ES2063605R - - Google Patents

Info

Publication number
ES2063605R
ES2063605R ES9102341A ES9102341A ES2063605R ES 2063605 R ES2063605 R ES 2063605R ES 9102341 A ES9102341 A ES 9102341A ES 9102341 A ES9102341 A ES 9102341A ES 2063605 R ES2063605 R ES 2063605R
Authority
ES
Spain
Prior art keywords
attack
wing
aerodynamic wing
crown
departure
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
ES9102341A
Other languages
English (en)
Spanish (es)
Other versions
ES2063605A2 (es
ES2063605B1 (es
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 filed Critical
Publication of ES2063605A2 publication Critical patent/ES2063605A2/es
Publication of ES2063605R publication Critical patent/ES2063605R/es
Application granted granted Critical
Publication of ES2063605B1 publication Critical patent/ES2063605B1/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
    • 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
    • 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
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/05—Variable camber or chord length

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
ES09102341A 1990-10-24 1991-10-23 Alabes estacionarios perfeccionados para una hilera l-oc. Expired - Lifetime ES2063605B1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/603,332 US5211703A (en) 1990-10-24 1990-10-24 Stationary blade design for L-OC row

Publications (3)

Publication Number Publication Date
ES2063605A2 ES2063605A2 (es) 1995-01-01
ES2063605R true ES2063605R (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1997-01-01
ES2063605B1 ES2063605B1 (es) 1997-08-01

Family

ID=24414979

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09102341A Expired - Lifetime ES2063605B1 (es) 1990-10-24 1991-10-23 Alabes estacionarios perfeccionados para una hilera l-oc.

Country Status (6)

Country Link
US (1) US5211703A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPH04262002A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
KR (1) KR920008312A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA2054077A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
ES (1) ES2063605B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1251670B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5352092A (en) * 1993-11-24 1994-10-04 Westinghouse Electric Corporation Light weight steam turbine blade
US5524341A (en) * 1994-09-26 1996-06-11 Westinghouse Electric Corporation Method of making a row of mix-tuned turbomachine blades
US6682301B2 (en) 2001-10-05 2004-01-27 General Electric Company Reduced shock transonic airfoil
GB2384276A (en) * 2002-01-18 2003-07-23 Alstom Gas turbine low pressure stage
US7179058B2 (en) * 2004-03-21 2007-02-20 Bharat Heavy Electricals Limited Aerodynamically wide range applicable cylindrical blade profiles
US7175393B2 (en) * 2004-03-31 2007-02-13 Bharat Heavy Electricals Limited Transonic blade profiles
CN101460706B (zh) * 2006-03-31 2012-02-08 阿尔斯通技术有限公司 用于流体机械、尤其是用于蒸汽涡轮机的导向叶片
KR20100054804A (ko) * 2007-07-27 2010-05-25 안살도 에너지아 에스.피.에이 증기 터빈 스테이지
EP2295725A1 (de) * 2009-08-13 2011-03-16 Siemens Aktiengesellschaft Ströhmungsmaschine mit Dampfentnahme
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
EP3108121B1 (en) 2014-02-19 2023-09-06 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
EP4509698A3 (en) 2014-02-19 2025-05-28 RTX Corporation Gas turbine engine airfoil
WO2015126715A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US10393139B2 (en) 2014-02-19 2019-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108106B1 (en) 2014-02-19 2022-05-04 Raytheon Technologies Corporation Gas turbine engine airfoil
WO2015175052A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
US10502229B2 (en) 2014-02-19 2019-12-10 United Technologies Corporation Gas turbine engine airfoil
WO2015126774A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108120B1 (en) 2014-02-19 2021-03-31 Raytheon Technologies Corporation Gas turbine engine having a geared architecture and a specific fixed airfoil structure
WO2015175073A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3108116B1 (en) 2014-02-19 2024-01-17 RTX Corporation Gas turbine engine
EP3108102A4 (en) * 2014-02-19 2017-02-22 United Technologies Corporation Gas turbine engine airfoil
WO2015126451A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
WO2015126452A1 (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
EP3108115B8 (en) 2014-02-19 2023-11-08 RTX Corporation Turbofan engine with geared architecture and lpc blades
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
EP3108104B1 (en) 2014-02-19 2019-06-12 United Technologies Corporation Gas turbine engine airfoil
EP3108123B1 (en) * 2014-02-19 2023-10-04 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
EP3108105B1 (en) 2014-02-19 2021-05-12 Raytheon Technologies Corporation Gas turbine engine airfoil
EP3108109B1 (en) 2014-02-19 2023-09-13 Raytheon Technologies Corporation Gas turbine engine fan blade
US20160160874A1 (en) * 2014-12-04 2016-06-09 Solar Turbines Incorporated Airfoil for inlet guide vane (igv) of multistage compressor
KR101695138B1 (ko) * 2016-10-25 2017-01-10 두산중공업 주식회사 실링 수단을 갖는 로터 어셈블리 및 그를 포함하는 터빈 장치
US10408072B2 (en) * 2017-05-08 2019-09-10 General Electric Company Turbine nozzle airfoil profile

