SE307216B - - Google Patents

Info

Publication number
SE307216B
SE307216B SE11885/63A SE1188563A SE307216B SE 307216 B SE307216 B SE 307216B SE 11885/63 A SE11885/63 A SE 11885/63A SE 1188563 A SE1188563 A SE 1188563A SE 307216 B SE307216 B SE 307216B
Authority
SE
Sweden
Prior art keywords
blades
flow
vanes
rotor
concave surfaces
Prior art date
Application number
SE11885/63A
Inventor
J Erwin
L Smith
Original Assignee
Gen Electric
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 Electric filed Critical Gen Electric
Publication of SE307216B publication Critical patent/SE307216B/xx

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
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • 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
    • 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
    • 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
    • F04D29/38—Blades
    • F04D29/384—Blades characterised by 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

996,041. Axial-flow compressors; turbine blades. GENERAL ELECTRIC CO. Oct. 25, 1963 [Oct. 29, 1962], No. 42174/63. Headings F1C and FIT. [Also in Division F2] Auxiliary blading for the rotor or stator blades of a compressor or turbine to augment and turn the secondary fluid flow between adjacent blades thereof, comprises flow directing vanes radically disposed on the blades substantially at the surfaces of the boundary layer and so disposed that the secondary, fluid flow passing near the concave surfaces of the blades is directed toward the convex surfaces of adjacent blades. Auxiliary vanes 16, Fig. 4, which may be flat but preferably are cambered, are provided at the root portions of compressor rotor blades 12 substantially at the surface of the boundary layer air at the rotor hub 10. The secondary air, which flows essentially normal to the main flow and, at the hub, flows radially inwardly on the concave surfaces of the blades and radially outwardly on the convex surfaces of adjacent blades, is augmented by some of the main flow by means of the vanes 16 which are oriented to promote flow in this direction. Consequently, more boundary layer air is turned into the main stream to mix therewith, and this results in a higher pressure rise across the compressor before stall. Alternatively, or in addition to, the vanes 16 may be positioned at the tip portions of the blades 12 to augment the secondary flow at the outer casing, in which case the vanes 16 will be oriented to direct flow radially outwardly at the concave surfaces of the blades 12. In an alternative embodiment, Fig. 5 (not shown), flat curved vanes are provided at the root and tip portions of the rotor blades on their concave surfaces only.
SE11885/63A 1962-10-29 1963-10-29 SE307216B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US233661A US3193185A (en) 1962-10-29 1962-10-29 Compressor blading

Publications (1)

Publication Number Publication Date
SE307216B true SE307216B (en) 1968-12-23

Family

ID=22878175

Family Applications (1)

Application Number Title Priority Date Filing Date
SE11885/63A SE307216B (en) 1962-10-29 1963-10-29

Country Status (6)

Country Link
US (1) US3193185A (en)
BE (1) BE638547A (en)
CH (1) CH417837A (en)
DE (1) DE1428110A1 (en)
GB (1) GB996041A (en)
SE (1) SE307216B (en)

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DE3017226A1 (en) * 1979-05-12 1980-11-20 Papst Motoren Kg FAN BLADE
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US5112187A (en) * 1990-09-12 1992-05-12 Westinghouse Electric Corp. Erosion control through reduction of moisture transport by secondary flow
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US6779979B1 (en) * 2003-04-23 2004-08-24 General Electric Company Methods and apparatus for structurally supporting airfoil tips
US6905309B2 (en) * 2003-08-28 2005-06-14 General Electric Company Methods and apparatus for reducing vibrations induced to compressor airfoils
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US7244104B2 (en) * 2005-05-31 2007-07-17 Pratt & Whitney Canada Corp. Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US7189056B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Blade and disk radial pre-swirlers
ITMI20060340A1 (en) * 2006-02-27 2007-08-28 Nuovo Pignone Spa SHOVEL OF A ROTOR OF A SECOND STAGE OF A COMPRESSOR
EP2093378A1 (en) * 2008-02-25 2009-08-26 ALSTOM Technology Ltd Upgrading method for a blade by retrofitting a winglet, and correspondingly upgraded blade
US8147207B2 (en) * 2008-09-04 2012-04-03 Siemens Energy, Inc. Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion
US8770460B2 (en) * 2008-12-23 2014-07-08 George E. Belzer Shield for surgical stapler and method of use
EP2336492A1 (en) * 2009-12-16 2011-06-22 Siemens Aktiengesellschaft Guide vane with a winglet for an energy converting machine and machine for converting energy comprising the guide vane
US8591195B2 (en) 2010-05-28 2013-11-26 Pratt & Whitney Canada Corp. Turbine blade with pressure side stiffening rib
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US8944774B2 (en) * 2012-01-03 2015-02-03 General Electric Company Gas turbine nozzle with a flow fence
US9359900B2 (en) 2012-10-05 2016-06-07 General Electric Company Exhaust diffuser
EP2799721B8 (en) * 2013-05-03 2016-12-07 Safran Aero Booster S.A. Axial turbomachine stator guide with auxiliary vanes on the vane feet
US9938984B2 (en) * 2014-12-29 2018-04-10 General Electric Company Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
US9874221B2 (en) 2014-12-29 2018-01-23 General Electric Company Axial compressor rotor incorporating splitter blades
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CN110067774A (en) * 2019-04-16 2019-07-30 中国航发湖南动力机械研究所 The compressor of combined impeller and gas-turbine unit
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IT202100002240A1 (en) 2021-02-02 2022-08-02 Gen Electric TURBINE ENGINE WITH REDUCED TRANSVERSE FLOW VANES
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Also Published As

Publication number Publication date
DE1428110A1 (en) 1969-02-13
US3193185A (en) 1965-07-06
CH417837A (en) 1966-07-31
BE638547A (en) 1900-01-01
GB996041A (en) 1965-06-23

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