EP1862642A2 - Pale de rotor d'une première phase d'un moteur à vapeur avec pied en forme de fourchette et ceinture de recouvrement - Google Patents

Pale de rotor d'une première phase d'un moteur à vapeur avec pied en forme de fourchette et ceinture de recouvrement Download PDF

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Publication number
EP1862642A2
EP1862642A2 EP07108516A EP07108516A EP1862642A2 EP 1862642 A2 EP1862642 A2 EP 1862642A2 EP 07108516 A EP07108516 A EP 07108516A EP 07108516 A EP07108516 A EP 07108516A EP 1862642 A2 EP1862642 A2 EP 1862642A2
Authority
EP
European Patent Office
Prior art keywords
blades
rotor
base portion
vapor
phase
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.)
Withdrawn
Application number
EP07108516A
Other languages
German (de)
English (en)
Other versions
EP1862642A3 (fr
Inventor
Carlo Cortese
Paolo Bendinelli
Vincenzo Vecchiarino
Fabio Valeri
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.)
Nuovo Pignone SpA
Original Assignee
Nuovo Pignone SpA
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 Nuovo Pignone SpA filed Critical Nuovo Pignone SpA
Publication of EP1862642A2 publication Critical patent/EP1862642A2/fr
Publication of EP1862642A3 publication Critical patent/EP1862642A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/31—Application in turbines in steam turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking

Definitions

  • the present invention relates generally to a rotor for traction engines such as turbines and, more specifically, to a first phase, or action phase, of a rotor of a vapor turbine.
  • a vapor turbine is a rotary machine which exploits the thermal energy of pressurized vapor for converting it to useful mechanical energy. This energy transformation takes place with intermediate transformation into kinetic energy.
  • All the phases of a vapor turbine consist of two essential organs: a distributor, in which the thermal energy is either totally or partially converted into kinetic energy, and a disk wheel, in which the residual thermal energy contained in the vapor is converted into kinetic energy and it is then all transferred into mechanical energy which can be used at the shaft.
  • stator blades or nozzles
  • rotor blades are moveable and are integral with the shaft.
  • stator the fixed parts in contact with the vapor
  • rotor the unit consisting of the shaft and parts integral therewith
  • reaction The phases are characterized by the mode with which the vapor yields its energy to the shaft, and on the basis of this are called “action” or “reaction”.
  • reaction phases In order to optimize the performances and costs, action and reaction phases can be found in a single vapor turbine.
  • the action step consists of fixed nozzles which cause the expansion of the vapor, creating high-velocity jets and kinetic energy, with a strongly angular direction with respect to the axis of the machine.
  • the jets meet the rotor blades, they considerably vary the direction as a result of the specific concave profile, and the vapor yields part of its kinetic energy in the form of mechanical rotation energy to the shaft.
  • This phenomenon can cause a lack of contact between adjacent blades and consequently excessive vibrations of the blades themselves which, under resonance conditions, can cause the cracking and consequent breakage of the blades.
  • An objective of various aspects of the present invention is therefore to overcome the above drawback, by providing a rotor for vapor turbines which avoids or in any case reduces the breakage of blades due to the use of wet vapor and, at the same time, which allows a high aerodynamic efficiency.
  • Each sector 10 comprises a varying number of blades 12 arranged circumferentially on the rotor.
  • the blades 12 are grouped into sectors 10 of four blades 12 each to form a rotor equipped with a total of hundred-and-twelve blades divided into twenty-eight sectors.
  • each blade 12 comprises a first concave surface 14, which is pressurized for the action of the vapor, and a second convex surface 16, which, on the contrary, is in depression and which is opposite the first surface 14.
  • the two concave 14 and convex 16 surfaces are continuous and connected to each other, and together form the overall aerodynamic profile, or side, of the blade 12 (figure 4).
  • a base portion 18, commonly called “foot”, of the blades 12 there is therefore a connecting joint 20 with the above aerodynamic profile of each blade 12, said base portion 18 being formed in a single piece with the blades 12 and being suitable for being fixed to the main body or disk 22 of the rotor of a vapor turbine.
  • a covering belt 24 is also envisaged, also called “top” of the blades 12, which form an outer ring for the rotor.
  • the jets of vapor coming from the fixed nozzles are directed onto the concave surface 14 of the blades 12, between the base portion 18 and the covering belt 24, to start the movement of the rotor.
  • each blade 12 has, on its contact portion with the covering belt 24, one or more pins 26 (figure 2) which are inserted in corresponding holes situated on the covering belt 24 itself, said pins 26 then being riveted after insertion in the above holes to effect the definitive coupling between the covering belt 24 and the blades 12.
  • the coupling between the base portion 18 of the blades 12 and the disk 22 of the rotor is effected by "fork" insertion in the radial direction of the rotor itself.
  • the rotor of a first phase of a vapor turbine achieves the objective specified above of reducing the breakages of the blades, due in particular to the use of wet vapor, by means of a series of expedients which at the same time do not jeopardize the aerodynamic efficiency of the turbine as a whole.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)
EP07108516A 2006-05-31 2007-05-21 Pale de rotor d'une première phase d'un moteur à vapeur avec pied en forme de fourchette et ceinture de recouvrement Withdrawn EP1862642A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT001064A ITMI20061064A1 (it) 2006-05-31 2006-05-31 PALA ROTORICA DI UN PRIMO STADIO DI UNA TURBINA A VAèPORE CON PIEDE A FORCHETTA E NASTRO DI COPERTURA

