EP2652270A1 - Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine - Google Patents

Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine

Info

Publication number
EP2652270A1
EP2652270A1 EP11807954.0A EP11807954A EP2652270A1 EP 2652270 A1 EP2652270 A1 EP 2652270A1 EP 11807954 A EP11807954 A EP 11807954A EP 2652270 A1 EP2652270 A1 EP 2652270A1
Authority
EP
European Patent Office
Prior art keywords
rotor
measuring device
distance measuring
distance
blades
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Withdrawn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
EP11807954.0A
Other languages
German (de)
English (en)
Inventor
Karsten Klein
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Priority to EP11807954.0A priority Critical patent/EP2652270A1/fr
Publication of EP2652270A1 publication Critical patent/EP2652270A1/fr
Withdrawn legal-status Critical Current

Links

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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/14—Testing gas-turbine engines or jet-propulsion engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B19/00—Single-purpose machines or devices for particular grinding operations not covered by any other main group
    • B24B19/14—Single-purpose machines or devices for particular grinding operations not covered by any other main group for grinding turbine blades, propeller blades or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B24—GRINDING; POLISHING
    • B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B49/00—Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation
    • B24B49/02—Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation according to the instantaneous size and required size of the workpiece acted upon, the measuring or gauging being continuous or intermittent
    • B24B49/04—Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation according to the instantaneous size and required size of the workpiece acted upon, the measuring or gauging being continuous or intermittent involving measurement of the workpiece at the place of grinding during grinding operation
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/02—Measuring arrangements characterised by the use of optical techniques for measuring length, width or thickness
    • G01B11/028—Measuring arrangements characterised by the use of optical techniques for measuring length, width or thickness by measuring lateral position of a boundary of the object
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/08—Measuring arrangements characterised by the use of optical techniques for measuring diameters
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/08—Measuring arrangements characterised by the use of optical techniques for measuring diameters
    • G01B11/12—Measuring arrangements characterised by the use of optical techniques for measuring diameters internal diameters
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/14—Measuring arrangements characterised by the use of optical techniques for measuring distance or clearance between spaced objects or spaced apertures
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/26—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B11/27—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/26—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B11/27—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • G01B11/272—Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes using photoelectric detection means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/22—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/22—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes
    • G01B21/24—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes for testing alignment of axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
    • G01B21/22—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes
    • G01B21/26—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring angles or tapers; for testing the alignment of axes for testing wheel alignment
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/30—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/30—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B7/305—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes for testing perpendicularity
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/30—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B7/31—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/30—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B7/31—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes
    • G01B7/312—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes for testing the alignment of axes for measuring eccentricity, i.e. lateral shift between two parallel axes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/30—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes
    • G01B7/315—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring angles or tapers; for testing the alignment of axes for testing wheel alignment
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/88—Lidar systems specially adapted for specific applications
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/34—Balancing of radial or axial forces on regenerative rotors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making

