MX359777B - Montaje de rotor de compresor y sistema de nivelación para motor de turbina de gas. - Google Patents
Montaje de rotor de compresor y sistema de nivelación para motor de turbina de gas.Info
- Publication number
- MX359777B MX359777B MX2015005939A MX2015005939A MX359777B MX 359777 B MX359777 B MX 359777B MX 2015005939 A MX2015005939 A MX 2015005939A MX 2015005939 A MX2015005939 A MX 2015005939A MX 359777 B MX359777 B MX 359777B
- Authority
- MX
- Mexico
- Prior art keywords
- weldment
- aft
- balancing
- compressor rotor
- rotor assembly
- Prior art date
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
- 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
-
- 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
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
-
- 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
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
-
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/662—Balancing of rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Testing Of Balance (AREA)
Abstract
Un método para nivelar un montaje de rotor de compresor que incluye una soldadura frontal y una soldadura trasera que incluye la pre-nivelación de la soldadura trasera del montaje de rotor de compresor con discos de compresor antes de colocar los discos de compresor con palas de rotor de compresor instaladas de forma circunferencial. La pre-nivelación de la soldadura trasera incluye medir un equilibrio de rotación de la soldadura trasera. La pre-nivelación de la soldadura trasera también incluye determinar el número de pesos bajo plataforma en una ranura circunferencial de uno de los discos de compresor. La pre-nivelación de la soldadura trasera incluye además montar cada peso bajo plataforma en la ubicación deseada.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/684,056 US9404367B2 (en) | 2012-11-21 | 2012-11-21 | Gas turbine engine compressor rotor assembly and balancing system |
PCT/US2013/070943 WO2014081790A1 (en) | 2012-11-21 | 2013-11-20 | Gas turbine engine compressor rotor assembly and balancing system |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2015005939A MX2015005939A (es) | 2015-09-23 |
MX359777B true MX359777B (es) | 2018-10-09 |
Family
ID=50728111
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2015005939A MX359777B (es) | 2012-11-21 | 2013-11-20 | Montaje de rotor de compresor y sistema de nivelación para motor de turbina de gas. |
Country Status (6)
Country | Link |
---|---|
US (1) | US9404367B2 (es) |
CN (1) | CN204804885U (es) |
CA (1) | CA2891448A1 (es) |
MX (1) | MX359777B (es) |
RU (1) | RU2660981C2 (es) |
WO (1) | WO2014081790A1 (es) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9388697B2 (en) * | 2012-07-17 | 2016-07-12 | Solar Turbines Incorporated | First stage compressor disk configured for balancing the compressor rotor assembly |
US10544678B2 (en) | 2015-02-04 | 2020-01-28 | United Technologies Corporation | Gas turbine engine rotor disk balancing |
US10584599B2 (en) | 2017-07-14 | 2020-03-10 | United Technologies Corporation | Compressor rotor stack assembly for gas turbine engine |
US10669875B2 (en) * | 2018-03-28 | 2020-06-02 | Solar Turbines Incorporated | Cross key anti-rotation spacer |
US11976564B1 (en) | 2023-03-30 | 2024-05-07 | Rolls-Royce North American Technologies Inc. | Splined balance weight for rotating components in gas turbine engines |
US12018579B1 (en) | 2023-08-08 | 2024-06-25 | Rolls-Royce North American Technologies Inc. | Clocking balance weight rotor assembly for gas turbine engines |
US12018580B1 (en) | 2023-08-08 | 2024-06-25 | Rolls-Royce North American Technologies Inc. | Rotor assembly for gas turbine engines with replaceable balance weight pins |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU129431A1 (ru) * | 1950-08-11 | 1959-11-30 | В.С. Осадченко | Способ компенсации динамической неуравновешенности роторов турбин и компрессоров |
DE2002469C3 (de) * | 1970-01-21 | 1978-03-30 | Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen | Laufschaufelbefestigung in einer schwalbenschwanzförmigen Umfangsnut eines Läufers axial durchströmter Strömungsmaschinen, insbesondere Gasturbinenstrahltriebwerke |
US3888601A (en) * | 1974-05-23 | 1975-06-10 | Gen Electric | Turbomachine with balancing means |
FR2358545A1 (fr) | 1976-07-16 | 1978-02-10 | Snecma | Perfectionnements aux dispositifs d'equilibrage de rotors |
US4477226A (en) * | 1983-05-09 | 1984-10-16 | General Electric Company | Balance for rotating member |
JPS6185501A (ja) * | 1984-10-03 | 1986-05-01 | Ngk Insulators Ltd | セラミツクスロ−タ−のバランス修正方法並びにそれに用いられる修正治具 |
