IT1251670B - Struttura di paletta fissa perfezionata per una fila l-oc - Google Patents

Struttura di paletta fissa perfezionata per una fila l-oc

Info

Publication number
IT1251670B
IT1251670B ITMI912671A ITMI912671A IT1251670B IT 1251670 B IT1251670 B IT 1251670B IT MI912671 A ITMI912671 A IT MI912671A IT MI912671 A ITMI912671 A IT MI912671A IT 1251670 B IT1251670 B IT 1251670B
Authority
IT
Italy
Prior art keywords
aerodynamic part
rotor
row
fixed blades
perfected
Prior art date
Application number
ITMI912671A
Other languages
English (en)
Italian (it)
Inventor
Ferleger Jurek
Harold Evans David
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of ITMI912671A0 publication Critical patent/ITMI912671A0/it
Publication of ITMI912671A1 publication Critical patent/ITMI912671A1/it
Application granted granted Critical
Publication of IT1251670B publication Critical patent/IT1251670B/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/05Variable 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)
ITMI912671A 1990-10-24 1991-10-08 Struttura di paletta fissa perfezionata per una fila l-oc IT1251670B (it)

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
ITMI912671A0 ITMI912671A0 (it) 1991-10-08
ITMI912671A1 ITMI912671A1 (it) 1993-04-08
IT1251670B true IT1251670B (it) 1995-05-19

Family

ID=24414979

Family Applications (1)

Application Number Title Priority Date Filing Date
ITMI912671A IT1251670B (it) 1990-10-24 1991-10-08 Struttura di paletta fissa perfezionata per una fila l-oc

Country Status (6)

Country Link
US (1) US5211703A (https=)
JP (1) JPH04262002A (https=)
KR (1) KR920008312A (https=)
CA (1) CA2054077A1 (https=)
ES (1) ES2063605B1 (https=)
IT (1) IT1251670B (https=)

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
WO2007113149A1 (de) * 2006-03-31 2007-10-11 Alstom Technology Ltd Leitschaufel für eine strömungsmaschine, insbesondere für eine dampfturbine
US8602729B2 (en) * 2007-07-27 2013-12-10 Ansaldo Energia S.P.A. Steam turbine stage
EP2295725A1 (de) * 2009-08-13 2011-03-16 Siemens Aktiengesellschaft Ströhmungsmaschine mit Dampfentnahme
US10584715B2 (en) 2014-02-19 2020-03-10 United Technologies Corporation Gas turbine engine airfoil
EP3108105B1 (en) 2014-02-19 2021-05-12 Raytheon Technologies Corporation Gas turbine engine airfoil
US10570916B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015175073A2 (en) 2014-02-19 2015-11-19 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
EP3108103B1 (en) 2014-02-19 2023-09-27 Raytheon Technologies Corporation Fan blade for a gas turbine engine
EP3108100B1 (en) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Gas turbine engine fan blade
WO2015175044A2 (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
US10570915B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
EP3985226B1 (en) 2014-02-19 2024-12-25 RTX Corporation Gas turbine engine airfoil
WO2015175052A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126941A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015175043A2 (en) * 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
US10495106B2 (en) 2014-02-19 2019-12-03 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108101B1 (en) 2014-02-19 2022-04-20 Raytheon Technologies Corporation Gas turbine engine airfoil
US10465702B2 (en) 2014-02-19 2019-11-05 United Technologies Corporation Gas turbine engine airfoil
US9567858B2 (en) 2014-02-19 2017-02-14 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
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
WO2015126448A1 (en) * 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
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
US5211703A (en) 1993-05-18
ES2063605A2 (es) 1995-01-01
ITMI912671A0 (it) 1991-10-08
KR920008312A (ko) 1992-05-27
JPH04262002A (ja) 1992-09-17
ITMI912671A1 (it) 1993-04-08
CA2054077A1 (en) 1992-04-25
ES2063605R (https=) 1997-01-01
ES2063605B1 (es) 1997-08-01

Similar Documents

Publication Publication Date Title
IT1251670B (it) Struttura di paletta fissa perfezionata per una fila l-oc
EP1057972A3 (en) Turbine blade tip with offset squealer
DE60044228D1 (de) Kompressorrotor- Konfiguration
GB1284538A (en) Blade for a fluid flow machine
ES8701306A1 (es) Turbina hidraulica
DE59606258D1 (de) Enteisen eines rotorblattes einer windkraftanlage
ES364334A1 (es) Un aparato compresor.
EP1013877A3 (en) Hollow airfoil for a gas turbine engine
WO1996014494A3 (en) Rotor airfoils to control tip leakage flows
EP0924382A3 (en) Leading edge cooling for a gas turbine blade
RU93043403A (ru) Осевая проточная турбина
EP1443215A3 (en) Integral tip seal in a fan-shroud structure
GB1270156A (en) Improvements in transonic blades for axial flow turbines
CA2048596A1 (en) High efficiency mixer impeller
GB840543A (en) Improvements in turbine blading
GB1500858A (en) Blade for thermal axial-flow turbo machines
KR910021518A (ko) 저압 증기 터빈에 사용되는 자유지지 날개
GB1419381A (en) Fan for gas turbine engines
CA2028447A1 (en) Rotor assembly for an axial-flow combine
EP1552161B8 (de) Laufrad f r eine pumpe
US2463340A (en) Axial flow turbine blade structure
GB1411269A (en) Construction of axial-flow rotary machine housings
US4863350A (en) Air turbine
EP0965761A3 (en) Turbo molecular pump
FR2403405A1 (fr) Unite de filature du type " open-end "

Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19941027