US3881842A - Diaphragm for steam turbine stage - Google Patents

Diaphragm for steam turbine stage Download PDF

Info

Publication number
US3881842A
US3881842A US349813A US34981373A US3881842A US 3881842 A US3881842 A US 3881842A US 349813 A US349813 A US 349813A US 34981373 A US34981373 A US 34981373A US 3881842 A US3881842 A US 3881842A
Authority
US
United States
Prior art keywords
blade
diaphragm
blades
liquid phase
guide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US349813A
Inventor
Jury Fedorovich Kosyak
Sergei Petrovich Sobolev
Ary Fedorovich Rudkovsky
Viktor Vasilievich Ugolnikov
Yakov Lvovich Iglinsky
Nikolai Artemovic Babadzhanian
Semen Iosifovich German
Ivan Fedorovich Ochkovsky
Teodor Markovich Zilber
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US349813A priority Critical patent/US3881842A/en
Application granted granted Critical
Publication of US3881842A publication Critical patent/US3881842A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32Collecting of condensation water; Drainage ; Removing solid particles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Definitions

  • a diaphragm for a steam turbine stage comprises hollow guide blades with one end of each blade being fixed to a diaphragm rim and with the other to a diaphragm body.
  • Each blade is provided with at least one slot for removal of liquid phase from wet steam, said slot being communicated with the interior of a blade and located in a moisture collecting groove made on the flat surface of the blade profile from the intake side of the wet steam main flow.
  • the present invention relates to the field of steam turbines and, more particularly, to diaphragrns for a steam turbine stage.
  • the present invention may be successfully used for removal of a course dispersoid phase from diaphragms of steam turbine stages working within wet steam ranges.
  • a diaphragm for a steam turbine comprising hollow guide blades.
  • Each of the blades has one end fixed to the diaphragm rim and the otherto the diaphragm body.
  • the arrangement of the diaphragm with respect to the runner of the tubine is so that the wet steam main flow, which leaves the guide blade channels formed by adjacent blade profiles, acts upon the runner thereby rotating it.
  • the diaphragm and the runner form a turbine stage.
  • the effective part of a turbine consists of a number of serially arranged turbine stages.
  • the liquid phase Upon passage of the wet steam flow through the guide blade channels, the liquid phase settles down to the surfaces of the guide blades and flows towards the outlet ends thereof. Having separated from the outlet ends of the guide blades the liquid phase reaches the runner blades.
  • the direction of the velocity vector of liquid phase is opposite to the vector of the runner rotational speed, thereby hampering the rotation of the runner decelerating it and resulting in a loss of efficiency of a turbine stage, and hence, of a turbine as a whole.
  • peripheral and intrachannel removal of liquid phase from guide blades of the diaphragm are peripheral and intrachannel removal of liquid phase from guide blades of the diaphragm.
  • An example of the intrachannel liquid phase removal from the surface of the guide blades is a diaphragm of a condensing turbine comprising the hollow guide blades.
  • Each blade has one end fixed to the diaphragm rim and the other to the diaphragm body. Furthermore, each blade is provided with a slot for removal of the liquid phase from wet steam. This slot is communicated with the interior of the blade and is located at the outlet end of the blade along the profile surface thereof. The interior of the blade is connected to a condenser. The liquid phase, upon flowing around the guide blade profile, is sucked into the interior of the blade through the slot due to a pressure difference in the channel formed by the profiles of the two adjacent blades.
  • the diaphragm of a low pressure stage comprises hollow guide blades. These blades partially or wholly are made of porous metal. One end of each blade is fixed to the diaphragm rim, and the other to the diaphragm body. The interior of the blade is communicated with a condenser.
  • liquid phase removal from the guide blade surface of this diaphragm is not very effective, because a portion of the liquid phase upon encountering the porous surface is rebound to the wet steam flow thus leading to the erosion of the runner blades and to gradual destruction of the blade edges resulting in a loss of the efficiency of a turbine stage.
  • a diaphragm of a steam turbine stage with the intrachannel moisture separation comprises hollow guide blades. One end of each blade is fixed to the diaphragm body and the other to the diaphragm rim.
  • the hollow blade is provided with an opening for moisture removal. These openings located at the outlet end of the blade are communicated with the interior of the blade.
  • the interior of the guide blade is connected to a turbine condenser.
  • Liquid phase flowing around a blade profile is sucked under the action of the pressure difference between the interior of the guide blade and the guide blade channel into the interior of the blade through the openings and upon passing further through the body and rim of the diaphragm it reaches the condenser.
  • the diaphragm comprises hollow guide blades. One end of each blade is fixed to the diaghragm rim and the other to the diaphragm body.
  • the hollow blade is provided with grooves made on the concave and convex sides thereof. The grooves are communicated with the interior of the blade which in turn is connected to a condenser.
  • Liquid phase flowing around the guide blade is sucked under the action of the pressure difference between the interior of the guide blade and the guide blade channel into the interior of the blade and then flows further into the condenser.
  • such embodiment of the diaphragm permits only a small quantity of the liquid phase to be led out of the effective part of the turbine since the slots are located in the zone of high pressure gradients, where the liquid phase is subjected to atomization, blowing off the blades and entrainment by the wet steam flow giving rise to the runner blades erosion and a loss of the efficiency of a turbine stage.
  • Liquid phase flowing around the guide blade enters the internal chambers of the blade due to the pressure difference in the interior of the guide blade and in the channels of the guide blade, and then flows further to the condenser.
  • Such an arrangement of the guiding system cannot provide for maintenance of the moisture film in the vicinity of moisture-removing slots located in the zone of high pressure gradients. This film is atomized and entrained by the main flow bypassing the moisture-removing slots. Coming to the runner rotor blades the liquid phase destructs the inlet edge thereof and leads a loss of the efficiency of the turbine stage.
  • Another object of the present invention is to prolong the service life of the runner blades of the turbine stage and to increase reliability thereof by reducing their erosion.
  • the invention consists in that in a diaphragm for a steam turbine stage comprising hollow guide blades having one end fixed to the diaphragm rim and the other to the diaphragm body and being provided with at least one slot for removal of the liquid phase from wet steam, said slot being communicated with the interior of the blade, according to the invention, each hollow guide blade is provided with a moisture collecting groove formed on the flat surface of the blade profile on the wet steam inlet side thereof, and a slot for removing the liquid phase is located in the groove.
  • a steam turbine diaphragm made in accordance with the invention prevents a loss of the efficiency of a steam turbine stage.
  • Such an arrangement of the groove prevents the liquid phase accumulated in this groove from being entrained and separated by the main wet steam flow, while on the other hand, this arrangement contributes to an increase in quantity of the liquid phase removed from the effective part of the turbine.
  • the size of the slot be such as the velocity of the wet steam flow in this slot would be approximately equal to that of the main wet steam flow.
  • a diaphragm made in accordance with the present invention makes it possible to remove from the effective part of a turbine up to 8 percent of the liquid phase and about 60 percent of the coarse dispersoid liquid phase which is most detrimental from the viewpoint of the erosion and the liquid phase effectivity.
  • the removal of the liquid phase from the low-pressure cylinder of a stationary turbine used at a power plant substantially reduced the runner blade erosion and increased the turbine efficiency.
  • FIG. 1 is a view of a diaphragm for the ultimate stage of a steam turbine
  • FIG. 2 is an enlarged sectional view taken along the line IIII in FIG. 1;
  • FIG. 3 is a sectional view taken along the line III-III in FIG. 2;
  • FIG. 4 is a view of another embodiment of a steam turbine stage diaphragm made in accordance with the present invention.
  • a diaphragm for the ultimate stage of a steam turbine comprises welded hollow blades 1 (FIG. 1). One end of each blade 1 is welded to a diaphragm rim 2 and the other to a diaphragm body 4 by means of a bandage 3.
  • the rim 2 and the body 4 may have either cast or welded structure.
  • each hollow guide blade 1 is provided with a groove 5 (FIG. 2) adapted to collect liquid phase.
  • the groove is communicated with a slot 6 for the liquid phase removal.
  • the size of the slot 6 is such as to ensure that velocity of steam-and-water mixture in this slot be approximately equal to that of the wet steam main flow.
  • the profiles of the adjacent guide blades 1 define a guide channel 7 (FIG. 3) adapted to receive the wet steam main flow.
  • the liquid phase collecting groove 5 is arranged on the flat surface 8 of the profile of the blade 1.
  • the surface 8 on the convex portion of the blade 1 is subjected to the action of low pressure gradients.
  • the slot 6 is communicated with the interior 9 of the guide blade 1.
  • an external bandage 12 (FIG. 2) is made only at the outlet portion of the blade 1, this bandage being welded along with the blade 1 to the rim 2 on the wet steam outlet side. On the wet steam inlet side the guide blades 1 are welded directly to the rim 2.
  • the interior 9 of the guide blade 1 (FIG. 3) is communicated only with an annular channel 13 (FIG. 2) of the rim 2 and with an annular channel 14 of the body 4.
  • the rim 2 is provided with openings 15 facing each guide blade 1, which are adapted to establish communication between the channel 13 and a condenser (not shown in the drawings), and with an annular channel 16 formed on the wet steam outlet side to remove moisture from the preceding stage.
  • the slots 6 (FIG. 4) provided for the liquid phase removal are disposed at 150 to the plane extending through the inlet edges 17 of the hollow guide blades 1, thereby contributing to an increase in quantity of the liquid phase being sucked out.
  • the wet steam leaving the preceding stage contains a substantial quantity of the coarse dispersoid moisture.
  • component drops of moisture are deflected towards the periphery and guided to the convex portion of the guide blades 1 (F IG. 1) of the next turbine stage.
  • a fraction of moisture is removed via the channel 16 (FIG. 2) formed in the rim 2 of the diaphragm at the wet steam inlet side, while the rest of the moisture flows to the convex portion of the hollow guide blades 1.
  • the ratio between the cross-sectional areas of the throttle openings 15 and of the slots 6 of the guide blades 1 is selected so that the wet steam velocity in these slots be equal to the velocity of the wet steam main flow. This velocity is an optimal one from the viewpoint of the moisture removal.
  • a diaphragm for a steam turbine stage comprising hollow guided blades having concave and convex sur-. faces for directing the main wet steam flow onto turbine rotor blades; a diaphragm rim having one end of each guide blade being fixed thereto; and a diaphragm body having the other end of each said guide blade fixed thereto, each said guide blade having a flat surface portion on the convex surface proximate the wet steam inlet side thereof, a plurality of radially spaced slots in said flat surface portion extending along the upstream side of each said blade and communicating with the interior of said blade, and a radially extending recessed portion forming a groove common to all of said slots on respectively each of said blades for collecting the liquid phase formed on said flat surface portion of each blade.
  • each of said slots for the liquid phase removal being inclined at an angle of relative to the inlet plane of said hollow guide blades.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A diaphragm for a steam turbine stage comprises hollow guide blades with one end of each blade being fixed to a diaphragm rim and with the other - to a diaphragm body. Each blade is provided with at least one slot for removal of liquid phase from wet steam, said slot being communicated with the interior of a blade and located in a moisture collecting groove made on the flat surface of the blade profile from the intake side of the wet steam main flow.

