U.S. patent number 3,784,320 [Application Number 05/227,809] was granted by the patent office on 1974-01-08 for method and means for retaining ceramic turbine blades.
This patent grant is currently assigned to Motoren-Und Turbinen-Union. Invention is credited to Wilhelm Hoffmuller, Axel Rossmann.
United States Patent |
3,784,320 |
Rossmann , et al. |
January 8, 1974 |
METHOD AND MEANS FOR RETAINING CERAMIC TURBINE BLADES
Abstract
A method and means for retaining ceramic turbine blades in steel
rotors using metallic felt shims interposed between the edges of
the blade root and side walls of a slot formed in the rotor. The
metallic felt shims are formed of very thin metallic fibers
sintered together to form a thin sheet of felt material. This
sintered felt sheet is then compressed beyond its first plastic
limit, at which point it again becomes elastic, exhibiting
favorable elastic properties for absorbing the relatively large
rotative and centrifugal forces between the rotor and blade during
use. Since the force between blade and rotor transfer is almost
exclusively through elastic deformation of the shim means, the
friction coefficients between the shim and rotor or blade structure
need not be precisely controlled. The shim is fixed to the rotor
structure by brazing or the like. The predeformed metal felt
material also acts as a heat insulator to prevent or inhibit the
transfer of high blade temperatures and heat to the rotor.
Inventors: |
Rossmann; Axel (Munich,
DT), Hoffmuller; Wilhelm (Munich, DT) |
Assignee: |
Motoren-Und Turbinen-Union
(Munich, DT)
|
Family
ID: |
5799354 |
Appl.
No.: |
05/227,809 |
Filed: |
February 22, 1972 |
Foreign Application Priority Data
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Feb 20, 1971 [DT] |
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P 21 08 176.5 |
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Current U.S.
Class: |
416/215;
416/241R; 416/241B; 416/219R |
Current CPC
Class: |
F01D
5/3084 (20130101); F01D 5/3092 (20130101); F01D
5/284 (20130101) |
Current International
Class: |
F01D
5/00 (20060101); F01D 5/30 (20060101); F01D
5/28 (20060101); F01d 005/30 () |
Field of
Search: |
;416/241,219-221,215 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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892,785 |
|
Jan 1944 |
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FR |
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1,163,439 |
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Apr 1958 |
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FR |
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664,986 |
|
Jan 1952 |
|
GB |
|
753,229 |
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Jul 1956 |
|
GB |
|
914,548 |
|
Jan 1963 |
|
GB |
|
Primary Examiner: Powell, Jr.; Everette A.
Attorney, Agent or Firm: Paul M. Craig, Jr. et al.
Claims
1. An arrangement for retaining turbine blades, especially ceramic
turbine blades, in a circumferentially extending slot of a
rotatable rotor, especially a steel rotor, comprising: wall means
forming said slot including inclined portions with a surface
component facing inwardly toward the axis of rotation of the rotor,
surface means on said blade arranged in said slot approximately
parallel to said inclined portions at a small spacing from said
inclined portions, and metallic shim means positioned between the
inclined portions and the surface means, said shim means being
constructed of a sintered metal felt material which has been
predeformed beyond a first plastic limit so that it exhibits highly
elastic properties for elastically absorbing the large centrifugal
forces between the rotor and blade during use whereby the relative
movement of the blade and rotor is primarily a function of the
elasticity of the shim, said shim means also forming a thermal
insulation between the rotor and the blade.
2. An arrangement according to claim 1, wherein said shim means is
fixedly attached to one of said inclined portions and said surface
means.
3. An arrangement according to claim 1, wherein said shim means is
fixedly attached to said inclined portions by brazing.
4. An arrangement according to claim 2, wherein said shim means is
approximately one millimeter thick after predeformation and without
any compressive loads.
5. An arrangement according to claim 2, wherein said shim means is
composed of metal fibers approximately 6 to 15 .mu.m in diameter
which are sintered by the application of high heat, pressure and
reduced atmosphere to form a metal felt structure which is then
predeformed by compression.
6. An arrangement according to claim 5, wherein said metal fibers
consist of 1.5 percent Co, 22 percent Cr. 9 percent Mo, 0.6 percent
W, 18 percent Fe, 0.10 percent C, 1.0 percent Si, 1.0 percent Mn,
balance Ni.