Definitions

  • the invention relates to a method for determining the diameter of a rotor equipped with blades of a turbomachine. It further relates to a measuring system for a rotor of a turbomachine.
  • Turbomachines generally include continuous fluid power machinery such as compressors, steam and gas turbines.
  • energy is converted from a hot combustion gas to kinetic energy which drives a ⁇ hand, a compressor connected upstream and on the other hand, typically a generator for generating electricity.
  • a gas turbine can also be used to power aircraft.
  • Gas turbines include on the one hand fixed vanes, which carry the air and gas flow, and located on the rotor of the gas turbine blades, which rotate around the axis of the flow ⁇ machine and form in the axial direction successively arranged blade rings.
  • the blades ting the axis of the turbomachine to a coaxially arranged inner wall, which thus the flow passage for the combustion gas defi ned ⁇ .
  • the distance between the body of the running ⁇ blade and the inner wall should be kept as low as possible in order to minimize the loss of efficiency by along the inner wall of the blades flowing past combustion gas.
  • the object of the invention is therefore to provide a method which allows a comparatively long life of the blade and at the same time a particularly high efficiency of Strö ⁇ tion machine.
  • This object is achieved according to the invention, by which is detected by ⁇ diameter of the rotor with the blades in ⁇ the rotor with the blade ring is set into a rotational movement, outside the region of the motion acting ⁇ felkranzes an associated thereto, arranged distance measuring ⁇ means the distance to the rotating on the distance measuring device rotating blade in the blade ring detected and the detected distance is used to determine the diameter of the rotor ⁇ sers.
  • the invention proceeds from the consideration that a comparatively long service life with a simultaneous optimization ⁇ tion efficiency zen by a controlled reduction in the minimum distance between inner wall and Laufschaufelspit- would be achievable.
  • this minimum distance is in particular ⁇ special, because the Laufschaufein when installed in the rotor in the cold state have a certain play that must be integrated into the corresponding tolerance models.
  • This game leads to a fluctuation in the diameter of the rotor with the built-in blades on the respective blade ring.
  • a distance measuring device associated therewith is arranged outside the region of the rotor blade ring, and the distance to the rotor blades of the rotor blade ring rotating past the distance measuring device is measured.
  • the absolute rotor diameter can be determined by calculation.
  • the rotor radius is of the known distance of the detected distance to subtrahie ⁇ ren.
  • a second distance measuring device associated therewith is arranged outside the region of the rotor blade ring.
  • a single distance measuring device capable ⁇ namely only to measure the distance of the blades to a fixed reference system having its reference to the fixed axis of the rotor but does not need to be known.
  • a third distance measuring device associated therewith is advantageously arranged outside the area of a second rotor blade ring, and the distance to the moving blades of the second rotor blade ring rotating past the third distance measuring device is measured.
  • DEVICES Such additional arrangement of one or more Abstandsmes- permits simultaneous as well as reliabil ⁇ SiGe determining the diameter in each axial portion of the rotor.
  • the respective distance measuring device is displaced in the axial direction of the rotor.
  • a displaceably arranged distance measuring device makes it possible to measure at different rotor blade rings in different axial regions of the engine without having to use a multiplicity of distance measuring devices.
  • a laser distance measuring device used in a particularly advantageous embodiment. This allows a particularly accurate measurement of the Ab ⁇ states, whereby the minimum distance of the inner wall to the Laufschaufein can be adjusted even more precisely.
  • the method is carried out in a balancing system and / or during balancing of the rotor.
  • balancing imbalances of the rotor are eliminated before being fed to final assembly in the turbine.
  • the rotor is set in rotation and measured corresponding imbalances.
  • This process in which the play of the rotor blade is eliminated by the rotation, can also be used in the manner of a double use for the use the written measure of the distance, so that here a particularly fast and economical process for determining the rotor diameter is achieved.
  • a minimum speed for the Rotati ⁇ onsterrorism during the execution of the measurement is given. This is chosen so that a game of blades reliably eliminating centrifugal force occurs and corre ⁇ sponding tolerances are excluded.
  • the minimum speed should be determined specifically based on the parameters of the rotor ⁇ .
  • the speed - at which the measurement is Runaway ⁇ leads - identical or at least almost identical to the rated speed of the rotor or even larger.
  • This has the advantage that, as in the intended use centrifugal force induced changes in length of components, especially in Turbi nen- and compressor blades and disks occur, which are taken into account in the determination of the absolute rotor diameter. If the blades of such blades are wound, even a centrifugal force, the diameter of the rotor influencing Entwindung occur, which is also taken into account in the determination and determination of the diameter of the inner wall.
  • ⁇ th rotor diameter of the inner wall diameter can be determined more accurately than before, so that radial From ⁇ stood dimensions can be achieved between blade tips and inner wall smaller than before.
  • the turbomachine thus designed can then achieve a better efficiency than bishe and stripping of blades on the inner wall due to a small in the design radial gap can be safely avoided.
  • the thus-detected diameter of the rotor is used before geous enough in the construction of the inner casing of the turbomachine.
  • the minimum distance can be reduced by the now significantly reduced tolerance in the rotor diameter. reduced diameter and it is achieved a higher efficiency.
  • a turbomachine with the Darge ⁇ presented method is constructed and comes in an advantageous embodiment in a power plant used.
  • the invention is achieved by the measuring system comprises a holding device for the rotor with a number of rotor blades forming blades, a balancing housing surrounding the rotor, further a Antriebsvor ⁇ direction, designed to move the rotor in one Rota ⁇ tion movement, and a distance measuring device, designed to measure the distance to the rotating past the distance measuring device blades of the blade ring.
  • the measuring system is able to determine the rotor diameter in conjunction with the distance between the sensor and the axis of the rotor.
  • the senor can be arranged on the inside of the balancing housing, which is structurally much simpler to design than inside the turbomachine or on a separate stand.
  • the distance between the sensor or sensor head and the rotor can also be substantially larger-for example a few decimetres-than in sensors known from the prior art, which are always used in the turbomachines for determining the radial gap. This facilitates the measurement setup and avoids costly mounting of the sensor.