Description

D United States Patent 1191 1111 3,881,842 Kosyak et al. May 6, 1975 DIAPHRAGM FOR STEAM TURBINE [51] Int. Cl. F0ld 25/32 STAGE [58] Field of Search 4115/121 A, 168; 416/168 [76] Inventors: Jury Fedorovich Kosyak, prospekt Moskovsky 202, kv. s5; Sergei [561 References Petrovich Sobolev, pereulok UNITED STATES PATENTS Molchanovsky y 2,362,831 11 1944 Kraft 415/168 Fedorovich Rudkovsky, ploschad 2,399,009 4/1946 Doran 415/121 A f l 3 FOREIGN PATENTS OR APPLICATIONS vasllievlch Ugolmkov, ploschad 343 07 931 U t d d 68 me mg om Teveleva 2/2, kv. 28, Yakov Lvovlch 948,293 H1964 United Kingdom Iglinsky, ulitsa Mezhlauka, 9/2, kv. 39; Nikolai Artemovich Babadzhanian, ulitsa Ganny, 44, kv. 3; Semen Iosifovich German, ulitsa Mayakovskogo, 11, kv. 21; Ivan Fedorovich Ochkovsky, ulitsa Kleimenovskaya 15; Teodor Markovich Zilber, ulitsa Danilevskogo, 22, kv. 100, all of Kharkov, U.S.S.R.
[22] Filed: Apr. 10, 1973 [21] Appl. No.: 349,813
[52] US. Cl. 415/168; 415/121 A vzs gawl 7 a Primary Examiner-Henry F. Raduazo [57] ABSTRACT A diaphragm for a steam turbine stage comprises hollow guide blades with one end of each blade being fixed to a diaphragm rim and with the other to a diaphragm body. Each blade is provided with at least one slot for removal of liquid phase from wet steam, said slot being communicated with the interior of a blade and located in a moisture collecting groove made on the flat surface of the blade profile from the intake side of the wet steam main flow.
2 Claims, 4 Drawing Figures PATENIEDMAY 6l975 SHEET 2 OF 2 DIAPHRAGM FOR STEAM TURBINE STAGE The present invention relates to the field of steam turbines and, more particularly, to diaphragrns for a steam turbine stage.
The present invention may be successfully used for removal of a course dispersoid phase from diaphragms of steam turbine stages working within wet steam ranges.
A diaphragm for a steam turbine comprising hollow guide blades is known. Each of the blades has one end fixed to the diaphragm rim and the otherto the diaphragm body. The arrangement of the diaphragm with respect to the runner of the tubine is so that the wet steam main flow, which leaves the guide blade channels formed by adjacent blade profiles, acts upon the runner thereby rotating it. The diaphragm and the runner form a turbine stage. The effective part of a turbine consists of a number of serially arranged turbine stages.
Wet steam consists of gaseous and liquid phases.
Upon passage of the wet steam flow through the guide blade channels, the liquid phase settles down to the surfaces of the guide blades and flows towards the outlet ends thereof. Having separated from the outlet ends of the guide blades the liquid phase reaches the runner blades. The direction of the velocity vector of liquid phase is opposite to the vector of the runner rotational speed, thereby hampering the rotation of the runner decelerating it and resulting in a loss of efficiency of a turbine stage, and hence, of a turbine as a whole.
Furthermore, the contact between the liquid phase and the runner of a turbine brings about the erosion of the latter which also leads to a loss of efficiency and shortening of the service life of the blade and a turbine as a whole.
Attempts to prevent contact of the liquid phase with the runner blades of a turbine were made following two paths:
peripheral and intrachannel removal of liquid phase from guide blades of the diaphragm.
In the case of the peripheral removal of the liquid phase the latter is rejected into the peripheral zone and led out of the effective part of the turbine under the action of the wet steam main flow and the centrifugal forces upon the runner blades.
The common practice revealed that the peripheral moisture removal is not effective.
An example of the intrachannel liquid phase removal from the surface of the guide blades is a diaphragm of a condensing turbine comprising the hollow guide blades. Each blade has one end fixed to the diaphragm rim and the other to the diaphragm body. Furthermore, each blade is provided with a slot for removal of the liquid phase from wet steam. This slot is communicated with the interior of the blade and is located at the outlet end of the blade along the profile surface thereof. The interior of the blade is connected to a condenser. The liquid phase, upon flowing around the guide blade profile, is sucked into the interior of the blade through the slot due to a pressure difference in the channel formed by the profiles of the two adjacent blades. From the interior of the blade the liquid phase is led out into the condenser through the body and the rim of the diaphragm. However, only a small quantity of the liquid phase can be led out of the effective part of the turbine due to the fact that the slots are located in the zone of high pressure gradients, and in this zone the liquid phase is atomized, blown off and entrained by the main wet steam flow to the runner of the turbine stage. This also gives rise to the erosion of the runner blades thus resulting in a loss of the efficiency of the turbine stage.