7. An arrangement according to claim 2, wherein further shim means
of similar material are provided between the radially innermost end
of the blade and the bottom of the slot.
8. An arrangement according to claim 1, wherein said slot and the
radially inner end of said blade are of corresponding triangular
cross-section shapes.
9. A method for retaining turbine blades, especially ceramic
turbine blades, in a circumferentially extending slot of a
rotatable rotor, especially a steel rotor, comprising: forming the
slot and the surface of the blade so as to have respective parallel
surfaces facing one another with the slot surface having a surface
component facing relatively inwardly toward the axis of rotation of
the rotor, constructing shim means of sintered metal felt,
predeforming the shim means beyond a first plastic limit so that
the shim means exhibits elastic properties and high strength, and
placing the predeformed shim means between the respective parallel
surfaces of said slot and blade whereby the shim means effectively
elastically absorbs the transfer of centrifugal forces between said
rotor and blade during use.
10. A method according to claim 9, wherein the step of predeforming
the shim means includes compressing the shim means in a press.
11. A method according to claim 9, wherein the step of predeforming
the shim means includes compressing the shim means by placing it
into a rotor and blade assembly and rotating said rotor to cause
relative movement of said rotor and blade to compress the shim
means.
12. A method according to claim 9, further comprising the step of
fixing said shim means to said rotor.
13. A method according to claim 9, further comprising the step of
positioning a predeformed shim means between the radially innermost
end of the blade and the bottom of the slot for supporting the
blade at rest.
14. A method according to claim 9, wherein said shim means is
composed of metal fibers approximately 6 to 15 .mu.m in diameter,
and wherein said step of constructing the shim means includes
sintering these metal fibers by the application of high heat,
pressure and reduced atmosphere which effectively connects the
fibers at their contact points.
15. A method according to claim 14, wherein said metal fibers
consist of 1.5 percent Co, 22 percent Cr, 9 percent Mo, 0.6 percent
W, 18 percent Fe, 0.10 percent C, 1.0 percent Si, 1.0 percent Mn,
balance Ni.
16. A method according to claim 9, wherein said shim means is
compressed from a thickness of approximately 1.25 mm to
approximately 1.00 mm during the predeforming step.
17. A shim for use in turbine rotor blade construction comprising a
uniform metallic felt material consisting of sintered metallic
fibers, said material having highly elastic properties and
providing thermal insulation.
18. A shim according to claim 17, wherein said metallic fibers are
approximately 6 to 15 .mu.m in diameter and are sintered by the
application of high heat, pressure and reduced atmosphere.
19. A shim according to claim 18, wherein said metallic felt
material consists of 1.5 percent Co, 22 percent Cr, 9 percent Mo,
0.6 percent W, 18 percent Fe, 0.10 percent C, 1.0 percent Si, 1.0
percent Mn, and balance Ni.
20. A shim according to claim 17, wherein said metallic felt
material is deformed beyond a first plastic limit to achieve the
elastic properties.
Description
BACKGROUND OF THE INVENTION
This invention relates to means for anchoring ceramic turbine
blades in a circumferential walled slot in a steel rotor or blade
seating ring using shims of a heat resistant metallic material
arranged between the blades and the rotor.
German Pat. No. 943,863 discloses a turbine rotor of steel
construction having ceramic blading and metallic layers intervening
between the blades and the steel rotor. The intervening layer of
this patent consists of shims of a non-scaling, heat resistant
metallic material loosely arranged between the bearing surfaces of
the blade root and the supporting surfaces of a suitably conformed
seat in the rotor. Since, in operation the blade is subject to an
outward pull under large centrifugal forces, the shims of this
patent are intended to improve the friction ratios at the bearing
surfaces. A difficulty with this arrangement is that the friction
ratios are very difficult to control adequately especially at
elevated temperatures. A further difficulty with this arrangement
is that in the process of deformation the loosely arranged metallic
shim will inevitably set, so that localized compression may be the
cause of stress peaks in the shim and steel rotor with the
resulting failure of the materials.
DESCRIPTION OF THE INVENTION
The present invention contemplates the provision of means for
retaining turbine blades, especially ceramic turbine blades in
rotors, especially steel rotors, such that uniform transfer of the
retaining force is ensured despite the dimensional tolerances
imposed by manufacturing practice and such that the largely
uncertain friction ratios at the bearing surfaces can be ignored.
