GB2245661A - Turbine balancing system - Google Patents
Turbine balancing system Download PDFInfo
- 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
Links
- 238000013500 data storage Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000013518 transcription Methods 0.000 description 1
- 230000035897 transcription Effects 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01G—WEIGHING
- G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
- G01G19/40—Weighing 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
- G01G19/413—Weighing 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
- G01G19/414—Weighing 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
- G01G19/415—Weighing 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
-
- 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
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/30—Compensating imbalance
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/30—Compensating imbalance
- G01M1/36—Compensating 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.
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)
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)
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 |
-
1990
- 1990-07-03 GB GB9014755A patent/GB2245661B/en not_active Expired - Fee Related
Patent Citations (1)
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)
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 |