[go: up one dir, main page]

GB2245661A - Turbine balancing system - Google Patents

Turbine balancing system Download PDF

Info

Publication number
GB2245661A
GB2245661A GB9014755A GB9014755A GB2245661A GB 2245661 A GB2245661 A GB 2245661A GB 9014755 A GB9014755 A GB 9014755A GB 9014755 A GB9014755 A GB 9014755A GB 2245661 A GB2245661 A GB 2245661A
Authority
GB
United Kingdom
Prior art keywords
turbine
blades
processor
balancing system
disc
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.)
Granted
Application number
GB9014755A
Other versions
GB9014755D0 (en
GB2245661B (en
Inventor
Andrew Keith Wilson
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB9014755A priority Critical patent/GB2245661B/en
Publication of GB9014755D0 publication Critical patent/GB9014755D0/en
Publication of GB2245661A publication Critical patent/GB2245661A/en
Application granted granted Critical
Publication of GB2245661B publication Critical patent/GB2245661B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01GWEIGHING
    • G01G19/00Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
    • G01G19/40Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups with provisions for indicating, recording, or computing price or other quantities dependent on the weight
    • G01G19/413Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups with provisions for indicating, recording, or computing price or other quantities dependent on the weight using electromechanical or electronic computing means
    • G01G19/414Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups with provisions for indicating, recording, or computing price or other quantities dependent on the weight using electromechanical or electronic computing means using electronic computing means only
    • G01G19/415Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups with provisions for indicating, recording, or computing price or other quantities dependent on the weight using electromechanical or electronic computing means using electronic computing means only combined with recording means
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/027Arrangements for balancing
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/30Compensating imbalance
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00Testing static or dynamic balance of machines or structures
    • G01M1/30Compensating imbalance
    • G01M1/36Compensating imbalance by adjusting position of masses built-in the body to be tested

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Mathematical Physics (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Balance (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A turbine balancing system uses a set of deadweighing scales 10 providing a mass readout signal directly to a computer 12 which stores them in memory 12A. When all of the blades for a turbine have been weighed the computer calculates the positions they must be placed in on the turbine disc in order to produce a balanced turbine. The information is supplied to a printer 14 or a VDU. The computer 12 can be supplied initially via a keyboard 13 or a bar code reader with data representing the amount by which the turbine disc is out of balance. <IMAGE>

