FR2536365A1 - Pale pour propulseur d'aeronef - Google Patents

Pale pour propulseur d'aeronef Download PDF

Info

Publication number
FR2536365A1
FR2536365A1 FR8219337A FR8219337A FR2536365A1 FR 2536365 A1 FR2536365 A1 FR 2536365A1 FR 8219337 A FR8219337 A FR 8219337A FR 8219337 A FR8219337 A FR 8219337A FR 2536365 A1 FR2536365 A1 FR 2536365A1
Authority
FR
France
Prior art keywords
zone
profile
curvature
thickness
blade
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.)
Granted
Application number
FR8219337A
Other languages
English (en)
French (fr)
Other versions
FR2536365B1 (enExample
Inventor
Jean-Jacques Thibert
Jean-Marc Bousquet
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR8219337A priority Critical patent/FR2536365A1/fr
Priority to JP58217079A priority patent/JPS59118597A/ja
Priority to SU833665258A priority patent/SU1540653A3/ru
Priority to EP83402231A priority patent/EP0110766B1/fr
Priority to DE8383402231T priority patent/DE3372195D1/de
Publication of FR2536365A1 publication Critical patent/FR2536365A1/fr
Priority to US06/724,945 priority patent/US4652213A/en
Application granted granted Critical
Publication of FR2536365B1 publication Critical patent/FR2536365B1/fr
Granted 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
    • 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

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Tires In General (AREA)
  • General Details Of Gearings (AREA)
  • Retarders (AREA)
FR8219337A 1982-11-18 1982-11-18 Pale pour propulseur d'aeronef Granted FR2536365A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR8219337A FR2536365A1 (fr) 1982-11-18 1982-11-18 Pale pour propulseur d'aeronef
JP58217079A JPS59118597A (ja) 1982-11-18 1983-11-17 航空機用推進機の翼
SU833665258A SU1540653A3 (ru) 1982-11-18 1983-11-17 Аэродинамический профиль лопасти воздушного винта летательного аппарата
EP83402231A EP0110766B1 (fr) 1982-11-18 1983-11-18 Pale pour propulseur d'aéronef
DE8383402231T DE3372195D1 (en) 1982-11-18 1983-11-18 Blade for an aircraft propeller
US06/724,945 US4652213A (en) 1982-11-18 1985-04-19 Propeller blade for aircraft propulsion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8219337A FR2536365A1 (fr) 1982-11-18 1982-11-18 Pale pour propulseur d'aeronef

Publications (2)

Publication Number Publication Date
FR2536365A1 true FR2536365A1 (fr) 1984-05-25
FR2536365B1 FR2536365B1 (enExample) 1985-04-26

Family

ID=9279296

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8219337A Granted FR2536365A1 (fr) 1982-11-18 1982-11-18 Pale pour propulseur d'aeronef

Country Status (6)