Also known in the art is a diaphragm of a steam turbine low pressure stage.
The diaphragm of a low pressure stage comprises hollow guide blades. These blades partially or wholly are made of porous metal. One end of each blade is fixed to the diaphragm rim, and the other to the diaphragm body. The interior of the blade is communicated with a condenser.
Upon contacting the surface of the guide blade the liquid phase due to the pressure difference between the interior of the guide blades and the guide blade channels is sucked into the interior of the guide blade and then is fed into the condenser.
However, the liquid phase removal from the guide blade surface of this diaphragm is not very effective, because a portion of the liquid phase upon encountering the porous surface is rebound to the wet steam flow thus leading to the erosion of the runner blades and to gradual destruction of the blade edges resulting in a loss of the efficiency of a turbine stage.
Furthermore, known in the art is a diaphragm of a steam turbine stage with the intrachannel moisture separation. This diaphragm comprises hollow guide blades. One end of each blade is fixed to the diaphragm body and the other to the diaphragm rim. The hollow blade is provided with an opening for moisture removal. These openings located at the outlet end of the blade are communicated with the interior of the blade. The interior of the guide blade is connected to a turbine condenser.
Liquid phase flowing around a blade profile is sucked under the action of the pressure difference between the interior of the guide blade and the guide blade channel into the interior of the blade through the openings and upon passing further through the body and rim of the diaphragm it reaches the condenser.
Such an arrangement, however, allows only a small quantity of the liquid phase to be removed from the effective part of the turbine since the openings provided in the guide blades are located in the zone of high pressure gradients thus leading to atomization of the liquid phase and entrainment thereof with the wet steam main flow to the runner blades.
Upon contacting the edges of the runner blades the liquid phase gives rise to erosion thereof, i.e. gradual destruction of the inlet edges of these blades, thus leading to a loss of the efficiency of the turbine blades.
Also known in the art is a diaphragm of a steam turbine stage with intrachannel separation of moisture.
The diaphragm comprises hollow guide blades. One end of each blade is fixed to the diaghragm rim and the other to the diaphragm body. The hollow blade is provided with grooves made on the concave and convex sides thereof. The grooves are communicated with the interior of the blade which in turn is connected to a condenser.
Liquid phase flowing around the guide blade is sucked under the action of the pressure difference between the interior of the guide blade and the guide blade channel into the interior of the blade and then flows further into the condenser. However, such embodiment of the diaphragm permits only a small quantity of the liquid phase to be led out of the effective part of the turbine since the slots are located in the zone of high pressure gradients, where the liquid phase is subjected to atomization, blowing off the blades and entrainment by the wet steam flow giving rise to the runner blades erosion and a loss of the efficiency of a turbine stage.
It is also known another construction of a turbine diaphragm with the intrachannel moisture separation system comprising the guide blades. One end of each blade is fixed to the diaphragm body and the other to the diaphragm rim. In this construction a slot is provided on the concave surface of the blade for moisture removal. Furthermore, openings are made in the concave surface of the blades, said openings being arranged downstream relative to the slots and on the isobar line as to the height of the blade. Each group consisting of the slot and the openings is provided with individual lip and a bleeding chamber. The interior of the blade is divided into chambers sealed off each other, said chambers in turn being communicated with a condenser.
Liquid phase flowing around the guide blade enters the internal chambers of the blade due to the pressure difference in the interior of the guide blade and in the channels of the guide blade, and then flows further to the condenser. However, such an arrangement of the guiding system cannot provide for maintenance of the moisture film in the vicinity of moisture-removing slots located in the zone of high pressure gradients. This film is atomized and entrained by the main flow bypassing the moisture-removing slots. Coming to the runner rotor blades the liquid phase destructs the inlet edge thereof and leads a loss of the efficiency of the turbine stage.
