
to those practiced for the first and second preferred embodiments and for their comparison
samples, and in any case are per se conventional. The resulting material pieces were,
as before, machined using per se conventional processes such as shaving and the like,
so as to form four vanes such as shown in Fig. 2, corresponding to the preforms as
shown in the appropriate ones of Figs. 3 through 6. Again, the one of these vanes,
the reinforcing fibers of which had orientation A, was an embodiment - the third preferred
embodiment - of the present invention, while on the other hand the other three of
these vanes, the reinforcing fibers of which had orientations B, C, and D respectively,
were not embodiments of the present invention, but on the contrary were a second set
of comparison samples.
[0052] Each of these vanes 36 in turn was subjected to assessment tests to evaluate the
bending strength characteristic, the wear resistance characteristic, and the scuffing
and seizure resistance characteristics thereof, of the same general nature as in the
case of the first preferred embodiment and of its comparison examples, detailed above.
In this case, the material which was used for the rotor member 26 and for the hollow
cylinder member 2 of the compressor was in both cases a high silicon type aluminum
alloy of type JIS A390.
[0053] The results of these tests again will not be detailed at length herein, in view of
the desirability of conciseness of disclosure; suffice it to say again as a summary
that the vane whose constituent short reinforcing fibers had fiber orientation A,
i.e. the third preferred embodiment of the fiber reinforced metal compressor vane
of the present invention, was clearly superior in overall characteristics to the other
three vanes, whose constituent short reinforcing fibers had fiber orientations B,
C, and D, i.e. these first through third comparison example vanes. In other words,
each of these first through third comparison example vanes was deficient in one or
more required performance characteristics, and only the third preferred embodiment
of the fiber reinforced metal compressor vane of the present invention was satisfactory
with regard to all of: bending strength characteristic, anti wear characteristics
of its two sides 42 and 44, and anti wear characteristic of its edge portion 40, as
well as being satisfactory with regard to the scuffing and seizure resistance characteristics
thereof.
The Fourth preferred Embodiment, and Comparison Examples
[0054] t Now, the fourth preferred embodiment of the fiber reinforced metal compressor vane
of the present invention will be described in concrete terms, along with other comparison
examples. In this fourth preferred embodiment and its comparison samples, the reinforcing
material used was a quantity of silicon nitride whisker material of a type made by
Tateho Chemical K.K., which had average fiber length of approximately 100 microns
and average fiber diameter of approximately 1 micron. From this silicon nitride whisker
material there were prepared, substantially as before except that the fiber volume
proportions were now approximately 40% in each case, four different whisker material
preforms, again as shown in Figs. 3 through 6 with the same approximate dimensions
as before, and with the same orientations of the whiskers in each preform. Again,
these four preforms were manufactured by per se conventional methods which will not
be particularly discussed herein.
[0055] Next, each of these four preforms 50, 52, 54, and 56 was subjected to a high pressure
casting process, substantially as before except that the matrix metal utilized was
now an aluminum alloy of type JIS standard AC8A. The particular details of this casting
process, and of the subsequent processing steps for the resultant pieces of composite
material, will not be particularly discussed herein, since they are similar or identical
to those practiced for the first through the third preferred embodiments and for their
comparison samples, and in any case are per se conventional. The resulting material
pieces were, as before, machined using per se conventional processes such as shaving
and the like, so as to form four vanes such as shown in Fig. 2, corresponding to the
preforms as shown in the appropriate ones of Figs. 3 through 6. Again, the one of
these vanes, the reinforcing fibers of which had orientation A, was an embodiment
- the fourth preferred embodiment - of the present invention, while on the other hand
the other three of these vanes, the reinforcing fibers of which had orientations B,
C, and D respectively, were not embodiments of the present invention, but on the contrary
were a second set of comparison samples.
[0056] Each of these vanes 36 in turn was subjected to assessment tests to evaluate the
bending strength characteristic, the wear resistance characteristic, and the scuffing
and seizure resistance characteristics thereof, of the same general nature as in the
case of the first preferred embodiment and of its comparison examples, detailed above.