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US784670A (en) * 1904-03-19 1905-03-14 Hugh Francis Fullagar Fluid-pressure turbine.
US2299449A (en) * 1941-07-05 1942-10-20 Allis Chalmers Mfg Co Diaphragm construction
GB605361A (en) * 1945-01-19 1948-07-21 Sulzer Ag Improvements in or relating to multi-stage axial flow compressors
US2640679A (en) * 1950-03-21 1953-06-02 Gen Motors Corp Turbine or compressor stator ring
US2934259A (en) * 1956-06-18 1960-04-26 United Aircraft Corp Compressor blading
US3475108A (en) * 1968-02-14 1969-10-28 Siemens Ag Blade structure for turbines
JPS55123301A (en) * 1979-03-16 1980-09-22 Hitachi Ltd Turbine blade
JPS6229604A (ja) * 1985-07-30 1987-02-07 三浦　輝明 舗装坂道における滑り止め目地の施工法
US4741667A (en) * 1986-05-28 1988-05-03 United Technologies Corporation Stator vane
US4915581A (en) * 1989-01-03 1990-04-10 Westinghouse Electric Corp. Steam turbine with improved inner cylinder
US4900223A (en) * 1989-02-21 1990-02-13 Westinghouse Electric Corp Steam turbine
US4900230A (en) * 1989-04-27 1990-02-13 Westinghouse Electric Corp. Low pressure end blade for a low pressure steam turbine

Also Published As

Publication number Publication date
ITMI912671A1 (it) 1993-04-08
KR920008312A (ko) 1992-05-27
ITMI912671A0 (it) 1991-10-08
IT1251670B (it) 1995-05-19
CA2054077A1 (en) 1992-04-25
ES2063605A2 (es) 1995-01-01
JPH04262002A (ja) 1992-09-17
US5211703A (en) 1993-05-18
ES2063605B1 (es) 1997-08-01

Similar Documents

Publication Publication Date Title
ES2063605B1 (es) Alabes estacionarios perfeccionados para una hilera l-oc.
MX9303996A (es) Sello mecanico de superficie para proporcionar un sello entre un par de componentes relativamente girables.
ES2043488A2 (es) Perfeccionamientos en la sujecion de alabes de turbomaquinas.
ES2076676T3 (es) Juntas mecanicas de obturacion frontal.
ES2143872T3 (es) Unidad de envase.
ES2099309T3 (es) Carcasa de bomba hecha de chapa.
AR245813A1 (es) Aparato para enfriar anillos obturadores de eje de un conjunto de turbina y generador.
ES2009789B3 (es) Sistema de sellado y purga de la alta presion para turbinas de vapor.
ES2125559T3 (es) Rotor para ventilador transversal.
GB1432994A (en) Compressor for gas turbine engines
ES2066729R (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB587563A (en) Improvements relating to mountings for power plant
ES2032178A6 (es) Alabe de montaje libre para utilizacion en turbinas de vapor de baja presion.
ES2009550A6 (es) Una turbomaquina.,particularmente una turbina de vapor con alabes de entrada axil dotados de reducidas fugas y rozamientos con el aire.
ES2000105A4 (es) Cilindro con virola giratoria.
ES2008688B3 (es) Cilindro accionado por fluido.
GB855040A (en) Sealing arrangement
ES2012707A6 (es) Una turbina de vapor de flujo doble.
GB720802A (en) Improvements in and relating to assembly of blades for turbines and compressors
ES8102268A1 (es) Perfeccionamientos introducidos en un compuesto de turbina de vapor y condensador unidos entre si mediante una instala-cion de soporte
ES2015821A6 (es) Un metodo para acondicionar una muela rectificadora.
GB1554962A (en) Gas turbine power plants
ES2049156A2 (es) Junta empernada de plano doble para conjuntos segmentarios de alabes fijos de turbina soportados separadamente.
GB1438582A (en) Turbine installation
GB1179064A (en) Gas turbine power plant.

Legal Events

Date Code Title Description
EC2A Search report published

Date of ref document: 19950101

Kind code of ref document: R

Effective date: 19950101

FA2A Application withdrawn

Effective date: 19980323