US4743165A (en) * | 1986-10-22 | 1988-05-10 | United Technologies Corporation | Drum rotors for gas turbine engines |
US4767272A (en) * | 1987-10-14 | 1988-08-30 | United Technologies Corporation | Method for reducing blade tip variation of a bladed rotor |
SE514159C2 (sv) | 1998-05-25 | 2001-01-15 | Abb Ab | Gasturbininrättning innefattande ett balanseringsorgan |
US6908285B2 (en) * | 2003-04-08 | 2005-06-21 | General Electric Company | Methods and apparatus for assembling rotatable machines |
US20050265846A1 (en) * | 2004-06-01 | 2005-12-01 | Przytulski James C | Balance assembly for rotary turbine component and method for installing and/or adjusting balance weight |
FR2896289B1 (fr) * | 2006-01-13 | 2008-03-28 | Snecma Sa | Masselotte d'equilibrage, disque de rotor en etant equipe, rotor et moteur d'aeronef les comportant |
FR2907498B1 (fr) | 2006-10-24 | 2009-01-23 | Snecma Sa | Systeme d'equilibrage pour rotor de turbomachine |
US7685876B2 (en) * | 2006-12-20 | 2010-03-30 | General Electric Company | Methods and systems for balancing a rotatable member |
US8186955B2 (en) * | 2007-11-08 | 2012-05-29 | General Electric Company | Rotating machine balancing member assembly including multiple interlocking balancing members |
US8342804B2 (en) * | 2008-09-30 | 2013-01-01 | Pratt & Whitney Canada Corp. | Rotor disc and method of balancing |
US8177487B2 (en) | 2009-05-04 | 2012-05-15 | General Electric Company | Rotary machine balance weights |
GB0908502D0 (en) * | 2009-05-19 | 2009-06-24 | Rolls Royce Plc | A balanced rotor for a turbine engine |
US8348616B2 (en) | 2009-06-16 | 2013-01-08 | General Electric Company | Trapped spring balance weight and rotor assembly |
EP2397651A1 (en) * | 2010-06-17 | 2011-12-21 | Siemens Aktiengesellschaft | Balance correction weight providing constant mass |
GB2481582A (en) * | 2010-06-28 | 2012-01-04 | Rolls Royce Plc | A method for predicting initial unbalance in a component such as a blisk |
-
2012
- 2012-11-21 US US13/684,056 patent/US9404367B2/en not_active Expired - Fee Related
-
2013
- 2013-11-20 CN CN201390000858.7U patent/CN204804885U/zh not_active Expired - Fee Related
- 2013-11-20 WO PCT/US2013/070943 patent/WO2014081790A1/en active Application Filing
- 2013-11-20 CA CA2891448A patent/CA2891448A1/en not_active Abandoned
- 2013-11-20 RU RU2015121819A patent/RU2660981C2/ru not_active IP Right Cessation
- 2013-11-20 MX MX2015005939A patent/MX359777B/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
WO2014081790A1 (en) | 2014-05-30 |
US9404367B2 (en) | 2016-08-02 |
RU2660981C2 (ru) | 2018-07-11 |
RU2015121819A (ru) | 2016-12-27 |
US20140140849A1 (en) | 2014-05-22 |
CN204804885U (zh) | 2015-11-25 |
MX2015005939A (es) | 2015-09-23 |
CA2891448A1 (en) | 2014-05-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MX359777B (es) | Montaje de rotor de compresor y sistema de nivelación para motor de turbina de gas. | |
WO2012087420A3 (en) | Method for balancing rotating assembly of gas turbine engine | |
GB201110141D0 (en) | A method of detecting shaft break | |
WO2013060420A3 (de) | Verfahren zur bestimmung einer mechanischen beschädigung eines rotorblatts einer windenergieanlage | |
GB201301604D0 (en) | System For Detecting An Impact On An Aircraft Engine Impeller Wheel | |
WO2014099634A3 (en) | Lightweight shrouded fan blade | |
EP2597292B8 (en) | Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings | |
IN2012DE00256A (es) | ||
IN2014DN10346A (es) | ||
EP3640434A3 (en) | Hybrid rotor disk assembly with ceramic matrix composites platform for a gas turbine engine | |
EP2620591B8 (en) | Gas turbine engine stator vane assembly with inner shroud | |
WO2012025434A3 (de) | Verfahren und detektierungsvorrichtung zum detektieren von fehlzündungen in einem verbrennungsmotor | |
EP2487335A3 (en) | Case with ballistic liner | |
MX2013011418A (es) | Corte de plataforma de paleta de turbina. | |
IN2015DN00295A (es) | ||
NZ610656A (en) | Method for operating a wind power plant | |
MX2014011945A (es) | Sistema de equilibrio de rotor de inercia dinamica pasiva para turbomaquinaria. | |
IN2014DE00775A (es) | ||
WO2015088623A3 (en) | Balanced rotating component for a gas powered engine | |
GB201302069D0 (en) | An Axisymmetric Part For An Aviation Turbine Engine Rotor | |
BR112012031972A2 (pt) | sistema hidroelétrico em um duto e método para manter as lâminas da turbina em um alojamento substancialmente livre de água | |
RU2012134278A (ru) | Турбоустановка | |
GB2519845B (en) | Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan | |
IN2014DN08863A (es) | ||
WO2014197031A3 (en) | Thermally conformable liner for reducing system level fan blade out loads |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant or registration |