It is an object of the present invention to increase efficiency of a steam turbine stage by substantially removing the coarse dispersoid liquid phase from the main wet steam flow.
Another object of the present invention is to prolong the service life of the runner blades of the turbine stage and to increase reliability thereof by reducing their erosion.
In accordance with these and other objects, the invention consists in that in a diaphragm for a steam turbine stage comprising hollow guide blades having one end fixed to the diaphragm rim and the other to the diaphragm body and being provided with at least one slot for removal of the liquid phase from wet steam, said slot being communicated with the interior of the blade, according to the invention, each hollow guide blade is provided with a moisture collecting groove formed on the flat surface of the blade profile on the wet steam inlet side thereof, and a slot for removing the liquid phase is located in the groove.
A steam turbine diaphragm made in accordance with the invention prevents a loss of the efficiency of a steam turbine stage.
These objects are achieved by removing the coarse dispersoid liquid phase from the wet steam flow. The film flowing in the groove eliminates the possibility of the rejection of the drops of moisture back into the wet steam flow at the moment of their contact with the blade. At the same time, the liquid phase is accumulated in the groove of each blade, wherefrom it is sucked out into the interior of the guide blade.
Considerable reduction of quantity of the coarse dispersoid liquid phase ensures, due to less intensive erosion, an increase in the service life and reliability of the runner blades of a turbine stage.
It is advantageous to arrange the groove on the flat surface of the convex portion of the blade which is characterized by rather low pressure gradients.
Such an arrangement of the groove prevents the liquid phase accumulated in this groove from being entrained and separated by the main wet steam flow, while on the other hand, this arrangement contributes to an increase in quantity of the liquid phase removed from the effective part of the turbine.
It is also advantageous to arrange the slots for moisture removal at to the plane extending through the inlet edges of the hollow guide blades which also contributes to an increase in quantity of the sucked-out moisture.
It ia advisable that the size of the slot be such as the velocity of the wet steam flow in this slot would be approximately equal to that of the main wet steam flow.
This condition ensures the most effective suction of the liquid phase from steam. The reduction of wet steam suction speed in the slot results in an additional entrainment of the liquid phase from the slot to the guide blade channels by the main flow thereby reducing the efficiency of operation of the diaphragm.
An increase in the wet steam velocity in the slot leads to the removal of an additional quantity of working medium from the effective part of the turbine which also leads to a loss of the turbine stage efficiency.
A diaphragm made in accordance with the present invention makes it possible to remove from the effective part of a turbine up to 8 percent of the liquid phase and about 60 percent of the coarse dispersoid liquid phase which is most detrimental from the viewpoint of the erosion and the liquid phase effectivity. The removal of the liquid phase from the low-pressure cylinder of a stationary turbine used at a power plant substantially reduced the runner blade erosion and increased the turbine efficiency.
Further features and advantages of the present invention will appear from the following detailed description with reference to the accompanying drawings, in which:
FIG. 1 is a view of a diaphragm for the ultimate stage of a steam turbine;
FIG. 2 is an enlarged sectional view taken along the line IIII in FIG. 1;
FIG. 3 is a sectional view taken along the line III-III in FIG. 2;
FIG. 4 is a view of another embodiment of a steam turbine stage diaphragm made in accordance with the present invention.
A diaphragm for the ultimate stage of a steam turbine comprises welded hollow blades 1 (FIG. 1). One end of each blade 1 is welded to a diaphragm rim 2 and the other to a diaphragm body 4 by means of a bandage 3. The rim 2 and the body 4 may have either cast or welded structure.