Description

TURBINE BALANCING SYSTEM This invention relates to a turbine balancing system, particularly for balancing a gas turbine.
In gas turbines it is necessary to ensure that the turbine is correctly balanced. This can be done by attaching balance weights to the turbine. However, in gas turbines comprising a central disc and a plurality of separate turbine blades secured to the outer edge of the disc there are unavoidable random variations in the weight and centre of gravity of the blades due to manufacturing tolerances and it is generally possible to arrange the positions of the blades around the disc so that these variations interact to balance the turbine, so avoiding the need to use separate balance weights.
However, balancing the turbine in this way is a time consuming task requiring expensive equipment.
Referring to figure 1,in order to balance a turbine a set of turbine blades 1 are individually weighed and their weights recorded, generally by being written on the blade. The blades 1 are then laid out in order of weight as shown in figure 1, where H is the heaviest blade, H2 the next heaviest and so on until Hnt the lightest blade is reached, 'n' being the number of blades on the turbine. A turbine can have 78 or more blades 1, so these are not trivial tasks, they require a large amount of time and there is considerable scope for error.
The blades 1 are then assembled on a turbine disc 2 in an order based on their relative weights. The heaviest blade H1 is attached first, then the second heaviest blade H2 is attached opposite H1. The lightest blade is then attached adjacent to H1 in the clockwise direction and the second lightest blade Hun 1 is attached adjacent to H2 in the clockwise direction. The third and fourth heaviest blades, H3 and H4 are then attached 4 H and H res adjacent Hn and Hn 1 respectively and the third and fourth lightest blades Hn~2 and Hn~3 are attached adjacent H3 and H4. This attachment sequence is followed around the whole of the disc 2.
The assembled turbine is then placed on a balance machine and checked by rotating it at speed and measuring the forces produced by any offset of the centre of mass of the turbine from its intended axis of rotation. The balance machine will inform the assembler of the direction and size of the out of balance vector.
If this vector is larger than the acceptable limit some of the blades must be exchanged and the turbine placed on the balance machine again. The assembler must use his experience to decide which blades to exchange in order to reduce the out of balance vector to an acceptable level and it may take a number of such exchanges to do this.
In some cases it is possible to simply remove and exchange two turbine blades without taking the turbine off the balance machine, but it is often necessary, especially in turbines with interlocking blades, to remove the turbine from the balance machine and place it on a special jig before any blades can be removed.
Balance machines are very large and expensive pieces of equipment so turbine balancing can only be carried out at relatively small number of fixed instilations.
In many cases it is necessary to send turbines needing blade replacement back to the manufacturer in another country simply because the user does not have turbine balancing facilities.
It has been proposed that turbine balancing could be carried out by measuring the moments of each blade individually and then calculating which arrangement of blades will produce an acceptable resultant moment.
Although this overcomes the need for a balance machine it requires the use of a moment measuring machine, which is again expensive and requires careful setting in position.
This invention was intended to produce a turbine balancing system at least partially overcoming these problems.
This invention provides a turbine balancing system comprising a set of deadweighing scales arranged to supply signals describing the mass placed on the scales to a processor, the processor being linked to a memory device and a data output device and programmed so that when a plurality of turbine blades are placed one after another on the scales signals describing their mass values are stored in the memory device until a specific number of blades have been weighed, whereupon the processor calculates the positions in which the blades must be placed on a turbine disc to produce a balanced turbine and then reads out this information on the data output device.
It has been realised that in many turbines the variation in the position of the centre of gravity of the turbine blades is not significant and only the variations in the blade mass need to be taken into account in order to balance the turbine. As a result the use of a moment measuring system is unnecessary and the task of calculating the necessary blade positions can be simplified. An integrated system in which deadweighing scales supply mass data directly to a processing system removes the possibility of data transcription errors causing an unbalanced turbine to be produced.
A turbine balancing system employing the invention will now be described by way of example only with reference to the accompanying diagrammatic figures in which; Figure 3 shows a turbine balancing system according to the invention.
Referring to figure 3 a turbine balancing system comprises a set of deadweighing scales 10 with a top pan 11. The scales 10 are linked to send data to a computer 12 including a data storage device 12A and a processor 12B. The computer 12 also receives data from a keyboard 13 and is connected to a printer 14.
In order to balance a turbine the number of blades on the turbine is entered into the computer 12 using the keyboard 13. Then each blade 15 in turn is weighed on the scales 10, which sends a signal giving the weight of the blade 15 to the computer 12 which stores it in the data storage device 12A, and then marked temporarily with an identifying number. The first blade 15 to be weighed being numbered 1, the second being numbered 2 and so on.
When a number of blades 15 equal to the number of blades on the turbine have been weighed the processor 12B uses the information in the data storage device 12A to calculate the sequence in which they must be placed on the disc to produce an acceptable resultant moment.
The computer does this by calculating the out of balance moment of the blades 15 in their initial random distribution. It then swaps two blades 15 at random and calculates the new moment, if it is higher it goes back to the original distribution, if lower it keeps the new diestribution. It then swaps another pair and repeats the process. This sequence is repeated until a distribution is found where no exchange of blades produces a lower moment.
This information is supplied to the user in the form of a printout from the printer 14 showing the number assigned to the blades 15 on weighing and their new order. For example, that working working clockwise, the first blade should be no 12, the second no 3 and so on.
If the turbine blades cannot be arranged to produce a balanced turbine the processor prints out a message saying this on the printer 14. A different selection of blades will then be made from the stock of blades.
If the disc itself is out of balance the amount and direction of its out of balance vector is permanently recorded on the disc. This data can then be supplied to the computer 12 at the start of the balancing operation, using the keyboard 13, and the processor 12B can calculate the necessary blade positions to produce an acceptable resultant moment including the effect of the unbalance of the disc 2. In this case the print out showing the sequence in which the blades 15 must be placed on the disc must also identify where on the disc the first blade in the sequence should be placed.
The numbers identifying the blades 15 could of course be placed on tags or labels attached to the blades 15 rather than being directly placed on the blades, similarly the direction and size of any out of balance vector produced by the disc could be contained in any document associated with the disc rather than being recorded on the disc itself.
The keyboard could be replaced with some other manual data inputting device, such as a bar code reader.
The printer could be replaced by any other data readout device, such as a VDU.

