CH428071A - Blading of an axial flow compressor - Google Patents

Blading of an axial flow compressor

Info

Publication number
CH428071A
CH428071A CH807062A CH807062A CH428071A CH 428071 A CH428071 A CH 428071A CH 807062 A CH807062 A CH 807062A CH 807062 A CH807062 A CH 807062A CH 428071 A CH428071 A CH 428071A
Authority
CH
Switzerland
Prior art keywords
blading
axial flow
flow compressor
compressor
axial
Prior art date
Application number
CH807062A
Other languages
German (de)
Inventor
Fortescue Peter
Original Assignee
Gen Dynamics 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 Gen Dynamics Corp filed Critical Gen Dynamics Corp
Publication of CH428071A publication Critical patent/CH428071A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—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
    • 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
    • F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • F04D29/544—Blade shapes
CH807062A 1961-07-05 1962-07-05 Blading of an axial flow compressor CH428071A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US121875A US3112866A (en) 1961-07-05 1961-07-05 Compressor blade structure

Publications (1)

Publication Number Publication Date
CH428071A true CH428071A (en) 1967-01-15

Family

ID=22399293

Family Applications (1)

Application Number Title Priority Date Filing Date
CH807062A CH428071A (en) 1961-07-05 1962-07-05 Blading of an axial flow compressor

Country Status (4)

Country Link
US (1) US3112866A (en)
CH (1) CH428071A (en)
DE (1) DE1428098A1 (en)
GB (1) GB951713A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0343888A2 (en) * 1988-05-27 1989-11-29 Herman E. Sheets Method and apparatus for producing fluid pressure and controlling boundary layer
WO1997004217A1 (en) * 1995-07-14 1997-02-06 Bmw Rolls-Royce Gmbh Tandem turbine-blade cascade

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3775023A (en) * 1971-02-17 1973-11-27 Teledyne Ind Multistage axial flow compressor
US3867062A (en) * 1971-09-24 1975-02-18 Theodor H Troller High energy axial flow transfer stage
US3937592A (en) * 1973-05-30 1976-02-10 Gutehoffnungshutte Sterkrade Aktiengesellschaft Multi-stage axial flow compressor
US3877835A (en) * 1973-07-13 1975-04-15 Fred M Siptrott High and low pressure hydro turbine
US5486091A (en) * 1994-04-19 1996-01-23 United Technologies Corporation Gas turbine airfoil clocking
JPH11311130A (en) 1998-04-27 1999-11-09 Kawasaki Heavy Ind Ltd Booster structure for jet engine
GB2376723B (en) * 2001-06-20 2004-12-08 Rolls Royce Plc Tandem guide vane
TW546443B (en) * 2002-09-27 2003-08-11 Delta Electronics Inc Axial flow fan with a plurality of segment blades
US7478629B2 (en) * 2004-11-04 2009-01-20 Del Valle Bravo Facundo Axial flow supercharger and fluid compression machine
GB2441543B (en) * 2006-09-07 2008-07-23 Rolls Royce Plc An array of components
US20090317237A1 (en) * 2008-06-20 2009-12-24 General Electric Company System and method for reduction of unsteady pressures in turbomachinery
JP5374199B2 (en) * 2009-03-19 2013-12-25 三菱重工業株式会社 gas turbine
JP5202597B2 (en) * 2010-09-16 2013-06-05 株式会社日立製作所 Axial flow compressor, gas turbine system equipped with axial flow compressor, and method for remodeling axial flow compressor
US20150152879A1 (en) * 2013-11-29 2015-06-04 Applied Thermal/Fluid Analysis Center Limited Liability Company Blade structure of axial fan
DE102015223212A1 (en) * 2015-11-24 2017-05-24 MTU Aero Engines AG Process, compressor and turbomachinery
CN113309729B (en) * 2021-07-29 2022-01-21 中国航发上海商用航空发动机制造有限责任公司 Multistage axial flow compressor test monitoring method and device

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR811104A (en) * 1936-09-08 1937-04-07 Aerodynamic rotary compressor
FR876380A (en) * 1940-12-09 1942-11-04 Brown Axial compressor with recovery turbine
FR982027A (en) * 1943-06-01 1951-06-04 Further development of axial compressors
US2699319A (en) * 1949-12-02 1955-01-11 Chrysler Corp Power conversion machine
US2931563A (en) * 1955-09-19 1960-04-05 Eggleton Frederick Construction of axial flow compressors
GB780240A (en) * 1955-09-19 1957-07-31 Frederick Eggleton Improvements in or relating to the construction of axial flow turbines or compressors

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0343888A2 (en) * 1988-05-27 1989-11-29 Herman E. Sheets Method and apparatus for producing fluid pressure and controlling boundary layer
EP0343888A3 (en) * 1988-05-27 1990-09-19 Herman E. Sheets Method and apparatus for producing fluid pressure and controlling boundary layer
WO1997004217A1 (en) * 1995-07-14 1997-02-06 Bmw Rolls-Royce Gmbh Tandem turbine-blade cascade

Also Published As

Publication number Publication date
US3112866A (en) 1963-12-03
DE1428098A1 (en) 1969-07-17
GB951713A (en) 1964-03-11

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