Country Link
US (1) US4652213A (enExample)
EP (1) EP0110766B1 (enExample)
JP (1) JPS59118597A (enExample)
DE (1) DE3372195D1 (enExample)
FR (1) FR2536365A1 (enExample)
SU (1) SU1540653A3 (enExample)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE33589E (en) * 1986-09-03 1991-05-14 United Technologies Corporation Helicopter blade airfoil
US4744728A (en) * 1986-09-03 1988-05-17 United Technologies Corporation Helicopter blade airfoil
US4834617A (en) * 1987-09-03 1989-05-30 United Technologies Corporation Airfoiled blade
FR2628062B1 (fr) * 1988-03-07 1990-08-10 Aerospatiale Pale pour helice carenee a hautes performances, helice carenee multipale pourvue de telles pales et agencement de rotor de queue a helice carenee pour aeronef a voilure tournante
GB2220712B (en) * 1988-07-13 1992-12-09 Rolls Royce Plc Open rotor blading
US5024396A (en) * 1988-07-19 1991-06-18 Principia Recherche Developpement Sa Air or submarine engine with improved contour
US4941803A (en) * 1989-02-01 1990-07-17 United Technologies Corporation Airfoiled blade
JP2633413B2 (ja) * 1991-06-03 1997-07-23 富士重工業株式会社 回転翼航空機の回転翼羽根
FR2689852B1 (fr) * 1992-04-09 1994-06-17 Eurocopter France Pale pour voilure tournante d'aeronef, a extremite en fleche.
WO1994008846A1 (fr) * 1992-10-16 1994-04-28 Aktsionernoe Obschestvo 'aviatika' Helice
US5417548A (en) * 1994-01-14 1995-05-23 Midwest Research Institute Root region airfoil for wind turbine
RU2123453C1 (ru) * 1996-12-15 1998-12-20 Центральный аэрогидродинамический институт им.проф.Н.Е.Жуковского Лопасть винта
US5911559A (en) * 1997-09-16 1999-06-15 United Technologies Corporation Airfoiled blade for a propeller
US6378802B1 (en) * 1998-05-04 2002-04-30 Manuel Munoz Saiz Enhance aerodynamic profile
US6607164B2 (en) 2001-10-22 2003-08-19 Toyota Motor Sales, U.S.A., Inc. Wing airfoil
ES2268912B1 (es) * 2003-03-13 2008-02-16 Indar Maquinas Hidraulicas, S.L Grupo electrobomba multietapa.
US20040206852A1 (en) * 2003-04-16 2004-10-21 Saiz Manuel Munoz Aerodynamic profile
IT1401661B1 (it) * 2010-08-25 2013-08-02 Nuova Pignone S R L Forma di profilo areodinamico per compressore.
US9340277B2 (en) * 2012-02-29 2016-05-17 General Electric Company Airfoils for use in rotary machines
DE102013008145A1 (de) * 2013-05-14 2014-11-20 Man Diesel & Turbo Se Laufschaufel für einen Verdichter und Verdichter mit einer solchen Laufschaufel
US9278744B1 (en) 2015-03-26 2016-03-08 Frank Chester ChetProp air or water propeller and spinner with front and back leg assemblies attached to spinner
CN105129071B (zh) * 2015-06-26 2017-03-08 北京昶远科技有限公司 太阳能飞机翼型设计方法及太阳能飞机翼型
US10710705B2 (en) * 2017-06-28 2020-07-14 General Electric Company Open rotor and airfoil therefor
US10358926B2 (en) * 2017-08-11 2019-07-23 General Electric Company Low-noise airfoil for an open rotor
FR3077803B1 (fr) * 2018-02-15 2020-07-31 Airbus Helicopters Methode d'amelioration d'une pale afin d'augmenter son incidence negative de decrochage
EP3891066A4 (en) * 2018-12-07 2022-08-10 Joby Aero, Inc. ROTATING AIRFORCE AND DESIGN METHOD THEREFORE
WO2021092677A1 (en) * 2019-11-14 2021-05-20 Delson Aeronautics Ltd. Ultra-wide-chord propeller
RU2769545C1 (ru) * 2021-05-14 2022-04-04 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Аэродинамический профиль несущего элемента летательного аппарата

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463054A1 (fr) * 1979-08-10 1981-02-20 Aerospatiale Profil de pale pour voilure tournante d'aeronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3343512A (en) * 1966-05-20 1967-09-26 Francis R Rasmussen Hydrofoil with unsymmetrical nose profile
GB1383070A (en) * 1971-12-13 1975-02-05 Boeing Co Hydrodynamic sections
US4142837A (en) * 1977-11-11 1979-03-06 United Technologies Corporation Helicopter blade
GB2016397B (en) * 1978-02-02 1982-03-24 Aerospatiale Aerofoil
US4459083A (en) * 1979-03-06 1984-07-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Shapes for rotating airfoils
FR2490586A1 (fr) * 1980-09-24 1982-03-26 Aerospatiale Profil de pale pour voilure tournante d'aeronef
US4412664A (en) * 1982-06-25 1983-11-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Family of airfoil shapes for rotating blades

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463054A1 (fr) * 1979-08-10 1981-02-20 Aerospatiale Profil de pale pour voilure tournante d'aeronef

Also Published As

Publication number Publication date
US4652213A (en) 1987-03-24
JPS59118597A (ja) 1984-07-09
EP0110766A1 (fr) 1984-06-13
FR2536365B1 (enExample) 1985-04-26
DE3372195D1 (en) 1987-07-30
SU1540653A3 (ru) 1990-01-30
EP0110766B1 (fr) 1987-06-24

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