Claims (4)

1A turbine balancing system comprising a set of deadweighing scales arranged to supply signals describing the mass placed on the scales to a processor, the processor being linked to a memory device and a data output device and programmed so that when a plurality of turbine blades are placed one after another on the scales signals describing their mass values are stored in the memory device until a specific number of blades have been weighed, whereupon the processor calculates the positions in which the blades must be placed on a turbine disc to produce a balanced turbine and then reads out this information on the data output device.
2 A turbine balancing system as claimed in claim 1 in which the processor is also linked to a keyboard and the keyboard is used to tell the processor the specific number of blades to be weighed.
3 A turbine balancing system as claimed in claim 2 in which the keyboard is also used to supply the processor with data giving the out of balance vector of the turbine disc.
4 A turbine balancing system substantially as shown in or as described with reference to figure 3 of the accompanying drawings.
GB9014755A 1990-07-03 1990-07-03 Turbine balancing system Expired - Fee Related GB2245661B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9014755A GB2245661B (en) 1990-07-03 1990-07-03 Turbine balancing system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9014755A GB2245661B (en) 1990-07-03 1990-07-03 Turbine balancing system

Publications (3)

Publication Number Publication Date
GB9014755D0 GB9014755D0 (en) 1990-08-22
GB2245661A true GB2245661A (en) 1992-01-08
GB2245661B GB2245661B (en) 1993-12-15

Family

ID=10678603

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9014755A Expired - Fee Related GB2245661B (en) 1990-07-03 1990-07-03 Turbine balancing system

Country Status (1)

Country Link
GB (1) GB2245661B (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996029586A1 (en) * 1995-03-20 1996-09-26 United Technologies Corporation Method of balancing a bladed rotor
EP1382858A1 (en) * 2002-07-17 2004-01-21 Snecma Moteurs Distribution method for rotor blades of a turbomachine
EP1467063A1 (en) * 2003-04-08 2004-10-13 General Electric Company Methods and apparatus for assembling rotatable machines
GB2416228A (en) * 2004-07-13 2006-01-18 Gen Electric Method of determining optimum blade locations
GB2416227A (en) * 2004-07-13 2006-01-18 Gen Electric Method of determining optimum blade locations
EP1580543A3 (en) * 2004-03-26 2006-02-15 Hofmann Mess- und Auswuchttechnik GmbH & Co. KG Balancing device for compensating the unbalance of rotors of wind power installations
RU2317418C1 (en) * 2006-04-05 2008-02-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Method of arrangement of turbomachine rotor blades
RU2355889C2 (en) * 2007-07-25 2009-05-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Turbine unit rotor blade arrangement method
DE102009016123A1 (en) * 2009-04-03 2010-10-21 Schenck Rotec Gmbh Method for determining imbalance of rotor, involves attaching blades on carrier disk based on evaluation result, and determining imbalance of rotor by focal point scale, where blades are provided with barcode or matrix code
JP2014084839A (en) * 2012-10-26 2014-05-12 Toshiba Corp Low-speed balance method and low-speed balance device
RU2590983C2 (en) * 2014-10-30 2016-07-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Method of forming a set of turbo machine impeller blades
EP3572619A1 (en) * 2018-05-25 2019-11-27 Rolls-Royce plc Rotor blade arrangement
US10989227B2 (en) 2018-05-25 2021-04-27 Rolls-Royce Plc Rotor blade arrangement
US11111816B2 (en) 2018-05-25 2021-09-07 Rolls-Royce Plc Rotor blade arrangement

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4767272A (en) * 1987-10-14 1988-08-30 United Technologies Corporation Method for reducing blade tip variation of a bladed rotor