  • Another advantage is that the sensor only has to withstand the temperatures that occur during balancing and not the operating temperatures of the gas turbine. This significantly increases the choice of possible sensors and measurement methods, and also allows the use of inexpensive sensors. Preferably then optical sensors are used.
  • a gas turbine 101 has a compressor 102 for combustion air, a combustion chamber 104 and a turbine unit 106 for driving the compressor 102 and a generator, not shown, or a work ⁇ machine on.
  • turbine unit 106 and compressor 102 are arranged on a common turbine shaft 108, also referred to as a turbine rotor, to which the generator or the working machine is also connected, and which is rotatably mounted about its center axis 109.
  • These units form the rotor of the gas turbine 101.
  • the combustion chamber 104 designed in the manner of an annular combustion chamber is provided with a number of burners 110 equipped for the combustion of a liquid or gaseous fuel.
  • the turbine unit 106 has a number of rotatable blades 112 connected to the turbine shaft 108.
  • the blades 112 are arranged in a ring on the turbine shaft 108 and thus form a number of blade ⁇ wreaths or rows.
  • the turbine unit 106 includes a number of stationary vanes 114 which are also annularly attached to a vane support 116 of the turbine unit 106 to form rows of vanes.
  • the blades 112 serve to drive the turbine shaft 108 by momentum transfer from the tur ⁇ binenech 106 flowing through the working medium M.
  • the vanes 114 serve to flow the working medium M between two seen in the flow direction of the working medium M consecutive blade rows or blade rings.
  • a successive pair of a ring of guide vanes 114, or a guide blade row and of a ring of blades 112 or a moving blade row is thereby ⁇ be also referred to as a turbine stage.
  • Each vane 114 has a platform 118 that is attached ⁇ arranged for fixing the respective guide vane 114 at a guide vane 116 of the turbine unit 106 as a wall element.
  • the platform 118 is a thermally relatively highly loaded component, which for the turbine unit forming the outer Begren ⁇ wetting of a hot-gas duct 106 by flowing working medium M.
  • Each rotor blade 112 is secured in an analogous manner via a designated also as a blade ⁇ designated platform 119 to the turbine shaft 108th
  • each ring segment 121 is arranged on a guide vane carrier ⁇ 1 the turbine unit 106,121 respectively.
  • the outer upper ⁇ surface of each ring segment 121 is also called the, exposed to the turbine unit 106 flowing through the working medium M and spaced in the radial direction from the outer end of the opposed blades 112 by a gap.
  • the arranged between adjacent rows of stator ring segments 121 serve in particular as Ab ⁇ cover elements that protect the inner housing in the guide blade carrier 116 or other housing-mounting components from thermal Sprintbe ⁇ claim by the turbine 106 flowing through the hot working medium M.
  • the combustion chamber 104 is configured in the embodiment as so genann ⁇ te annular combustion chamber, in which a plurality of spaced circumferentially around the turbine shaft 108 around burners 110 open into a common combustion chamber space.
  • the combustion chamber 104 is configured in its entirety as an annular structure, which is positioned around the turbine shaft 108 around.
  • the gap shown between the blades 112 on the one hand and the ring segments 121 and 118 on the other platforms, which together form the inner wall of the hot gas duct should be particularly low supported ⁇ th to increase the efficiency. This is made possible by precise determination of the diam ⁇ sers of the rotor.
  • the measurement of the rotor diameter takes place during the Aus ⁇ balancing operation.
  • the rotor with turbine shaft 108 and rotor blades 112 is arranged in a balancing housing 122, as shown schematically in FIG.
  • the rotor is set in rotational motion and rotated at the rated speed of the rotor.
  • This is Example ⁇ example in rotors of turbines used for power generation stationary at 3000 min -1 and at 3600 min -1, depending on the mains frequency. Meanwhile, corresponding imbalances are localized and compensated.
  • the rotational movement is thus performed at a predetermined minimum speed and thus also eliminates the play of the blades 112 in their attachment to the turbine shaft 108 this state take place, a particularly accurate measurement of diam ⁇ sers of the rotor.
  • the rotor diameter occurring during operation can be determined much more accurately than in a simulation.
  • the blades then sit without play in their retaining grooves and their blades experience meanwhile centrifugally induced elongations, which are detected by the Messsys ⁇ tem when determining the rotor diameter.
  • each distance measuring device 124 which are designed as laser distance measuring devices, are arranged in pairs opposite each other.
  • the Abstandsmessein ⁇ directions 124 are movable in the axial direction along the central axis 109 and can thus be assigned in pairs each to any blade ring.
  • the distance of each paired distance measuring device 124 has been precisely determined in advance, so that the diameter measurement of the rotor on each blade ring can be determined precisely by measuring the distance on both sides of the rotor 112.
  • the invention relates to a method for Ermitte ⁇ development of the diameter of a 114 equipped kitchens ⁇ ended with rotor blades of a turbomachine rotor.
  • a waste to arrange 124 in order subsequently to To measure distance to the 114 running on the distance measuring device over 124 Laufschaufelkranzes, which can be determined in conjunction with the distance between the sensor and the axis of the rotor, the rotor diameter.
  • the rotor diameter can then be taken into account in the construction and assembly of the turbomachine. With this knowledge, it is possible to minimize the gap between the inner wall and the blades 112 in the construction of the gas turbine 101 and thus increase the efficiency.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Electromagnetism (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Magnetically Actuated Valves (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles (114) d'une turbomachine. L'invention vise à obtenir une durée de vie comparativement élevée des aubes mobiles et simultanément un rendement particulièrement élevé de la turbomachine. A cet effet, le rotor muni de la couronne d'aubes mobiles est déplacé selon un mouvement de rotation et un dispositif de mesure de distance (124) associé à celle-ci est agencé à l'extérieur de la zone de la couronne d'aubes mobiles, afin de mesurer ensuite la distance par rapport aux aubes mobiles (114) de la couronne d'aubes mobiles tournant devant le dispositif de mesure de distance (124), le diamètre du rotor étant déterminé en relation avec la distance entre le capteur et l'axe du rotor. Le diamètre du rotor peut alors être pris en considération lors de la construction de la turbomachine.
EP11807954.0A 2011-02-22 2011-12-30 Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine Withdrawn EP2652270A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP11807954.0A EP2652270A1 (fr) 2011-02-22 2011-12-30 Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP11155389A EP2492452A1 (fr) 2011-02-22 2011-02-22 Procédé de construction d'une turbomachine
EP11807954.0A EP2652270A1 (fr) 2011-02-22 2011-12-30 Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine
PCT/EP2011/074285 WO2012113487A1 (fr) 2011-02-22 2011-12-30 Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine

