ES2123700T3 - Rejilla de paletas con bordes delanteros en forma de flecha. - Google Patents

Rejilla de paletas con bordes delanteros en forma de flecha.

Info

Publication number
ES2123700T3
ES2123700T3 ES94119705T ES94119705T ES2123700T3 ES 2123700 T3 ES2123700 T3 ES 2123700T3 ES 94119705 T ES94119705 T ES 94119705T ES 94119705 T ES94119705 T ES 94119705T ES 2123700 T3 ES2123700 T3 ES 2123700T3
Authority
ES
Spain
Prior art keywords
pallet
area
arrow
foot
axial
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.)
Expired - Lifetime
Application number
ES94119705T
Other languages
English (en)
Inventor
Reinhard Dr Niehus
Norbert Hubner
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of ES2123700T3 publication Critical patent/ES2123700T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Chain Conveyers (AREA)

Abstract

UNA REJILLA 2,3 DE PALETA PARA MAQUINA DE CORRIENTE AXIAL MUESTRA PALETAS 4,5, QUE DISPONEN DE FORMA DE FLECHA AXIAL, EN LA ZONA DE LAS PUNTAS 17,13 DE LA HOJA DE PALETA Y DEL PIE DE PALETA DE FORMA POSITIVA. LOS BORDE 11 DELANTEROS DE LA PALETA EN LA ZONA DE LA PUNTA 17 DE LA HOJA DE PALETA Y DEL PIE 13 DE ESTA PALETA MUESTRAN UN TRAMO QUE DISCURRE EN LINEA RECTA Y EN CONEXION CON EL, CON RESPECTO A LA ZONA MEDIA DE LA PALETA, UN TRAMO QUE DISCURRE DE FORMA DOBLADA. LA DISPOSICION DE FLECHA EN LA DIRECCION Z AXIAL PUEDE SER SOPORTADO POR MEDIO DE UNA CURVATURA DE LAS PALETAS 4,5 EN LA DIRECCION ..OMEGA.. PERIMETRICA. POR MOTIVOS DEL DESARROLLO EN FORMA DE FLECHA, EN LINEA RECTA, DE LOS BORDES 11 DELANTEROS DE LA PALETA EN LA ZONA DE LA PUNTA 7 DE HOJA DE PALETA Y DEL PIE 13 DE LA PALETA RESULTA UN INFLUJO DE LA CORRIENTE SECUNDARIA, DE FORMA QUE SE PERMITE UNA MEJORA DEL RENDIMIENTO DE ETAPA TANTO EN LA ZONA DE PALETA, COMO TAMBIEN EN LA REJILLA 2 O 3 DE LA PALETA DE CONDUCCION.
ES94119705T 1993-12-23 1994-12-14 Rejilla de paletas con bordes delanteros en forma de flecha. Expired - Lifetime ES2123700T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19934344189 DE4344189C1 (de) 1993-12-23 1993-12-23 Axial-Schaufelgitter mit gepfeilten Schaufelvorderkanten

Publications (1)

Publication Number Publication Date
ES2123700T3 true ES2123700T3 (es) 1999-01-16

Family

ID=6506022

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94119705T Expired - Lifetime ES2123700T3 (es) 1993-12-23 1994-12-14 Rejilla de paletas con bordes delanteros en forma de flecha.

Country Status (3)

Country Link
EP (1) EP0661413B1 (es)
DE (1) DE4344189C1 (es)
ES (1) ES2123700T3 (es)

