Background of the Invention
1. Field of the Invention
[0001] This invention relates to metal fiber structures and more particularly to molded
metal fiber structures.
2. Description of the Prior Art
[0002] Abradable seals made from metal fibers have been used to seal various areas in rotary
compressors and in turbine engines and their compressor sections, including the space
between the turbine blade tips and the engine housing and the space between the turbine
shaft and the turbine vanes.
[0003] These seals must provide sufficient abradability, gas flow blockage and erosion resistance.
Increasing density enhances erosion resistance and gas flow blockage, but it adversely
affects abradability.
[0004] The prior art seals are fabricated by working with a flat brittle porous sheet of
sintered metal fibers. The sheet is cut to size and a reinforcing backing is welded
to it or it is brazed into a ring. An undesirable "butt joint" results in the ring
seal due to the welding or brazing operations. In these prior art seals there is a
random orientation of the fibers in the porous sheet which cannot be changed once
the sheet is formed. Also, the density throughout the sheet and hence throughout the
resulting seals is substantially uniform.
Summary of the Invention
[0005] According to the present invention the fibers are charged directly into a pre-shaped
mold of a desired configuration. The fibers are then compressed and heat treated while
still in the mold.
[0006] The compression of the fibers in the mold also produces a gradation in the density
along the direction of compression. The density is greatest near the compressing member.
Increased density portion of the seal is desirable for providing more effective fluid
blockage while decreased density is desirable for areas in which enhanced abradability
is desired without compromising gas flow blockage. By combining a plurality of green
unsintered compressed elements at different points in the mold, desired density areas
different from other areas may be produced.
[0007] The fiber metal structures produced according to the present invention have no seams,
require no brazing of sheet ends, and are easier to make than prior art structures.
[0008] The ability to heat treat the seals or other fiber metal structures while they are
still in a mold eliminates many handling steps and also permits the use of weights
on the mold to control density and to prevent expansion during heating operations.
[0009] The prior art seals, since they are manufactured in sheet form, are characterized
by two "strength directions": (i) the tensile strength measured in any direction within
and parallel to the plane of the sheet; and (ii) the tensile strength perpendicular
to the plane of the sheet.
[0010] The seals of the present invention are manufactured in annular configuration rather
than in sheet form. The resultant tube-like seals may have any particular annular
configuration including but not limited to a hollow cylinder, a hollow conic section,
or a toroidal section. These seals can be characterized by three "strength directions";
radial, axial, and circumferential. Thus, one of the great advantages of this invention
is the ability to preselect the tensile strength in the axial, circumferential, and
radial directions and make them different or the same, as desired.
Description of the Drawings
[0011]
FIG. 1 is a perspective view of a compression fixture according to the present invention.
FIG. 2 is a schematic depiction of a fiber metal seal made with the fixture of FIG.
1.
FIG. 3 is a schematic depiction in cross-section of a compression fixture according
to the present invention with the compression ring inserted in the fixture for making
a seal such as shown in FIG. 2.
FIG. 4 is a photomicrograph at 100 X magnification of a cross-section of a conventional
seal.
FIG. 5 is a photomicrograph at 100 X magnification of a cross-section of a seal according
to the present invention.
FIG. 6 is a photomicrograph at 100 X magnification of a cross-section of a seal according
to the present invention, the section taken through the part of the seal which in
manufacture was near the compression ring.
FIG. 7 is a photomicrograph at 100 X magnification of the middle of the seal of FIG.
6.
FIGS. 8, 9 and 10 depict solids of revolution according to the present invention.
Description of Preferred Embodiments
[0012] As shown in FIG. 1 one embodiment of a compression fixture 10 according to the present
invention has the baseplate 12, the inner cylinder 14, the outer cylinder 16, and
the compression ring 18. All of these parts are precisely sized so that the compressing
ring 18 will fit into the cavity 17 between the two cylinders 14, 16 which are secured
to the baseplate 12. FIG. 3 shows the portion that is cut out of the outer cylinder
16 to accommodate a solid backing ring 22 to which the seal to be produced can be
attached or bonded during processing.
[0013] Metal fibers 21 are introduced into the cavity 17 between the cylinders 14 and 16.
The compression ring 18 is then pressed down on the fibers 21 forcing them further
into the cavity 17 and into the area encircled by the ring 22. A fiber mass or seal
of a desired density can be produced by introducing a known weight of fiber into the
cavity 17, measuring its height, calculating the height of the mass at the desired
density, and compressing the mass to that height.
[0014] The metal fibers 21 used for the embodiment shown in FIGS. 1, 2, and 3 are of random
irregular geometry with a relatively high aspect ratio of about 75 ("aspect ratio"
means ratio of fiber length to fiber diameter). The normal bulk density of a mass
of such fibers is about 10% (or a porosity of 90%), which is too low for the gas flow
blockage and erosion resistance required of an abradable seal. By densifying the mass
or body of fibers in a compression fixture such as fixture 10, the required density
results. "Density" is expressed here in percentage and means the ratio of material
in a given volume compared to 100% solid material in the same volume.