At the wet steam inlet side each hollow guide blade 1 is provided with a groove 5 (FIG. 2) adapted to collect liquid phase. The groove is communicated with a slot 6 for the liquid phase removal. The size of the slot 6 is such as to ensure that velocity of steam-and-water mixture in this slot be approximately equal to that of the wet steam main flow.
The profiles of the adjacent guide blades 1 define a guide channel 7 (FIG. 3) adapted to receive the wet steam main flow.
The liquid phase collecting groove 5 is arranged on the flat surface 8 of the profile of the blade 1. The surface 8 on the convex portion of the blade 1 is subjected to the action of low pressure gradients. The slot 6 is communicated with the interior 9 of the guide blade 1.
In order to ensure a required distance between the outlet edges 10 of the guide blades 1 and those of a throat 11 of the guide channels 7, an external bandage 12 (FIG. 2) is made only at the outlet portion of the blade 1, this bandage being welded along with the blade 1 to the rim 2 on the wet steam outlet side. On the wet steam inlet side the guide blades 1 are welded directly to the rim 2.
The interior 9 of the guide blade 1 (FIG. 3) is communicated only with an annular channel 13 (FIG. 2) of the rim 2 and with an annular channel 14 of the body 4. The rim 2 is provided with openings 15 facing each guide blade 1, which are adapted to establish communication between the channel 13 and a condenser (not shown in the drawings), and with an annular channel 16 formed on the wet steam outlet side to remove moisture from the preceding stage.
In case where a diaphragm is used in the ultimate stage of a steam turbine, the slots 6 (FIG. 4) provided for the liquid phase removal are disposed at 150 to the plane extending through the inlet edges 17 of the hollow guide blades 1, thereby contributing to an increase in quantity of the liquid phase being sucked out.
In operation of the ultimate turbine stage the wet steam leaving the preceding stage contains a substantial quantity of the coarse dispersoid moisture. Under the action of a high circumferential velocity, component drops of moisture are deflected towards the periphery and guided to the convex portion of the guide blades 1 (F IG. 1) of the next turbine stage. A fraction of moisture is removed via the channel 16 (FIG. 2) formed in the rim 2 of the diaphragm at the wet steam inlet side, while the rest of the moisture flows to the convex portion of the hollow guide blades 1. Due to a pressure difference between the chamber 9 of the guide blade (FIG. 3) and the guide channel 7, moisture passes into the interior 9 of the guide blade 1 through the slots 6.
Some quantity of moisture flows from the interior 9 of the guide blades in the upper half of the diaphragm into the annular channel 14 (FIG. 2) formed in the diaphragm body 4, and then flows to the lower half of the diaphragm and through the interior 9 of several blades 1 to the channel 13 made in the rim 2, wherefrom moisture reaches the condenser through the openings 15. A portion of moisture is entrained by wet steam and led out of the stage through the openings 15. From the blades of the lower half of the diaphragm moisture flows directly to the annular channel 13 of the rim 2 and to the condenser through the openings 15.
In order to ensure the most effective moisture removal from the surface of the guide blades 1, the ratio between the cross-sectional areas of the throttle openings 15 and of the slots 6 of the guide blades 1 is selected so that the wet steam velocity in these slots be equal to the velocity of the wet steam main flow. This velocity is an optimal one from the viewpoint of the moisture removal.
It will be apparent to those skilled in the art that various modifications may be made in the structure of the steam turbine stage without departing from the scope of the appended claims.
What is claimed is:
l. A diaphragm for a steam turbine stage comprising hollow guided blades having concave and convex sur-. faces for directing the main wet steam flow onto turbine rotor blades; a diaphragm rim having one end of each guide blade being fixed thereto; and a diaphragm body having the other end of each said guide blade fixed thereto, each said guide blade having a flat surface portion on the convex surface proximate the wet steam inlet side thereof, a plurality of radially spaced slots in said flat surface portion extending along the upstream side of each said blade and communicating with the interior of said blade, and a radially extending recessed portion forming a groove common to all of said slots on respectively each of said blades for collecting the liquid phase formed on said flat surface portion of each blade.
2. A diaphragm as claimed in claim 1, each of said slots for the liquid phase removal being inclined at an angle of relative to the inlet plane of said hollow guide blades.