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WO2006060001A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
US8468795B2 (en) 2004-12-01 2013-06-25 United Technologies Corporation Diffuser aspiration for a tip turbine engine
WO2006059996A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
EP1710397B1 (en) 2005-03-31 2014-06-11 Kabushiki Kaisha Toshiba Bowed nozzle vane
US7510371B2 (en) * 2005-06-06 2009-03-31 General Electric Company Forward tilted turbine nozzle
US7513102B2 (en) * 2005-06-06 2009-04-07 General Electric Company Integrated counterrotating turbofan
DE102005042115A1 (de) 2005-09-05 2007-03-08 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit blockweise definierter Profilskelettlinie
DE102005060699A1 (de) 2005-12-19 2007-06-21 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Verstellstator
JP4719038B2 (ja) * 2006-03-14 2011-07-06 三菱重工業株式会社 軸流流体機械用翼
US7726937B2 (en) * 2006-09-12 2010-06-01 United Technologies Corporation Turbine engine compressor vanes
DE102006055869A1 (de) 2006-11-23 2008-05-29 Rolls-Royce Deutschland Ltd & Co Kg Schaufelblattdesign für die Lauf- und Leitschaufeln einer Turbomaschine
DE102007020476A1 (de) * 2007-04-27 2008-11-06 Rolls-Royce Deutschland Ltd & Co Kg Vorderkantenverlauf für Turbomaschinenkomponenten
FR2924958B1 (fr) * 2007-12-14 2012-08-24 Snecma Aube de turbomachine realisee de fonderie avec un engraissement local de la section de la pale
US8075259B2 (en) * 2009-02-13 2011-12-13 United Technologies Corporation Turbine vane airfoil with turning flow and axial/circumferential trailing edge configuration
EP2441918A1 (en) 2010-10-18 2012-04-18 Siemens Aktiengesellschaft Gas turbine annular diffuser
ITCO20120059A1 (it) * 2012-12-13 2014-06-14 Nuovo Pignone Srl Metodi per produrre pale cave sagomate in 3d di turbomacchine mediante produzione additiva, pale cave di turbomacchina e turbomacchine
EP2824277B1 (de) * 2013-07-12 2016-03-23 MTU Aero Engines GmbH Gasturbinenstufe
EP3108103B1 (en) 2014-02-19 2023-09-27 Raytheon Technologies Corporation Fan blade for a gas turbine engine
EP3108101B1 (en) 2014-02-19 2022-04-20 Raytheon Technologies Corporation Gas turbine engine airfoil
US10557477B2 (en) 2014-02-19 2020-02-11 United Technologies Corporation Gas turbine engine airfoil
US10590775B2 (en) 2014-02-19 2020-03-17 United Technologies Corporation Gas turbine engine airfoil
WO2015126450A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP4509698A3 (en) 2014-02-19 2025-05-28 RTX Corporation Gas turbine engine airfoil
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
EP3108116B1 (en) 2014-02-19 2024-01-17 RTX Corporation Gas turbine engine
EP4279706A3 (en) 2014-02-19 2024-02-28 RTX Corporation Turbofan engine with geared architecture and lpc blade airfoils
EP3108104B1 (en) 2014-02-19 2019-06-12 United Technologies Corporation Gas turbine engine airfoil
EP3108113A4 (en) 2014-02-19 2017-03-15 United Technologies Corporation Gas turbine engine airfoil
WO2015127032A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015126715A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108122B1 (en) 2014-02-19 2023-09-20 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
EP3108109B1 (en) * 2014-02-19 2023-09-13 Raytheon Technologies Corporation Gas turbine engine fan blade
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
US10495106B2 (en) 2014-02-19 2019-12-03 United Technologies Corporation Gas turbine engine airfoil
US9599064B2 (en) 2014-02-19 2017-03-21 United Technologies Corporation Gas turbine engine airfoil
EP3108100B1 (en) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Gas turbine engine fan blade
WO2015175045A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015175051A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3108106B1 (en) 2014-02-19 2022-05-04 Raytheon Technologies Corporation Gas turbine engine airfoil
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ES2717801T3 (es) 2015-10-26 2019-06-25 MTU Aero Engines AG Alabe móvil
DE102015224151B4 (de) * 2015-12-03 2025-12-11 MTU Aero Engines AG Laufschaufel für eine Gasturbine und Gasturbine
US11220910B2 (en) * 2019-07-26 2022-01-11 Pratt & Whitney Canada Corp. Compressor stator
PL3816397T3 (pl) * 2019-10-31 2023-06-19 General Electric Company Łopatki turbiny o kontrolowanym przepływie

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Also Published As

Publication number Publication date
EP0661413B1 (de) 1998-08-26
DE4344189C1 (de) 1995-08-03
EP0661413A1 (de) 1995-07-05

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