BE677969A - - Google Patents

Info

Publication number
BE677969A
BE677969A BE677969DA BE677969A BE 677969 A BE677969 A BE 677969A BE 677969D A BE677969D A BE 677969DA BE 677969 A BE677969 A BE 677969A
Authority
BE
Belgium
Application number
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 BE677969A publication Critical patent/BE677969A/xx

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
    • 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
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE677969D 1965-05-07 1966-03-17 BE677969A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR16264A FR1442526A (fr) 1965-05-07 1965-05-07 Perfectionnements aux canaux courbes parcourus par un gaz ou une vapeur

Publications (1)

Publication Number Publication Date
BE677969A true BE677969A (de) 1966-09-01

Family

ID=8578260

Family Applications (1)

Application Number Title Priority Date Filing Date
BE677969D BE677969A (de) 1965-05-07 1966-03-17

Country Status (5)

Country Link
US (1) US3529631A (de)
BE (1) BE677969A (de)
DE (1) DE1426862B2 (de)
FR (1) FR1442526A (de)
GB (1) GB1132259A (de)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2393930A1 (fr) * 1977-06-09 1979-01-05 United Technologies Corp Plates-formes d'aubages a trainance reduite
FR2485620A1 (fr) * 1980-06-24 1981-12-31 Mtu Muenchen Gmbh Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages
WO1982002418A1 (en) * 1981-01-05 1982-07-22 Bessay Raymond Turbine stage
WO1996000841A1 (en) * 1993-06-14 1996-01-11 United Technologies Corporation Flow directing assembly for the compression section of a rotary machine
EP0846867A2 (de) * 1996-12-06 1998-06-10 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Turbomaschine mit transsonischer Verdichterstufe

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4002414A (en) * 1971-10-21 1977-01-11 Coleman Jr Richard R Compressor-expander rotor as employed with an integral turbo-compressor wave engine
US4099268A (en) * 1977-01-24 1978-07-04 Ingersoll-Rand Company Mixing device
JPS5447907A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Blading structure for axial-flow fluid machine
WO1980000468A1 (en) * 1978-08-25 1980-03-20 Cummins Engine Co Inc Turbomachine
DE3202855C1 (de) * 1982-01-29 1983-03-31 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verminderung von Sekundaerstroemungsverlusten in einem beschaufelten Stroemungskanal
FR2523642A1 (fr) * 1982-03-19 1983-09-23 Alsthom Atlantique Aubage directeur pour veines divergentes de turbine a vapeur
US5046370A (en) * 1983-11-21 1991-09-10 Great Plains Industries Inc. Flow meter with improved turbine blades
US4856348A (en) * 1983-11-21 1989-08-15 Great Plains, Industries, Inc. Flow meter turbine
US4700579A (en) * 1983-11-21 1987-10-20 Great Plains Industries, Inc. Digital flow meter for dispensing fluids
US4958985A (en) * 1989-03-01 1990-09-25 Westinghouse Electric Corp. Performance low pressure end blading
US4900230A (en) * 1989-04-27 1990-02-13 Westinghouse Electric Corp. Low pressure end blade for a low pressure steam turbine
US5251149A (en) * 1991-08-02 1993-10-05 Great Plains Industries, Inc. Electronic nutating disc flow meter
GB9823840D0 (en) * 1998-10-30 1998-12-23 Rolls Royce Plc Bladed ducting for turbomachinery
US6511294B1 (en) 1999-09-23 2003-01-28 General Electric Company Reduced-stress compressor blisk flowpath
US6524070B1 (en) 2000-08-21 2003-02-25 General Electric Company Method and apparatus for reducing rotor assembly circumferential rim stress
US6471474B1 (en) 2000-10-20 2002-10-29 General Electric Company Method and apparatus for reducing rotor assembly circumferential rim stress
CA2569026C (en) * 2004-09-24 2009-10-20 Ishikawajima-Harima Heavy Industries Co., Ltd. Wall configuration of axial-flow machine, and gas turbine engine
US7874794B2 (en) * 2006-03-21 2011-01-25 General Electric Company Blade row for a rotary machine and method of fabricating same
GB0704426D0 (en) * 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine
DE102007020025A1 (de) 2007-04-27 2008-10-30 Honda Motor Co., Ltd. Form eines Gaskanals in einer Axialströmungs-Gasturbinenmaschine
US8517686B2 (en) * 2009-11-20 2013-08-27 United Technologies Corporation Flow passage for gas turbine engine
US20110310697A1 (en) * 2010-06-22 2011-12-22 Sebastian Hirschberg Dust mixing device
US9267386B2 (en) 2012-06-29 2016-02-23 United Technologies Corporation Fairing assembly
EP2885506B8 (de) 2012-08-17 2021-03-31 Raytheon Technologies Corporation Profilierte durchflusswegfläche
US9140128B2 (en) 2012-09-28 2015-09-22 United Technologes Corporation Endwall contouring
US9212558B2 (en) 2012-09-28 2015-12-15 United Technologies Corporation Endwall contouring
US20150110617A1 (en) * 2013-10-23 2015-04-23 General Electric Company Turbine airfoil including tip fillet
CN106593540B (zh) * 2017-02-03 2018-06-26 刘欧阳 一种涡轮叶片以及由该涡轮叶片组成的涡轮
DE102017122524A1 (de) * 2017-09-28 2019-03-28 Abb Turbo Systems Ag Diffusor für einen Verdichter