Claims (2)

1. A diaphragm for a steam turbine stage comprising hollow guided blades having concave and convex surfaces for directing the main wet steam flow onto turbine rotor blades; a diaphragm rim having one end of each guide blade being fixed thereto; and a diaphragm body having the other end of each said guide blade fixed thereto, each said guide blade having a flat surface portion on the convex surface proximate the wet steam inlet side thereof, a plurality of radially spaced slots in said flat surface portion extending along the upstream side of each said blade and communicating with the interior of said blade, and a radially extending recessed portion forming a groove common to all of said slots on respectively each of said blades for collecting the liquid phase formed on said flat surface portion of each blade.
2. A diaphragm as claimed in claim 1, each of said slots for the liquid phase removal being inclined at an angle of 150* relative to the inlet plane of said hollow guide blades.
US349813A 1973-04-10 1973-04-10 Diaphragm for steam turbine stage Expired - Lifetime US3881842A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US349813A US3881842A (en) 1973-04-10 1973-04-10 Diaphragm for steam turbine stage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US349813A US3881842A (en) 1973-04-10 1973-04-10 Diaphragm for steam turbine stage

Publications (1)

Publication Number Publication Date
US3881842A true US3881842A (en) 1975-05-06

Family

ID=23374078

Family Applications (1)

Application Number Title Priority Date Filing Date
US349813A Expired - Lifetime US3881842A (en) 1973-04-10 1973-04-10 Diaphragm for steam turbine stage

Country Status (1)

Country Link
US (1) US3881842A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4263842A (en) * 1978-08-02 1981-04-28 Moore Robert D Adjustable louver assembly
US5161942A (en) * 1990-10-24 1992-11-10 Westinghouse Electric Corp. Moisture drainage of honeycomb seals
US6007296A (en) * 1997-03-08 1999-12-28 Abb Research Ltd. Guide blade for steam turbines
US20070014670A1 (en) * 2005-07-15 2007-01-18 Kabushiki Kaisha Toshiba Nozzle blade for steam turbine, nozzle diaphragm and steam turbine employing the same, and method of fabricating the same
US20070154306A1 (en) * 2006-01-04 2007-07-05 General Electric Company Rotary machines and methods of assembling
US20070274824A1 (en) * 2006-05-23 2007-11-29 General Electric Company Airfoil and method for moisture removal and steam injection
US20100329853A1 (en) * 2009-06-30 2010-12-30 General Electric Company Moisture removal provisions for steam turbine
CN102128060A (en) * 2011-04-28 2011-07-20 武汉大学 Superhydrophobic hollow dehumidifying stationary blade
JP2012241607A (en) * 2011-05-19 2012-12-10 Toshiba Corp Steam turbine
ITCO20110060A1 (en) * 2011-12-12 2013-06-13 Nuovo Pignone Spa STEAM TURBINE, PALLET AND METHOD
US8998571B2 (en) 2012-01-05 2015-04-07 General Electric Company Slotted turbine airfoil
JP2015068325A (en) * 2013-09-30 2015-04-13 株式会社東芝 Water droplet removing device for steam turbine
US9359913B2 (en) 2013-02-27 2016-06-07 General Electric Company Steam turbine inner shell assembly with common grooves
US20160169015A1 (en) * 2014-12-15 2016-06-16 Mitsubishi Hitachi Power Systems, Ltd. Steam Turbine Stationary Blade
JP2017502188A (en) * 2013-10-23 2017-01-19 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. Method for manufacturing a steam turbine stage

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2362831A (en) * 1943-08-20 1944-11-14 Gen Electric Elastic fluid turbine
US2399009A (en) * 1944-07-25 1946-04-23 Gen Electric Elastic fluid turbine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2362831A (en) * 1943-08-20 1944-11-14 Gen Electric Elastic fluid turbine
US2399009A (en) * 1944-07-25 1946-04-23 Gen Electric Elastic fluid turbine

