Title of Invention

PROCESS FOR PRODUCING A STATOR DIAPHRAGM IN A STEAM TURBINE AND STATOR DIAPHRAGM THUS PRODUCED.

Abstract TITLE: PROCESS FOR PRODUCING A STATOR DIAPHRAGM IN A STEAM TURBINE AND STATOR DIAPHRAGM THUS PRODUCED. A process for producing a stator diaphragm in a steam turbine or gas expander is disclosed. The process includes a preparation phase of two rings machined separately to obtain radial cavities having the profile of blades of a stator stage of the steam turbine or gas expander and for inserting respective ends of the stator blades into cavities in the two rings. An adhesive linen finish tape is applied to the external and internal diameters of the rings. A quantity of brazing material in paste-like form is injected into the cavities taking care to control the injection pressure so that the paste-like brazing material is caused to ascend as far as the limit of the corners of the edge of the slot facign the steam or gas flow channel. The rings are then subjected to a furnace brazing operation in vacuo.
Full Text Process for producing a stator diaphragm in a steam
turbine and stator diaphragm thus produced.
The present invention relates to a process for
producing a stator diaphragm in a steam turbine or gas
expander.
The present invention further relates to a stator
diaphragm for steam turbine or gas expander.
As is known, steam turbines are machines supplied by
vapour, generally water vapour, and suitable for
converting into mechanical work part of the kinetic
energy obtained following the expansion of the steam or
of a previously compressed gas.
In particular, in such machines, the previously
superheated or saturated steam, or a compressed gas, is
caused to expand in the turbine by passing through
several alternate stator and rotor stages.
The rotor stages are integral with the motor shaft to
which they transmit the overall torque, whereas the
stator stages serve to present the flow of steam or gas
in suitable conditions at the inlet of the rotor
blades.
The stator is constituted by a set of stator blades,
between each pair of which a corresponding nozzle is
located.
All the stator blades of a stage are fixed to the case
of the turbine and internally to an appropriate fixing
element, normally called a canopy.
The current technique for constructing and mounting the
stator parts of the steam turbines or gas expanders of
known construction is based on the following machining
cycle.
Firstly, the blade is obtained from a drawn bar, cut to
size and machined at the ends to create a coupling to
the case and a pin for fixing the canopy.
More specifically, the case has a C-shaped cavity
inside which the blades are introduced
circumferentially.
The pitch between the blades is ensured by a spacer
heel which undergoes the same end machining as the
blade for anchorage to the case.
Blades and heels are thus mounted alternately in a slot
obtained on the case of the turbine.
An appropriately perforated ring is then mounted on the
other end of the blade and its anchorage is ensured by
the riveting of the pins of the blades on the ring.
However, it will be noted that the system for mounting
the stator stage described above requires considerable
manual skill, so that it comprises long assembly times
and a qualitative outcome which depends on the ability
of the individual operator.
Furthermore, although this production method has proved
valid over the years, nowadays it is less compatible
with current requirements for reduced construction
times and process repeatability which are
characteristic of the typical specific conditions of
the current competitive market.
Finally, it will be noted that the optional dismantling
of this type of stator stage, when replacement is
required for example, also requires a considerable
amount of time, precisely because of the large number
of component parts.
The object of the invention is therefore to provide a
process for producing a stator diaphragm in a steam
turbine or in a gas expander which permits a reduction
of the construction and assembly time and the
associated machining work, with consequent major
financial advantages.
A further object of the invention is to provide a
process for constructing and brazing stator diaphragms
of steam turbines or gas expanders which enables
construction errors to be substantially reduced.
Another object of the invention is to provide a process
for constructing and brazing stator diaphragms of steam
turbines or gas expanders which enables subsequent
repair or replacement operations to be considerably
simplified.
These and further objects are achieved by a process for
producing a stator diaphragm in a steam turbine or in a
gas expander, characterized in that it provides a
preparation phase of two rings, machined separately to
obtain radial cavities having the profile of the blades
of a stator stage of the above-mentioned steam turbine
or of the above-mentioned gas expander and suitable for
the subsequent housing of the above-mentioned blades,
in which an appropriate quantity of brazing material,
in the form of paste, is inserted into the above-
mentioned cavities and the above-mentioned diaphragm is
subjected to a furnace brazing operation in vacuo.
According to a preferred embodiment of the present
invention, the preparation phase of the rings is
achieved by machining the rings separately by means of
water jet cutting, for the purpose of obtaining the
radial cavities having the profile of the blades, all
with the aid of a numerically controlled machine tool.
According to another preferred embodiment of the
present invention, the preparation phase of the
cavities of the rings is achieved by cutting the
cavities by laser.
Alternatively, the preparation phase of the cavities of
the rings is achieved by cutting the cavities by
electron discharge machining.
According to another preferred embodiment of the
present invention, the brazing material, in the form of
paste, is inserted into the cavities having the profile
of the blades. The subsequent furnace brazing
operation in vacuo promotes the penetration of the
brazing material into the clearance between the profile
of the blades and the said cavities.
According to a further preferred embodiment of the
present invention, subsequent to the brazing operation
the diaphragm is machined according to the final
dimensions and is cut into two half-rings by electron
discharge machining for final mounting in the case of
the above-mentioned steam turbine or the above-
mentioned gas expander.
The present invention also relates to a stator
diaphragm for steam turbine or for gas expander,
characterized in that it comprises two rings, machined
separately to obtain radial cavities having the profile
of the blades and suitable for the subsequent housing
of the above-mentioned blades, in which an appropriate
quantity of brazing material, in the form of paste, is
inserted in the above-mentioned cavities.
Further features of the invention are defined in the
claims accompanying the present patent application.
Further objects and advantages of the present invention
will be evident from a study of the description which
follows and of the accompanying drawings which are
provided purely by way of non-exhaustive explanatory
example, and in which:
Fig. 1 shows a schematic front view, partially in
section according to plane I-I of Fig. 2, of a