The present invention also contemplates a method for constructing
the means to carry out these functions.
The present invention further contemplates providing means for
safely avoiding local load concentrations and the ensuing stress
peaks while promoting the thermal fatigue strength. The present
invention also contemplates the provisions of a seating arrangment
for ceramic turbine blades which is economical in manufacture,
easily maintainable in use, and reliable over long periods of
time.
The present invention further contemplates the provision of an
arrangement for retaining turbine blades, especially ceramic
turbine blades, in a circumferentially extending slot of a
rotatable rotor, especially a steel rotor, including walls on the
slot including inclined portions with a surface component facing
inwardly toward the axis of rotation of the rotor, surfaces on the
blade arranged in the slot approximately parallel to the inclined
portions at a small spacing from the inclined portions, and shim
means positioned between the inclined portions and the surfaces on
the blade wherein the shim means are constructed of sintered metal
felt which has been predeformed beyond a first plastic limit so
that it exhibits highly elastic properties for elastically
absorbing the large centrifugal forces between the rotor and blade
during use whereby the relative movement of the blade and rotor is
primarily a function of the elasticity of the shim and wherein the
shim means also forms a thermal insulation between the rotor and
the blade.
The present invention further contemplates the provision of a
method for retaining turbine blades, especially ceramic turbine
blades, in a circumferentially extending slot of a rotatable rotor,
especially a steel rotor, including forming the slot and the
surface of the blade so as to have respective parallel surfaces
facing one another with the slot surface having a surface component
facing relatively inwardly toward the axis of rotation of the
rotor, constructing shim means of sintered metal felt, predeforming
the shim means beyond a first plastic limit so that the shim means
exhibits elastic properties and high strength, and placing the
predeformed shim means between the respective parallel surfaces of
the slot and blade whereby the shim means effectively elastically
absorbs the transfer of centrifugal forces between said rotor and
blade during use.
The present invention contemplates providing these above-mentioned
benefits by arranging a shim between the internal walls of the
steel rotor slot and the suitably conformed flanks of the blade
root which shim is constructed of a heat resistant, sintered,
highly flexible and elastic metallic felt previously deformed,
after having been sintered, beyond its first plastic limit. The
invention further contemplates attaching the shim to one of the
walls of the slot or the blade.
The basic material contemplated for use in the present invention
for forming the metallic felt has been finding use particularly in
filter work and seals and consists of a uniform metallic felt
composed of, for example, 6 to 15 /.mu.m diameter fibers sintered
by the application of high heat, pressure and reduced atmosphere to
form a metallic bond between the fiber particles along their
contact surfaces. The density, or the pore volume of the sintered
basic material, which exhibits elastic properties until the
proportional limit is reached, can be adjusted primarily by dosing
the pressure during sintering. The pore volume, as well as the
strength of the metallic felt shim is then optimized according to
the present invention by deformation after sintering. This
deformation may be achieved, for example, in a suitable press or as
a result of centrifugal force during a trial run on a blade and
rotor assembly.
While the analysis, 1.5 percent Co, 22 percent Cr, 9 percent Mo,
0.6 percent W, 18 percent Fe, 0.10 percent C, 1.0 percent Si, 1.0
percent Mn, balance Ni, is representative of a suitable felt
material, a material on Co base or of other alloy consistuents
would equally be practicable for use in the present invention.
It is contemplated by the present invention to deform the sintered
basic material beyond its first plastic limit (this first plastic
limit for the sintered material, it being understood that a plastic
limit for the basic unsintered material is surpassed during
sintering due to the high temperature and the pressure conditions
experienced during the sintering process). The thus deformed
metallic felt shim is distinguished with a high degree of
elasticity and very high strength. The range of elasticity of the
deformed felt is particularly suited for the range of forces
experienced in turbine rotor and blade assemblies of the type
referred to herein, such that during operation of the rotor, the
elastic limit is not exceeded thereby preventing stress peaks in
the shim. For example, the sintered basic material, once it has
exceeded a first plastic limit (order of magnitude of 10 to
10.sup.2 kp/cm.sup.2) can be compressed into a very elastic body
exhibiting a very respectable crushing limit (order of magnitude of
10.sup.3 kp/cm.sup.2). Note that 1 kp equals 1,000 grams. Also, the
term "crushing limit" refers to a second plastic limit of the
sintered metallic shim material. Therefore, the present invention
contemplates use of the felt material over the elastic range
between a first plastic limit and a crushing or second upper
plastic limit. Another special merit of the metallic felt shim
according to the present invention is that despite the presence of
a host of pore cells, its structure is substantially uniform such
that it possesses consistent and uniform mechanical and thermic
properties to ensure uniform transfer of the retaining force while
avoiding the build-up of stress peaks. An additional advantage of
the shim of the present invention is found in its notable
capability to dampen blade vibrations.