Publications (2)

Publication Number Publication Date
EP1862642A2 true EP1862642A2 (fr) 2007-12-05
EP1862642A3 EP1862642A3 (fr) 2009-03-25

Family

ID=38457565

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07108516A Withdrawn EP1862642A3 (fr) 2006-05-31 2007-05-21 Pale de rotor d'une première phase d'un moteur à vapeur avec pied en forme de fourchette et ceinture de recouvrement

Country Status (6)

Country Link
US (1) US20080044286A1 (fr)
EP (1) EP1862642A3 (fr)
JP (1) JP2007321762A (fr)
KR (1) KR20070115704A (fr)
CN (1) CN101082287A (fr)
IT (1) ITMI20061064A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010000228A2 (fr) * 2008-07-04 2010-01-07 Man Turbo Ag Aube et turbomachine pourvue d'une aube

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101114534B1 (ko) * 2009-08-14 2012-02-27 두산중공업 주식회사 핑거형 버켓의 조립방법
EP2690254B1 (fr) 2012-07-27 2017-04-26 General Electric Technology GmbH Fixations de pied de pale de rotor de turbine

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5299915A (en) * 1992-07-15 1994-04-05 General Electric Corporation Bucket for the last stage of a steam turbine
EP1331362A2 (fr) * 2002-01-28 2003-07-30 Kabushiki Kaisha Toshiba Turbine à vapeur géothermique

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4066384A (en) * 1975-07-18 1978-01-03 Westinghouse Electric Corporation Turbine rotor blade having integral tenon thereon and split shroud ring associated therewith
US5238368A (en) * 1991-01-16 1993-08-24 Ortolano Ralph J Converting grouped blading to equivalent integral covered blading
US6341941B1 (en) * 1997-09-05 2002-01-29 Hitachi, Ltd. Steam turbine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5299915A (en) * 1992-07-15 1994-04-05 General Electric Corporation Bucket for the last stage of a steam turbine
EP1331362A2 (fr) * 2002-01-28 2003-07-30 Kabushiki Kaisha Toshiba Turbine à vapeur géothermique

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010000228A2 (fr) * 2008-07-04 2010-01-07 Man Turbo Ag Aube et turbomachine pourvue d'une aube
WO2010000228A3 (fr) * 2008-07-04 2010-12-29 Man Diesel & Turbo Se Aube et turbomachine pourvue d'une aube
US8974187B2 (en) 2008-07-04 2015-03-10 Man Diesel & Turbo Se Rotor blade and flow engine comprising a rotor blade

Also Published As

Publication number Publication date
ITMI20061064A1 (it) 2007-12-01
US20080044286A1 (en) 2008-02-21
CN101082287A (zh) 2007-12-05
JP2007321762A (ja) 2007-12-13
KR20070115704A (ko) 2007-12-06
EP1862642A3 (fr) 2009-03-25

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