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4263842A (en) * 1978-08-02 1981-04-28 Moore Robert D Adjustable louver assembly
US5161942A (en) * 1990-10-24 1992-11-10 Westinghouse Electric Corp. Moisture drainage of honeycomb seals
US6007296A (en) * 1997-03-08 1999-12-28 Abb Research Ltd. Guide blade for steam turbines
US20070014670A1 (en) * 2005-07-15 2007-01-18 Kabushiki Kaisha Toshiba Nozzle blade for steam turbine, nozzle diaphragm and steam turbine employing the same, and method of fabricating the same
US20070154306A1 (en) * 2006-01-04 2007-07-05 General Electric Company Rotary machines and methods of assembling
US7780407B2 (en) 2006-01-04 2010-08-24 General Electric Company Rotary machines and methods of assembling
US20070274824A1 (en) * 2006-05-23 2007-11-29 General Electric Company Airfoil and method for moisture removal and steam injection
US7422415B2 (en) 2006-05-23 2008-09-09 General Electric Company Airfoil and method for moisture removal and steam injection
US20100329853A1 (en) * 2009-06-30 2010-12-30 General Electric Company Moisture removal provisions for steam turbine
CN102128060A (en) * 2011-04-28 2011-07-20 武汉大学 Superhydrophobic hollow dehumidifying stationary blade
JP2012241607A (en) * 2011-05-19 2012-12-10 Toshiba Corp Steam turbine
EP2604801A1 (en) * 2011-12-12 2013-06-19 Nuovo Pignone S.p.A. Brazed steam turbine guide vane module
ITCO20110060A1 (en) * 2011-12-12 2013-06-13 Nuovo Pignone Spa STEAM TURBINE, PALLET AND METHOD
CN103161512A (en) * 2011-12-12 2013-06-19 诺沃皮尼奥内有限公司 Steam turbine, blade, and method
KR20130066537A (en) * 2011-12-12 2013-06-20 누보 피그노네 에스피에이 Steam turbine, blade, and method
JP2013122246A (en) * 2011-12-12 2013-06-20 Nuovo Pignone Spa Steam turbine, blade, and method
RU2631852C2 (en) * 2011-12-12 2017-09-26 Нуово Пиньоне С.п.А. Stationary blading for steam turbine, multistage steam turbine and method for manufacturing blade unit
US8998571B2 (en) 2012-01-05 2015-04-07 General Electric Company Slotted turbine airfoil
US9359913B2 (en) 2013-02-27 2016-06-07 General Electric Company Steam turbine inner shell assembly with common grooves
JP2015068325A (en) * 2013-09-30 2015-04-13 株式会社東芝 Water droplet removing device for steam turbine
JP2017502188A (en) * 2013-10-23 2017-01-19 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータNuovo Pignone S.R.L. Method for manufacturing a steam turbine stage
US11333029B2 (en) 2013-10-23 2022-05-17 Nuovo Pignone Srl Method for manufacturing a stage of a steam turbine
US20160169015A1 (en) * 2014-12-15 2016-06-16 Mitsubishi Hitachi Power Systems, Ltd. Steam Turbine Stationary Blade
US10132178B2 (en) * 2014-12-15 2018-11-20 Mitsubishi Hitachi Power Systems, Ltd. Steam turbine stationary blade

Similar Documents

Publication Publication Date Title
US5573370A (en) Steam turbine
US3690786A (en) Low pressure end diffuser for axial flow elastic fluid turbines
US3274757A (en) Combination gas turbine and dust separator
US3876330A (en) Rotor blades for fluid flow machines
US4581048A (en) High-speed water separator
US3301529A (en) Steam turbines
JPH0250320B2 (en)
RU2058494C1 (en) Active steam turbine
US4534701A (en) Rotor or guide wheel of a turbine engine with shroud ring
KR880014227A (en) Partial arc high pressure steam turbine
US5167486A (en) Turbo-machine stage having reduced secondary losses
US4336039A (en) Geothermal turbine
GB1301002A (en) Improvements relating to fluid-flow machines
US4502838A (en) Solid wheel turbine
US3365124A (en) Compressor structure
US3120374A (en) Exhaust scroll for turbomachine
US3697191A (en) Erosion control in a steam turbine by moisture diversion
CA2054023A1 (en) Moisture drainage of honeycomb seals
US2399009A (en) Elastic fluid turbine
US3306576A (en) Arrangement for reducing steam condensation within steam turbines
US2362831A (en) Elastic fluid turbine
US3652182A (en) Turboseparator for polyphase fluids and turbine incorporating said turboseparator
RU2113595C1 (en) Steam turbine
US3724967A (en) Moisture removal device for a steam turbine
US3318077A (en) Device for removing water from the stages of steam turbines