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1315232A (en) * 1919-09-09 Hydeaulic bbaet-tubb
US2735612A (en) * 1956-02-21 hausmann
US1073421A (en) * 1912-05-20 1913-09-16 Emil Josse Elastic-fluid turbine.
US2166823A (en) * 1937-10-19 1939-07-18 Gen Electric Elastic fluid turbine nozzle
US2382913A (en) * 1943-04-12 1945-08-14 Gen Electric Centrifugal compressor
US2590797A (en) * 1950-02-03 1952-03-25 Gen Electric Low-pressure drop fluid duct bend
GB730009A (en) * 1952-01-02 1955-05-18 Fairey Aviat Co Ltd Improvements relating to ducts for fluid flow
US2931563A (en) * 1955-09-19 1960-04-05 Eggleton Frederick Construction of axial flow compressors
US2974927A (en) * 1955-09-27 1961-03-14 Elmer G Johnson Supersonic fluid machine
US2870958A (en) * 1956-01-13 1959-01-27 United Aircraft Corp Mixed blade compressor
FR1231173A (fr) * 1959-04-09 1960-09-27 Soc Lab Sarl Perfectionnements à l'écoulement des fluides suivant des trajectoires non rectilignes
US3000401A (en) * 1960-01-29 1961-09-19 Friedrich O Ringleb Boundary layer flow control device

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2393930A1 (fr) * 1977-06-09 1979-01-05 United Technologies Corp Plates-formes d'aubages a trainance reduite
FR2485620A1 (fr) * 1980-06-24 1981-12-31 Mtu Muenchen Gmbh Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages
WO1982002418A1 (en) * 1981-01-05 1982-07-22 Bessay Raymond Turbine stage
WO1996000841A1 (en) * 1993-06-14 1996-01-11 United Technologies Corporation Flow directing assembly for the compression section of a rotary machine
EP0846867A2 (de) * 1996-12-06 1998-06-10 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Turbomaschine mit transsonischer Verdichterstufe
EP0846867A3 (de) * 1996-12-06 1999-03-24 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Turbomaschine mit transsonischer Verdichterstufe

Also Published As

Publication number Publication date
FR1442526A (fr) 1966-06-17
DE1426862B2 (de) 1970-06-11
DE1426862A1 (de) 1969-05-08
GB1132259A (en) 1968-10-30
US3529631A (en) 1970-09-22

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: SOC. RATENAU & SOC. DU CREUSOT

Effective date: 19840317