BR112014005116B8 - Método para perfilar uma lâmina de substituição como uma parte de substituição para uma lâmina antiga para uma máquina de fluxo axial e lâmina de compressor - Google Patents

Método para perfilar uma lâmina de substituição como uma parte de substituição para uma lâmina antiga para uma máquina de fluxo axial e lâmina de compressor

Info

Publication number
BR112014005116B8
BR112014005116B8 BR112014005116A BR112014005116A BR112014005116B8 BR 112014005116 B8 BR112014005116 B8 BR 112014005116B8 BR 112014005116 A BR112014005116 A BR 112014005116A BR 112014005116 A BR112014005116 A BR 112014005116A BR 112014005116 B8 BR112014005116 B8 BR 112014005116B8
Authority
BR
Brazil
Prior art keywords
blade
replacement
airfoil
old
region
Prior art date
Application number
BR112014005116A
Other languages
English (en)
Other versions
BR112014005116A2 (pt
BR112014005116B1 (pt
Inventor
Cornelius Christian
Matthias Torsten
Original Assignee
Siemens Ag
Siemens Energy Global Gmbh & Co Kg
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, Siemens Energy Global Gmbh & Co Kg filed Critical Siemens Ag
Publication of BR112014005116A2 publication Critical patent/BR112014005116A2/pt
Publication of BR112014005116B1 publication Critical patent/BR112014005116B1/pt
Publication of BR112014005116B8 publication Critical patent/BR112014005116B8/pt

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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • B23P6/005—Repairing turbine components, e.g. moving or stationary blades, rotors using only replacement pieces of a particular form
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Architecture (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

MÉTODO PARA PERFILAR UMA LÂMINA DE SUBSTITUIÇÃO COMO UMA PARTE DE SUBSTITUIÇÃO PARA UMA LÂMINA ANTIGA PARA UMA TURBOMÁQUINA DE FLUXO AXIAL, LÂMINA DE ROTOR, LÂMINA DE ESTATOR, TURBINA A GÁS E LÂMINA DE COMPRESSOR. A presente invenção refere-se a um método para perfilar uma lâmina de substituição (1) para uma turbo máquina axial, que compreende as etapas de: medir a geometria do contorno do *cubo (5) e a geometria do contorno do *invólucro (6) do duto de fluxo da lâmina antiga (11), bem como a posição axial do centro de gravidade do aerofólio da lâmina antiga (11); definir a geometria do aerofólio de lâmina (2) da lâmina de substituição (1), o dito aerofólio de lâmina (2) tendo um varrimento retrógrado (14) na sua borda dianteira (7); definir uma região (21) do aerofólio de lâmina (2) que está próxima à montagem e na qual a influência positiva do varrimento retrógrado (14) no grau de eficiência de estágio é definida como baixa; e deslocar de modo axial a seção de aerofólio de lâmina de substituição (1) que é disposta fora dessa região (21) na direção a montante até que a posição axial do centro de gravidade do aerofólio de lâmina (2) da lâmina de substituição (1) coincida com aquela da lâmina antiga (11). Na região (21) a partir da seção de montagem lateral (5) para a seção de aerofólio de lâmina deslocada da lâmina de substituição (2), a borda dianteira (7) é inclinada a jusante em direção à montagem tal que o aerofólio de lâmina (2) tem um varrimento de transição (19) nessa região (21).
BR112014005116A 2011-09-09 2012-08-14 Método para perfilar uma lâmina de substituição como uma parte de substituição para uma lâmina antiga para uma máquina de fluxo axial e lâmina de compressor BR112014005116B8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP11180679.0 2011-09-09
EP11180679A EP2568114A1 (de) 2011-09-09 2011-09-09 Verfahren zum Profilieren einer Ersatzschaufel als ein Eratzteil für eine Altschaufel für eine Axialströmungsmaschine
PCT/EP2012/065842 WO2013034402A1 (de) 2011-09-09 2012-08-14 Verfahren zum profilieren einer ersatzschaufel als ein ersatzteil für eine altschaufel für eine axialströmungsmaschine

Publications (3)

Publication Number Publication Date
BR112014005116A2 BR112014005116A2 (pt) 2017-04-18
BR112014005116B1 BR112014005116B1 (pt) 2021-06-29
BR112014005116B8 true BR112014005116B8 (pt) 2023-04-25

Family

ID=46682835

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014005116A BR112014005116B8 (pt) 2011-09-09 2012-08-14 Método para perfilar uma lâmina de substituição como uma parte de substituição para uma lâmina antiga para uma máquina de fluxo axial e lâmina de compressor

Country Status (13)