[0015] In order to maximize gas flow blockage the fibers 21 are compressed in the direction
of the gas flow to be encountered by the seal. The seal 20, in FIG. 2, has had its
fibers in the mass densified by a compression ring moving in the same direction as
the indicated gas flow direction. The random irregular fibers used to form the seal
20 tend to accumulate in a random spatial orientation in planes parallel to the plane
of deposition.
[0016] The axial compression according to the present invention causes the fibers to be
re-oriented toward planes perpendicular to the direction of compression. This re-orientation,
although difficult to quantify, is readily apparent upon a visual examination of a
compressed product and is shown clearly in the photomicrograph of FIG. 5. A section
cut from a prior art seal ring is depicted in the photomicrograph shown in FIG. 4
wherein the backing metal portion of the ring is shown on the left-hand side of FIG.
4 in the vertical direction and the airflow through the seal ring is depicted by the
arrow on the right-hand side indicating that the airflow through the seal is also
in the vertical direction. As can be seen, the fibers are generally randomly oriented
with more of the fibers in the vertical direction which was the direction of formation
of the prior art sheet prior to forming the seal ring. A section cut from one of the
embodiments of this invention is depicted in the photomicrograph of FIG. 5 wherein
the backing ring is shown in a vertical position on the left-hand side of the figure
and the airflow is depicted by the arrow on the right-hand side of the figure. The
fibers in this embodiment are generally oriented perpendicular to the backing ring
and thus perpendicular to the airflow. The fibers were compressed perpendicular to
the base as well as perpendicular to the airflow direction as shown in FIG. 5. In
other words, the compression is parallel to the airflow and perpendicular to the backing
ring, thus providing flow impedance to the airflow through the seal and thereby making
the turbine more efficient.
[0017] The orientation of the fibers results in enhanced abradability as compared to conventional
seals. Abradability can be evaluated by simulating the conditions under which rotating
parts "rub" into the abradable seal. An explanation of how such tests are conducted
is given in Proceedings of the ASME, International Gas Turbine Conference, 1984, Paper
No. 84-GT-67. Table I lists rub test results for one "conventional" fiber metal seal
and two "invention" fiber metal seals.

It is seen that at comparable densities, the "invention" seal rubbed with only about
3% (5.6/196.6) of the unit rub energy of the conventional seal. At a density of 22.8%,
the rub energy of the "invention" seal is still well below that of the conventional
seal. Equally important, the wear ratios of the "invention" seals are less than that
of the "conventional" seamed seal.
[0018] Fibers can be introduced into the cavity 17 in a variety of ways including hand sifting,
hand sifting through a hand-held sieve, and hand sifting through a hand-held sieve
held over a funnel which is inserted into the cavity.
[0019] Surprisingly, axial compression of the fiber mass in the cavity 17 has produced a
remarkable density gradient effect in the final product which is not present in prior
art structures made from slurry-produced sheets of fiber metal. The density of the
compressed fiber mass is greatest near the area which is contacted by the compression
ring (the "top"). The density of the mid-portions is less than that of the top portion
and the density of the portions which were located near the base plate (the "bottom")
is greater than the density of the mid-portions yet slightly less than the top portions'
densities.
[0020] The density gradient effect can be modified by varying compression parameters and
modes of fiber introduction into the cavity. A variety of techniques can be used to
deposit fibers into the fixture cavity. For example all of the fibers can be introduced
into the cavity prior to any compression or portions of the total fiber mass can be
introduced and compressed in separate steps to form a structure with varying or alternating
density portions.
[0021] The photomicrographs of FIGS. 6 and 7 illustrate visually the density gradient across
a seal made with a fixture such as that of FIG. 1. FIGS. 6 and 7 show portions of
a molded seamless seal according to the present invention. The densities of the two
portions vary. Relative quantification of the densities was achieved by using the
reciprocal of the exposure time for each photomicrograph with illumination held constant
to establish a relative areal concentration of fibers in each portion of the seal.
The cross-sectional portion of the embodiment depicted in FIGS. 6 and 7 is arranged
in such a manner that the microstructure shown in FIG. 6 has an airflow in the vertical
direction through the material and the direction of the compression of the fibers
was also in the vertical direction. It can be seen in the photograph that the preferred
orientation of the fibers is in a horizontal arrangement perpendicular to both the
airflow and the direction of compression. The midsection or middle zone of the seal
material represented by the photomicrograph of FIG. 7 shows the fibers having less
density than the fibers in FIG. 6 while the airflow and direction of compression are
the same as shown in FIG. 6. It is also obvious from the photograph that besides the
density being less than is shown in FIG. 6 the fibers are more in a random array than
the more horizontally oriented fibers in FIG. 6.
[0022] The combination of a fiber-charged fixture with a compressing load such as is shown
in FIG.3 can be introduced into a heat treatment unit, e.g., a sintering furnace.
The load on the fiber mass restricts expansion during heating assuring that the resultant
structure will have the desired dimensions and eliminating the need for time-consuming
sizing and trimming. This method also obviates the need for multiple heat treatment
steps because the fibers are joined together by sintering in a mass of the size and
shape of the final product, and the mass is joined to its backing ring by brazing
simultaneously or in the same operation; thus requiring only one heat-treat operation.