Publications (1)

Publication Number Publication Date
EP2652270A1 true EP2652270A1 (fr) 2013-10-23

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Family Applications (2)

Application Number Title Priority Date Filing Date
EP11155389A Withdrawn EP2492452A1 (fr) 2011-02-22 2011-02-22 Procédé de construction d'une turbomachine
EP11807954.0A Withdrawn EP2652270A1 (fr) 2011-02-22 2011-12-30 Procédé de détermination du diamètre d'un rotor équipé d'aubes mobiles d'une turbomachine

Family Applications Before (1)

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EP11155389A Withdrawn EP2492452A1 (fr) 2011-02-22 2011-02-22 Procédé de construction d'une turbomachine

Country Status (7)

Country Link
US (1) US9671312B2 (fr)
EP (2) EP2492452A1 (fr)
JP (1) JP5638707B2 (fr)
CN (1) CN103384754B (fr)
BR (1) BR102012003750A8 (fr)
RU (1) RU2562928C2 (fr)
WO (1) WO2012113487A1 (fr)

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US9316493B2 (en) * 2013-12-13 2016-04-19 Siemens Energy, Inc. Method and apparatus for determining gas turbine dampening cone inner diameter
CN106091894B (zh) * 2016-06-30 2018-11-16 洛阳双瑞精铸钛业有限公司 一种透平机转子叶片的检测方法
CN107861060A (zh) * 2017-09-18 2018-03-30 大唐东北电力试验研究所有限公司 汽轮机转子扬度测量方法
CN108507482A (zh) * 2018-03-16 2018-09-07 中国航空工业集团公司北京航空精密机械研究所 一种测量涡轮转子的静动态叶尖回转半径的装置及方法
CN110068278A (zh) * 2019-04-22 2019-07-30 南京理工大学 基于fpga的非接触式光纤预制棒尺寸实时测量***及方法
CN112372451B (zh) * 2020-11-05 2022-11-08 中国航发哈尔滨东安发动机有限公司 一种高精度转子叶片及其轮缘尺寸控制方法
CN114001689B (zh) * 2021-11-10 2024-02-02 中国航发南方工业有限公司 航空发动机转子轴向尺寸测量装置及测量方法

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Also Published As

Publication number Publication date
BR102012003750A8 (pt) 2021-04-13
CN103384754A (zh) 2013-11-06
US9671312B2 (en) 2017-06-06
CN103384754B (zh) 2016-02-10
BR102012003750A2 (pt) 2015-01-27
RU2562928C2 (ru) 2015-09-10
RU2013142787A (ru) 2015-03-27
WO2012113487A1 (fr) 2012-08-30
EP2492452A1 (fr) 2012-08-29
JP2014506972A (ja) 2014-03-20
JP5638707B2 (ja) 2014-12-10
US20130330173A1 (en) 2013-12-12

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