Country Link
US (1) US9771803B2 (pt)
EP (2) EP2568114A1 (pt)
JP (1) JP6026537B2 (pt)
KR (1) KR101940353B1 (pt)
CN (1) CN103781995B (pt)
BR (1) BR112014005116B8 (pt)
CA (1) CA2848153C (pt)
HU (1) HUE029762T2 (pt)
MX (1) MX341606B (pt)
PL (1) PL2723988T3 (pt)
RU (1) RU2629110C2 (pt)
TW (1) TWI600824B (pt)
WO (1) WO2013034402A1 (pt)

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CN104429877B (zh) * 2014-11-04 2017-06-13 上海交通大学 可加热型家庭园艺蔬菜种植机
US10502220B2 (en) * 2016-07-22 2019-12-10 Solar Turbines Incorporated Method for improving turbine compressor performance
US10578125B2 (en) 2016-11-24 2020-03-03 Pratt & Whitney Canada Corp. Compressor stator vane with leading edge forward sweep
US20190106989A1 (en) * 2017-10-09 2019-04-11 United Technologies Corporation Gas turbine engine airfoil
KR102000281B1 (ko) 2017-10-11 2019-07-15 두산중공업 주식회사 압축기 및 이를 포함하는 가스 터빈
DE102018202888A1 (de) * 2018-02-26 2019-08-29 MTU Aero Engines AG Leitschaufelblatt für den Heissgaskanal einer Strömungsmaschine
CN109048220B (zh) * 2018-08-31 2021-03-23 中国航发贵州黎阳航空动力有限公司 一种更换飞机发动机叶片的方法
US11506059B2 (en) 2020-08-07 2022-11-22 Honeywell International Inc. Compressor impeller with partially swept leading edge surface

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DE1903642A1 (de) * 1969-01-20 1970-08-06 Bbc Sulzer Turbomaschinen Schaufelung fuer Rotoren von Axialverdichtern
US4585395A (en) 1983-12-12 1986-04-29 General Electric Company Gas turbine engine blade
FR2556409B1 (fr) * 1983-12-12 1991-07-12 Gen Electric Aube perfectionnee pour moteur a turbine a gaz et procede de fabrication
US5642985A (en) 1995-11-17 1997-07-01 United Technologies Corporation Swept turbomachinery blade
US6543997B2 (en) * 2001-07-13 2003-04-08 General Electric Co. Inlet guide vane for axial compressor
JP4045993B2 (ja) * 2003-03-28 2008-02-13 株式会社Ｉｈｉ ファン静翼、航空エンジン用ファン、及び航空エンジン
JP4664890B2 (ja) * 2006-11-02 2011-04-06 三菱重工業株式会社 遷音速翼及び軸流回転機
US7758306B2 (en) 2006-12-22 2010-07-20 General Electric Company Turbine assembly for a gas turbine engine and method of manufacturing the same
DE102008055824B4 (de) 2007-11-09 2016-08-11 Alstom Technology Ltd. Dampfturbine
US20090208339A1 (en) * 2008-02-15 2009-08-20 United Technologies Corporation Blade root stress relief
ITFO20080002A1 (it) * 2008-02-19 2008-05-20 Paolo Pietricola Pale rotoriche e statoriche con lean sinusoidale
RU2384750C1 (ru) 2008-11-11 2010-03-20 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Композитная облегченная лопатка преимущественно для вентиляторов авиационных двигателей
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US9790797B2 (en) * 2011-07-05 2017-10-17 United Technologies Corporation Subsonic swept fan blade

Also Published As

Publication number Publication date
KR20140067023A (ko) 2014-06-03
JP6026537B2 (ja) 2016-11-16
RU2629110C2 (ru) 2017-08-24
EP2723988A1 (de) 2014-04-30
PL2723988T3 (pl) 2016-10-31
BR112014005116A2 (pt) 2017-04-18
CN103781995A (zh) 2014-05-07
EP2723988B1 (de) 2016-04-20
TW201321595A (zh) 2013-06-01
US20140212282A1 (en) 2014-07-31
TWI600824B (zh) 2017-10-01
KR101940353B1 (ko) 2019-01-18
MX341606B (es) 2016-08-23
EP2568114A1 (de) 2013-03-13
US9771803B2 (en) 2017-09-26
JP2014526631A (ja) 2014-10-06
CA2848153C (en) 2019-12-31
HUE029762T2 (hu) 2017-04-28
BR112014005116B1 (pt) 2021-06-29
WO2013034402A1 (de) 2013-03-14
CA2848153A1 (en) 2013-03-14
RU2014113852A (ru) 2015-10-20
CN103781995B (zh) 2015-09-16
MX2014002748A (es) 2014-04-16

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 14/08/2012, OBSERVADAS AS CONDICOES LEGAIS.

B25G Requested change of headquarter approved

Owner name: SIEMENS AKTIENGESELLSCHAFT (DE)

B25A Requested transfer of rights approved

Owner name: SIEMENS ENERGY GLOBAL GMBH AND CO. KG (DE)