In this case, again, the material which was used for the rotor member 26 and for the
hollow cylinder member 2 of the compressor was in beth cases a high silicon type aluminum
alloy of type JIS A390.
[0057] The results of these tests again will not be detailed at length herein, in view of
the desirability of conciseness of disclosure; suffice it to say again as a summary
that the vane whose constituent short reinforcing fibers had fiber orientation A,
i.e. the fourth preferred embodiment of the fiber reinforced metal compressor vane
of the present invention, was clearly superior in overall characteristics to the other
three vanes, whose constituent short reinforcing fibers had fiber orientations B,
C, and D, i.e. these first through third comparison example vanes. In other words,
each of these first through third comparison example vanes was deficient in one or
more required performance characteristics, and only the fourth preferred embodiment
of the fiber reinforced metal compressor vane of the present invention was satisfactory
with regard to all of: bending strength characteristic, anti wear characteristics
of its two sides 42 and 44, and anti wear characteristic of its edge portion 40, as
well as being satisfactory with regard to the scuffing and seizure resistance characteristics
thereof.
Conclusion
[0058] This fiber reinforced metal compressor vane according to the present invention, in
its various preferred embodiments, was thus shown to have superior performance characteristics
with regard to bending strength characteristic, anti wear characteristics of its two
sides, anti wear characteristic of its edge portion, and also anti scuffing characteristic
and anti seizure characteristic. It is considered to have been amply demonstrated,
in the light of the various comparison examples, that this overall improvement in
performance characteristics is due to the choice of orientation for the reinforcing
fibers incorporated in the material of said compressor vanes. This is thought to be
because, according to such a fiber reinforced metal compressor vane as specified in
the claims to this patent application, since the orientation of the fibers of said
reinforcing short fiber material, when said vane is fitted to the compressor rotor,
is generally two dimensionally random and isotropic in planes perpendicular both to
the opposite side surfaces thereof and also to the edge portion thereof and thus substantially
perpendicular to the longitudinal direction of said rotor, thereby these reinforcing
short fibers, where they meet said opposite side surfaces and said edge portion of
said rotor, are overall on average angled at the maximum amount with respect to said
surfaces of said vane, which are the surfaces of said vane which particularly undergo
sliding friction during use of the compressor. That is to say, other orientations
for the reinforcing short fibers might increase the average angle which said reinforcing
short fibers might make at one of these surfaces, but only at the expense of the average
angle which said reinforcing short fibers might make at the other of said surfaces;
the specified orientation for the reinforcing short fiber material is the one which
maximizes the minimum average angle which said reinforcing short fibers make at both
of these surfaces. It is considered to be a consequence for the anti wear characteristics
and the anti scuffing and anti seizure characteristics of this vane and the compressor
incorporating it to have been significantly enhanced; and this was verified by the
experimental tests detailed above. Further, since the reinforcing short fibers are
generally oriented on planes which are perpendicular to the direction (taken as a
vector) of the bending stress to which the vane is subjected by the rotor during use
of the compressor, it is considered that this is the reason for the demonstrated significant
improvement in the bending strength of the vane, which as a matter of course further
increases its durability. Thereby, as a whole, the durability of a compressor including
this vane is, notably enhanced, and, since further it becomes possible to reduce the
thickness of the vane in accordance with the improved characteristics thereof, thereby
the swept volume of the compression or pumping chambers of the compressor can be significantly
increased, without making the compressor as a whole more bulky or heavier. As a result,
the pumping capacity of the compressor can be desirably enhanced to a significant
extent.
[0059] Although the present invention has been shown and described in terms of the preferred
embodiments thereof, and with reference to the appended drawings, it should not be
considered as being particularly limited thereby, since the details of any particular
embodiment, or of the drawings, could be varied without, in many cases, departing
from the ambit of the present invention. Accordingly, the scope of the present invention
is to be considered as being delimited, not by any particular perhaps entirely fortuitous
details of the disclosed preferred embodiments, or of the drawings, but solely by
the scope of the accompanying claims, which follow.