The thinner the shim material used, the larger will be the modulus
of resilience (c = p/f (kp/cm)) or specific restoring force. P =
spring bias or constant and f = spring stroke. A shim constructed
of the predeformed felt material contemplated by the present
invention (see specific thickness on example described), as
compared with an equally large, equally thick shim of solid steel,
with the same spring stroke (f), the thus produced forces (p) in
the first mentioned case are substantially smaller, for example,
approximately 10 times smaller than is the latter case. Therefore,
the arrangement contemplated by the present invention avoids peak
stresses in areas of locally concentrated loads.
Another asset of the shim in accordance with this invention is that
it offers a wide range of elastic deformability without setting
during rotation of the blades and that it therefore practically
eliminates the problem of controlling the friction ratios at the
bearing surfaces. In this, the high normal forces acting on the
shims cause their elastic deformation such that the radial
movements of the blade are proportional to the deformation of the
shims. As a result, the movement of the blade is primarily not a
function of the friction but is exactly governed by the elasticity
of the shim.
The metal felt shim contemplated by the present invention is
further characterized not only by its remarkable heat resistance
but also by its low thermal conductivity. This is of particular
advantage in that but a small portion of the heat is transferred
from the blade root, where the temperature level may in some
instances be depressed using specially ducted cooling air, to the
turbine rotor. Consequently, the requirements imposed on the rotor
material in the matter of heat resistance are therefore mitigated
permitting the use of less costly materials for the rotor. Owing to
the thermal insulation provided by the layer of metallic felt the
thermal fatigue strength of the blades is equally improved in that
the heat is stored in the highly heat-resistant ceramic blades and
prevented from immediately spreading into the large bulk of the
rotor body.
The accompanying drawing is a sectional view illustrating an
embodiment of the blade seating means assembled in accordance with
this invention. A dovetailed root 2 of a silicon nitride (Si.sub.3
N.sub.4) turbine blade 1 is seated in a circumferential slot 4 in a
steel rotor 3. Arranged between the flanks 2a of the blade root and
the parallelly extending walls 5 of the circumferential slot 4 is a
shim 6 of a heat resistant, sintered and predeformed metallic felt
construction secured in place by brazing or other suitable means.
To support the blade at rest such that the flanks 2a are held
against the shims 6 a strip 7 of metallic felt having the
above-described properties is inserted in the bottom of the
circumferential slot 4.
The shims 6 and strip 7 of the example illustrated may be
constructed of material consisting of 1.5 percent Co, 22 percent
Cr, 0 percent Mo, 0.6 percent W, 18 percent Fe, 0.10percent C, 1.0
percent Si, 1.0 percent Mn, balance Ni. Also materials on Co base
or other alloy constituents would be practical for use in
conjunction with the present invention. The thickness of the
sintered material before deformation could be, for example,
approximately 1.25 mm, which thickness would be compressed to
approximately 1.00 mm during the predeformation step. The pore
volume of the shim material after predeformation, could be
approximately 20 percent of the total volume of the shim. The pore
volume is naturally greater prior to the predeformation step. The
diameter of the blade carrier ring in the zone of the metal felt
shim could be approximately 80 mm. The above dimensions are given
by way of example only for a turbine rotor or blade construction
usable on an automobile gas turbine engine.
Other possible embodiments are also contemplated by this invention,
such as one in which a blade seating ring is split axially or
radially for bolting together, after the blade has been inserted,
the two wall portions carrying the metallic felt.
While we have described only several embodiments and illustrated
only one embodiment in accordance with the present invention, it is
understood that the same is not limited thereto but is susceptible
of numerous changes and modifications as known to those skilled in
the art, and we therefore do not wish to be limited to the details
shown and described herein but intend to cover all such changes and
modifications as are encompassed by the scope of the appended
claims.
* * * * *