stator blade, belonging to a set of stator blades
relating to a stator diaphragm, fixed in position
by means of the process according to the present
invention;
Fig. 2 shows a schematic view, partially in
section according to plane II-II of Fig. 1, of the
stator blade shown in Fig. 1; and
Fig. 3 shows a schematic view, according to
direction A of Fig. 1, of the cavity filled with
brazing material and relating to a stator blade.
With particular reference to the drawings mentioned,
the assembly comprising the stator diaphragm, and the
blades fixed thereto, is denoted overall by the
reference numeral 10.
In substance, in the machining process according to the
present invention, each blade 11 is fixed at the ends
by two rings 12 and 13, so as to create a diaphragm 10.
In particular, a first end of each blade 11 is fixed to
an internal ring 12 whereas another end of each blade
11 is fixed to an external ring 13.
The diaphragm 10 thus formed is then mounted in the
case of the steam turbine, or of the gas expander, in
which a cavity of rectangular cross-section has
previously been produced.
The diaphragm 10 is thus obtained with two rings 12 and
13, preferably forged, which are machined separately
with a water jet cutting process.
In this way radial slots are created with the profile
of the blades 11 for the subsequent housing of the said
blades.
Cutting is carried out with a numerically controlled
machine tool.
According to a number of alternative variants of the
present invention, the cutting process may be carried
out with laser or by means of electron discharge
machining.
The blades 11 are always obtained from a drawn bar and
are cut to size as previously carried out, but are not
machined to have the upper cavity for anchoring them to
the case and the pin at the other end is therefore no
longer present.
The brazing material 14, 14", in the form of paste, is
inserted into the cavities 15, 15" and into the
clearance between the profile of the blades 11 and the
cavities 15, 15" of the external 13 and internal 12
rings.
Brazing takes place in a furnace in vacuo, at
controlled temperature, according to the parameters
outlined below.
The blades 11 are fixed by making a small welding bead
with welding material (on the internal side of the ring
only) so as to ensure a stable position for the
subsequent operations.
An auxiliary adhesive linen-finish tape for the
injection of the brazing paste is applied to the
external and internal diameter of the rings.
The brazing material in the form of paste 14 and 14" is
then injected into the cavities 15 and 15" located on
the rings from both the side of the internal 12 and
external 13 diameter, care being taken to control the
injection pressure so as to cause the paste 14, 14" to
ascend as far as the limit of the corners of the edge
of the slot facing the steam flow channel.
Brazing takes place in a furnace in vacuo at a pressure
less than 5xl0-3 TORR.
After brazing, the diaphragm 10 is machined according
to the final dimensions and is then cut into two half-
rings, by means of electron discharge machining by wire
or laser.
Final assembly in the case is thus reduced to the sole
phase of installing the two half-rings.
The features of the process for producing a stator
diaphragm in a steam turbine to which the present
invention relates will be evident from the description
given, as will the advantages thereof.
The following concluding remarks are intended to define
these advantages more precisely.
The invention described above makes it possible to
install, in a single diaphragm, two rings inside which
the blades of the stator are rendered integral by
brazing.
This solution allows the use of a reduced number of
component parts and permits a considerable
simplification of the operations to replace the
diaphragm 10 when this becomes necessary.
In fact, a truly important aspect of the stator
diaphragm 10 of the invention is provided by the fact
that it gives rise to only two elements to be handled,
the upper half-ring and the lower half-ring, instead of
all the blades 11 as in the systems according to the
prior art.
This means that final assembly and any replacement
which may be necessary can be carried out in a greatly
reduced time, with reduced machine shut-down times and
consequent financial savings.
Furthermore, the structural strength of the diaphragm
is increased, and the manufacturing tolerances are also
reduced, thanks also to the automation of the
production process and the elimination of manual
adjustments.
The technology of water jet cutting, and in particular
of a numerically controlled machine, has been adapted
to the cutting of the slots and enables there to be an
average clearance of 0.05-0.2 mm on the profile of the
blades 11, ensuring economy of machining and accurate
results.
It is evident that numerous variants may be introduced
to the process for producing a stator diaphragm in a
steam turbine, to which the present invention relates,
without thereby departing from the principles of
novelty inherent in the inventive idea described.
Finally it is evident that in the practical
implementation of the invention, the materials, forms
and dimensions of the components described may be of
any kind, according to requirements, and they may be
replaced by others which are equivalent from the
technical point of view.
WE CLAIM:
1. Process for producing a stator diaphragm (10) in a steam turbine
or gas expander with a preparation phase of two rings machined
separately to obtain radial cavities (15,15") having the profile or
blades (110) of a stator stage of the steam turbine or gas
expander and for inserting respective ends of the stator blades
into cavities in the two rings and characterized by applying an
adhesive linen-finish tape to the external and internal diameters
of the rings, injecting into the cavities a quantity of brazing
material in paste-like form wherein care Is taken to control the
injection pressure so as to cause the paste-like brazing material
to ascend as far as the limit of the corners of the edge of the slot
facing the steam or gas flow channel and then subjecting the two
rings to a furnace brazing operation in vacuo.
2. Process according to claim 1, characterized in that the above-
mentioned preparation phase of the above-mentioned rings
(12,13) is achieved by machining the above-mentioned two rings
(12,13) separately by means of water Jet cutting, for the
purpose of obtaining the above-mentioned radial cavities (15,
15") having the profile of the blades (11), with the aid of a
numerically controlled machine tool.
3. Process according to claim 1, characterized in that the above-
mentioned preparation phase of the cavities (15, 15") of the
above-mentioned rings (12,13) is achieved by cutting the above-
mentioned cavities (15,15") by laser.
4. Process according to claim 1, characterized in that the above-
mentioned preparation phase of the cavities (15, 15") of the
above-mentioned rings (12,13) is achieved by cutting the above-
mentioned cavities (15,15") by electron discharge machining.
5. Process according to claim 1, characterized in that the brazing
material (14,14") in the form of paste, is inserted into the above-
mentioned cavities (15,15") and into the clearance between the
profile of the blades (11) and the above-mentioned cavities (15,
15") of the rings (12,13).