Also the hot deformation step required to permit work with low ductility materials
such as materials containing nickel aluminides is no longer necessary with the present
invention. Furthermore, intimate contact in the fiber mass in the fixture cavity is
achieved
before sintering making it possible to more closely meet prescribed size tolerances. Finally,
products made according to the present invention have no seam. Prior art products
with seam are undesirable because such seams present a path for low gas flow resistance.
[0023] The effectiveness of a gas seal is, of course, related to its ability to resist the
flow of gas internally. The greater its gas flow resistance, the more gas is forced
to impinge upon the working surfaces of the blades to produce useful work, and therefore
the greater the engine efficiency. "Conventional" seamed seals and "invention" seamless
seals were evaluated at nominal 21% densities at a flow velocity of 430 ft./hr. From
pressure drop measurements and the airflow settings, an Air Permeability Coefficient
("APC") can be calculated. The test results are reported in Table II.

The "conventional" seamed seals were tested (a) as fabricated and (b) treated with
cement to prevent flow of air through the joint. It is seen that at gas flows of 430
ft./hr., the amount of air flowing through a given frontal area of seal material for
a given pressure drop and thickness, was less than 50% of the "conventional" seal
and only about 61% of the APC for the conventional seamed seal in which the seam had
been treated with cement to block flow through it.
[0024] A porous metal fiber structure exhibits an anisotropic character for gas permeability.
Permeability parallel to the felting plane ("felting plane" is the plane of the porous
membrane on which the sheet of fibers is deposited) of conventionally produced fiber
metal structures can be up to twice as great as permeability perpendicular to this
plane. The methods of and means of the present invention effectively inverts this
relationship because the felting plane of a product produced according to the present
invention is perpendicular to the direction of the fluid that will flow through the
structure. The fiber orientation pattern of structures and seals according to this
invention enhances abradability, reduces axial fluid leakage through the seal, increases
erosion resistance and improved strength in the radial direction.
[0025] The porous metal fiber body described herein has a structure made up of the plurality
of discrete metal fibers, each of these metal fibers having a generally uniform diameter
or cross section along the length of the fiber with the fibers having a minimum diameter
of about 3 microns and up to a maximum diameter of about 145 microns. The maximum
fiber diameter in any one body is no more than about four times the minimum fiber
diameter of a fiber found in the same body. Included within the scope of this invention
is the requirement that the fibers within a body have a minimum length of at least
about 30 microns and a maximum length no more than about 7,620 microns and the individual
fibers have a length to diameter ratio ranging from at least about 10 to 1, to no
more than about 180 to 1. The adjacent fibers within the body that are touching exhibit
interfiber diffusion bonding such that a meniscus between the touching adjacent fibers
is formed and that the total fiber bonding produces a lattice network of autogenously
bonding or diffusion bonded fibers, one to the other. It has been found that the maximum
density of this fiber network is no more than about 70% and no less than about 12%.
The fiber network can have a greater density such that the maximum density of the
network is no more than about 50% greater than the minimum density of the network
and that the difference between the minimum and maximum densities should be at least
about 25%. It has been found that within the fiber network the highest density range
has a tensile strength profile such that the lowest tensile strength, by direction,
ranges from about 50 to 65% of the maximum tensile strength and that the intermediate
tensile strength ranges from about 65 to 85% of the maximum tensile strength. Further,
it has been found that the portion of the lowest density area of the network has a
three dimensional tensile strength profile such that all three directions have approximately
equal tensile strengths.
[0026] Although the description above has been directed to a tube-like object in the form
of a right circular cylinder, it should be evident that the instant invention is not
limited thereto. For example, tube-like objects, such as shown in FIGS. 8-10, can
readily be produced, having the controlled fiber orientation of this invention.
1. A process for making a tube-like abradable metal fiber seal exhibiting superior
abradability and gas flow blockage, comprising:
felting discrete metal fibers into a tube-like recess in a fixture, the felting done
in planes perpendicular to the longitudinal axis of the recess, the fixture having
only one open end with the recess formed of that open end, said fibers having a diameter
of 3 to 145 microns, a length of 30 to 7,620 microns, and a length to diameter range
of 10 to 180,
compressing the fibers in the recess by applying pressure in a direction coincident
with the recess's longitudinal axis to compress the fibers into a lattice network
having a density 12 to 70%,
heating the fibers to produce interdiffusion bonding between a majority of adjacent
fibers.
2. The process of Claim 1, in which said tube-like recess is in the form of a right
circular cylinder.
3. The process of Claim 2, in which a predetermined height of the outer circumferential
surface of said recess is fitted with tubular backing ring, such that said backing
ring may bond to the metal fiber seal during the heating of the fibers.
4. A tube-like, metal fiber abradable seal exhibiting superior abradability and gas
flow blockage, characterized by said fibers being oriented substantially perpendicular
to the longitudinal axis of the seal, said seal having been produced by the process
of Claim 1.
5. The seal of Claim 4, produced by the process of Claim 2.
6. The seal of Claim 5, produced by the process of Claim 3.