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996029586A1 (en) * 1995-03-20 1996-09-26 United Technologies Corporation Method of balancing a bladed rotor
RU2319841C2 (en) * 2002-07-17 2008-03-20 Снекма Моторс Method of arrangement of turbomachine rotor blades
EP1382858A1 (en) * 2002-07-17 2004-01-21 Snecma Moteurs Distribution method for rotor blades of a turbomachine
FR2842571A1 (en) * 2002-07-17 2004-01-23 Snecma Moteurs PROCESS FOR DISTRIBUTION OF TURBOMACHINE ROTOR BLADES
US7051436B2 (en) 2002-07-17 2006-05-30 Snecma Moteurs Method of distributing rotor blades in a turbomachine
EP1467063A1 (en) * 2003-04-08 2004-10-13 General Electric Company Methods and apparatus for assembling rotatable machines
US6908285B2 (en) 2003-04-08 2005-06-21 General Electric Company Methods and apparatus for assembling rotatable machines
CN100406678C (en) * 2003-04-08 2008-07-30 通用电气公司 Method and apparatus for assembling a rotatable machine
EP1580543A3 (en) * 2004-03-26 2006-02-15 Hofmann Mess- und Auswuchttechnik GmbH & Co. KG Balancing device for compensating the unbalance of rotors of wind power installations
GB2416227A (en) * 2004-07-13 2006-01-18 Gen Electric Method of determining optimum blade locations
GB2416228B (en) * 2004-07-13 2010-05-19 Gen Electric Methods and apparatus for assembling rotatable machines
US7090464B2 (en) 2004-07-13 2006-08-15 General Electric Company Methods and apparatus for assembling rotatable machines
GB2416228A (en) * 2004-07-13 2006-01-18 Gen Electric Method of determining optimum blade locations
US7416389B2 (en) 2004-07-13 2008-08-26 General Electric Company Methods and apparatus for assembling rotatable machines
GB2416227B (en) * 2004-07-13 2010-05-19 Gen Electric Methods and apparatus for assembling rotatable machines
RU2317418C1 (en) * 2006-04-05 2008-02-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Method of arrangement of turbomachine rotor blades
RU2355889C2 (en) * 2007-07-25 2009-05-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Turbine unit rotor blade arrangement method
DE102009016123A1 (en) * 2009-04-03 2010-10-21 Schenck Rotec Gmbh Method for determining imbalance of rotor, involves attaching blades on carrier disk based on evaluation result, and determining imbalance of rotor by focal point scale, where blades are provided with barcode or matrix code
DE102009016123B4 (en) * 2009-04-03 2014-07-17 Schenck Rotec Gmbh Method for assembling and determining the imbalance of rotors
JP2014084839A (en) * 2012-10-26 2014-05-12 Toshiba Corp Low-speed balance method and low-speed balance device
RU2590983C2 (en) * 2014-10-30 2016-07-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Method of forming a set of turbo machine impeller blades
EP3572619A1 (en) * 2018-05-25 2019-11-27 Rolls-Royce plc Rotor blade arrangement
US10954794B2 (en) 2018-05-25 2021-03-23 Rolls-Royce Plc Rotor blade arrangement
US10989227B2 (en) 2018-05-25 2021-04-27 Rolls-Royce Plc Rotor blade arrangement
US11111816B2 (en) 2018-05-25 2021-09-07 Rolls-Royce Plc Rotor blade arrangement

Also Published As

Publication number Publication date
GB9014755D0 (en) 1990-08-22
GB2245661B (en) 1993-12-15

Similar Documents

Publication Publication Date Title
GB2245661A (en) Turbine balancing system
CA1077623A (en) Remote postage meter charging system using an advanced microcomputerized postage meter
CA1196723A (en) Apparatus for providing interchangeable keyboard functions
US5072397A (en) Carrier management system enabling determination of charges with discounts
US7877223B2 (en) Method and apparatus for geometric rotor stacking and balancing
US5729459A (en) Carrier management system having a capability to determine weight based handling charges
EP0089190B1 (en) The production of descriptive labels for different items
CA2027772A1 (en) Method and apparatus for a mail processing system
US5726894A (en) Postage metering system including means for selecting postal processing services for a sheet and digitally printing thereon postal information pertaining to each selected postal processing service
DE102009016123B4 (en) Method for assembling and determining the imbalance of rotors
GB2027912A (en) Weighing apparatus
CA2054951A1 (en) Mail piece weight monitoring system and method
US5357629A (en) System for recording structured read only data table revisions and forming a directory to the latest revisions of table elements
CN101110093A (en) Crankshaft dynamic balance design method
Dancy et al. The initial imperfection data bank at the Delft University of Technology, part 2
US20180114374A1 (en) Method for Determining Fee For Sending a Mailing
US5079712A (en) Register setting arrangement for carrier management system
US1974A (en) Christopher edlvard dahpiitjr
JP2945204B2 (en) Printer
US2878677A (en) Static balancer for rotating parts
US673096A (en) Price-computing scale-beam.
Hodsman The Impact of new Technology on European Weighing Machine Regulations
JPH0656313B2 (en) Mixed combination weighing device
US221826A (en) Improvement in weighing apparatus
EP3767566A1 (en) Method and system for collecting batches of articles

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20010703