6. Process according to one of the preceding claims, characterized
in that, subsequent to the brazing operation, the above-
mentioned diaphragm (10) is machined according to the final
dimensions and is cut into two half-rings by electron discharge
machining or by laser for final mounting In the Internal case of
the above-mentioned steam turbine or the above-mentioned gas
expander.
7. Stator diaphragm (10) for a steam turbine or gas expander
comprising inner and outer rings (12,13) machined separately to
obtain radial cavities (15,150 having a profile of blades (11)
extending between said inner and outer rings and characterized
by a quantity of brazing material applied in the form of a paste
inserted in the above-mentioned cavities (15,15"), said rings
having an adhesive linen-finish tape applied to the external and
Internal diameters of the rings to cause the paste-like brazing
material to ascend as far as the limit of the corners of the edge
of the slot facing the steam or gas flow channel and heat being
applied to said braze material to form the diaphragm.
Process for producing a stator diaphragm in a steam
turbine and stator diaphragm thus produced
A process for producing a stator diaphragm (10) in a steam turbine
or gas expander is disclosed. The process includes a preparation
phase of two rings (12,13) machined separately to obtain radial
cavities (15,15") having the profile of blades (11) of a stator stage of
the steam turbine or gas expander and for inserting respective ends
of the stator blades into cavities in the two rings. An adhesive linen
finish tape is applied to the external and internal diameters of the
rings. A quantity of brazing material in paste-like form is injected into
the cavities taking care to control the injection pressure so that the
paste-like brazing material is caused to ascend as far as the limit of
the corners of the edge of the slot facing the steam or gas flow
channel. The rings are then subjected to a furnace brazing operation
in vacuo.

Documents:

214-cal-2001-granted-abstract.pdf

214-cal-2001-granted-claims.pdf

214-cal-2001-granted-correspondence.pdf

214-cal-2001-granted-description (complete).pdf

214-cal-2001-granted-drawings.pdf

214-cal-2001-granted-form 1.pdf

214-cal-2001-granted-form 18.pdf

214-cal-2001-granted-form 2.pdf

214-cal-2001-granted-form 3.pdf

214-cal-2001-granted-form 5.pdf

214-cal-2001-granted-letter patent.pdf

214-cal-2001-granted-pa.pdf

214-cal-2001-granted-priority document.pdf

214-cal-2001-granted-reply to examination report.pdf

214-cal-2001-granted-specification.pdf

214-cal-2001-granted-translated copy of priority document.pdf


Patent Number 218690
Indian Patent Application Number 214/CAL/2001
PG Journal Number 15/2008
Publication Date 11-Apr-2008
Grant Date 09-Apr-2008
Date of Filing 11-Apr-2001
Name of Patentee NUOVO PIGNONE HOLDING S.P.A.
Applicant Address 2, VIA FELICE MATTEUCCI, 50127 FIRENZE, ITALY.
Inventors:
# Inventor's Name Inventor's Address
1 GHELLI GIUSEPPE VIA ADUA 158 1-52043 CASTIGLION FIORENTINO (AREZZO) ITALY.
PCT International Classification Number F01D 9/04
PCT International Application Number N/A
PCT International Filing date
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 MI2000A 000870 2000-04-18 Italy