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DE3781763D1 - Verlustarmes propellerblatt fuer ueberschallbereich. - Google Patents

Verlustarmes propellerblatt fuer ueberschallbereich.

Info

Publication number
DE3781763D1
DE3781763D1 DE8787630211T DE3781763T DE3781763D1 DE 3781763 D1 DE3781763 D1 DE 3781763D1 DE 8787630211 T DE8787630211 T DE 8787630211T DE 3781763 T DE3781763 T DE 3781763T DE 3781763 D1 DE3781763 D1 DE 3781763D1
Authority
DE
Germany
Prior art keywords
loss
low
propeller blade
supervisory
range
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.)
Expired - Lifetime
Application number
DE8787630211T
Other languages
English (en)
Other versions
DE3781763T2 (de
Inventor
Harris David Weingold
Walter Benjamin Harvey
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE3781763D1 publication Critical patent/DE3781763D1/de
Application granted granted Critical
Publication of DE3781763T2 publication Critical patent/DE3781763T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16—Blades
    • B64C11/18—Aerodynamic features
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D21/00—Pump involving supersonic speed of pumped fluids
    • 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
    • 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
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Compressor (AREA)
DE8787630211T 1986-10-28 1987-10-26 Verlustarmes propellerblatt fuer ueberschallbereich. Expired - Lifetime DE3781763T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/924,007 US4726737A (en) 1986-10-28 1986-10-28 Reduced loss swept supersonic fan blade

Publications (2)

Publication Number Publication Date
DE3781763D1 true DE3781763D1 (de) 1992-10-22
DE3781763T2 DE3781763T2 (de) 1993-01-07

Family

ID=25449577

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787630211T Expired - Lifetime DE3781763T2 (de) 1986-10-28 1987-10-26 Verlustarmes propellerblatt fuer ueberschallbereich.

Country Status (8)

Country Link
US (1) US4726737A (de)
EP (1) EP0266298B1 (de)
JP (1) JP2673156B2 (de)
AU (1) AU601502B2 (de)
CA (1) CA1283366C (de)
DE (1) DE3781763T2 (de)
IL (1) IL84290A (de)
NO (1) NO168547C (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5167489A (en) * 1991-04-15 1992-12-01 General Electric Company Forward swept rotor blade
US5275531A (en) * 1993-04-30 1994-01-04 Teleflex, Incorporated Area ruled fan blade ends for turbofan jet engine
US5642985A (en) 1995-11-17 1997-07-01 United Technologies Corporation Swept turbomachinery blade
GB9607316D0 (en) * 1996-04-09 1996-06-12 Rolls Royce Plc Swept fan blade
US6071077A (en) * 1996-04-09 2000-06-06 Rolls-Royce Plc Swept fan blade
US6312219B1 (en) 1999-11-05 2001-11-06 General Electric Company Narrow waist vane
US6299412B1 (en) 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil
US6328533B1 (en) 1999-12-21 2001-12-11 General Electric Company Swept barrel airfoil
US6338609B1 (en) 2000-02-18 2002-01-15 General Electric Company Convex compressor casing
US7204676B2 (en) * 2004-05-14 2007-04-17 Pratt & Whitney Canada Corp. Fan blade curvature distribution for high core pressure ratio fan
US7320575B2 (en) * 2004-09-28 2008-01-22 General Electric Company Methods and apparatus for aerodynamically self-enhancing rotor blades
DE102004054752A1 (de) * 2004-11-12 2006-05-18 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe
GB0704426D0 (en) * 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine
JP4923073B2 (ja) * 2009-02-25 2012-04-25 株式会社日立製作所 遷音速翼
US9121285B2 (en) 2012-05-24 2015-09-01 General Electric Company Turbine and method for reducing shock losses in a turbine
US9212663B2 (en) 2013-01-28 2015-12-15 Terrence O'Neill All-supersonic ducted fan for propelling aircraft at high subsonic speeds
US9568009B2 (en) 2013-03-11 2017-02-14 Rolls-Royce Corporation Gas turbine engine flow path geometry
GB2544735B (en) * 2015-11-23 2018-02-07 Rolls Royce Plc Vanes of a gas turbine engine
US10710705B2 (en) 2017-06-28 2020-07-14 General Electric Company Open rotor and airfoil therefor
FR3080886B1 (fr) * 2018-05-02 2020-10-30 Safran Aircraft Engines Turbomachine a soufflante carenee
US11255199B2 (en) * 2020-05-20 2022-02-22 Rolls-Royce Corporation Airfoil with shaped mass reduction pocket
US11608743B1 (en) 2022-02-04 2023-03-21 General Electric Company Low-noise blade for an open rotor
US12049306B2 (en) 2022-02-04 2024-07-30 General Electric Company Low-noise blade for an open rotor

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA344800A (en) * 1934-09-25 Ondreas Arno Package filling machine
US2043736A (en) * 1935-02-07 1936-06-09 Hartzell Industries Ventilating fan
FR877989A (fr) * 1940-04-11 1943-01-07 Messerschmitt Ag Hélice aérienne
GB548090A (en) * 1940-05-16 1942-09-24 Westinghouse Electric Int Co Improvements in or relating to elastic fluid turbines
US2258795A (en) * 1941-06-14 1941-10-14 Westinghouse Electric & Mfg Co Elastic-fluid turbine
US2738950A (en) * 1945-12-13 1956-03-20 Lockheed Aircraft Corp Turbine machine having high velocity blading
SU266475A1 (ru) * 1966-07-29 1975-10-15 Б. М. Аронов Лопатка реактивной газовой турбины
DE1903642A1 (de) * 1969-01-20 1970-08-06 Bbc Sulzer Turbomaschinen Schaufelung fuer Rotoren von Axialverdichtern
SE392082B (sv) * 1974-11-15 1977-03-14 Jernforedling Ab Propellerblad till en sjelvflojlande propeller for batar
US3989406A (en) * 1974-11-26 1976-11-02 Bolt Beranek And Newman, Inc. Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors
US4358246A (en) * 1979-07-16 1982-11-09 United Technologies Corporation Noise reduction means for prop-fan and the construction thereof
FR2551145B1 (fr) * 1980-07-30 1990-08-17 Onera (Off Nat Aerospatiale) Etage de compresseur supersonique a aubes et procede de determination
US4431376A (en) * 1980-10-27 1984-02-14 United Technologies Corporation Airfoil shape for arrays of airfoils
US4569631A (en) * 1984-08-06 1986-02-11 Airflow Research And Manufacturing Corp. High strength fan

Also Published As

Publication number Publication date
JPS63120898A (ja) 1988-05-25
US4726737A (en) 1988-02-23
NO874474D0 (no) 1987-10-27
AU8049987A (en) 1988-05-05
IL84290A (en) 1992-01-15
NO168547B (no) 1991-11-25
NO874474L (no) 1988-04-29
NO168547C (no) 1992-03-04
EP0266298A2 (de) 1988-05-04
IL84290A0 (en) 1988-03-31
DE3781763T2 (de) 1993-01-07
EP0266298B1 (de) 1992-09-16
AU601502B2 (en) 1990-09-13
CA1283366C (en) 1991-04-23
EP0266298A3 (en) 1989-05-10
JP2673156B2 (ja) 1997-11-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition