FR3021030B1 - Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef - Google Patents

Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef Download PDF

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Publication number
FR3021030B1
FR3021030B1 FR1454283A FR1454283A FR3021030B1 FR 3021030 B1 FR3021030 B1 FR 3021030B1 FR 1454283 A FR1454283 A FR 1454283A FR 1454283 A FR1454283 A FR 1454283A FR 3021030 B1 FR3021030 B1 FR 3021030B1
Authority
FR
France
Prior art keywords
turbomachine
propeller
aircraft
anchor blade
radial translation
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.)
Active
Application number
FR1454283A
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English (en)
Other versions
FR3021030A1 (fr
Inventor
Bruno PETELLAZ
Catherine DELMAS
Stanislas TUTAJ
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.)
Ratier Figeac SAS
Original Assignee
Ratier Figeac SAS
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 Ratier Figeac SAS filed Critical Ratier Figeac SAS
Priority to FR1454283A priority Critical patent/FR3021030B1/fr
Priority to US14/712,094 priority patent/US9840921B2/en
Publication of FR3021030A1 publication Critical patent/FR3021030A1/fr
Application granted granted Critical
Publication of FR3021030B1 publication Critical patent/FR3021030B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/10—Anti- vibration means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0292—Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves
    • 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
    • F04D29/322—Blade mountings
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49337—Composite blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1454283A 2014-05-14 2014-05-14 Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef Active FR3021030B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1454283A FR3021030B1 (fr) 2014-05-14 2014-05-14 Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef
US14/712,094 US9840921B2 (en) 2014-05-14 2015-05-14 Blade anchored securely in radial translation, propeller, turbine engine and aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1454283 2014-05-14
FR1454283A FR3021030B1 (fr) 2014-05-14 2014-05-14 Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef

Publications (2)

Publication Number Publication Date
FR3021030A1 FR3021030A1 (fr) 2015-11-20
FR3021030B1 true FR3021030B1 (fr) 2018-01-05

Family

ID=51063705

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1454283A Active FR3021030B1 (fr) 2014-05-14 2014-05-14 Pale a ancrage securise en translation radiale, helice, turbomachine et aeronef

Country Status (2)

Country Link
US (1) US9840921B2 (fr)
FR (1) FR3021030B1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3050719B1 (fr) * 2016-04-28 2018-04-13 Airbus Operations Helice pour turbomachine d'aeronef comprenant des moyens de secours de calage en incidence de pale
FR3050718B1 (fr) * 2016-04-28 2022-02-18 Airbus Operations Sas Helice pour turbomachine d'aeronef comprenant des moyens simplifies de retention radiale de pale d'helice
FR3085415B1 (fr) * 2018-09-05 2021-04-16 Safran Aircraft Engines Aube comprenant une structure en materiau composite et une coque metallique
US11092020B2 (en) 2018-10-18 2021-08-17 Raytheon Technologies Corporation Rotor assembly for gas turbine engines
US11306601B2 (en) 2018-10-18 2022-04-19 Raytheon Technologies Corporation Pinned airfoil for gas turbine engines
FR3087830B1 (fr) * 2018-10-30 2020-10-16 Safran Aircraft Engines Aube comprenant une structure en materiau composite et une piece de raidissement metallique
FR3097835A1 (fr) 2019-06-27 2021-01-01 Airbus Helicopters Hélice d’avancement munie de pales interchangeables et procédé de montage de pales interchangeables sur une hélice d’avancement
US11059566B2 (en) * 2019-10-02 2021-07-13 Bell Textron Inc. Additive manufacture proprotor blade
FR3106364B1 (fr) * 2020-01-20 2021-12-10 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé
US11073030B1 (en) 2020-05-21 2021-07-27 Raytheon Technologies Corporation Airfoil attachment for gas turbine engines
US11454280B2 (en) * 2020-06-30 2022-09-27 Textron Innovations Inc. Rotor retention fitting with integral bearing and pitch control
CN115989178A (zh) * 2020-07-24 2023-04-18 赛峰飞机发动机公司 用于对飞行器涡轮发动机的螺旋桨轮叶的节距设定进行控制的系统
FR3123696B1 (fr) * 2021-06-02 2023-04-21 Safran Aircraft Engines Système de commande du calage angulaire d’une aube d’helice pour une turbomachine d’aeronef
CN115885110A (zh) * 2020-07-24 2023-03-31 赛峰飞机发动机公司 包括轮叶和轮叶桨距设置系统的组件
FR3120663B1 (fr) * 2021-03-09 2024-04-05 Safran Aircraft Engines Ensemble comportant une aube et un systeme de calage angulaire de l'aube
FR3126729A1 (fr) * 2021-09-08 2023-03-10 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé
FR3127472A1 (fr) 2021-09-27 2023-03-31 Airbus Helicopters pale de rotor avec un système de rétention et de reprises d’efforts dissociés et rotor muni de telles pales
FR3128972A1 (fr) * 2021-11-09 2023-05-12 Safran Aircraft Engines Liaison entre un pied d’aube et un dispositif de calage

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1769801A (en) * 1924-11-15 1930-07-01 Hamilton Standard Propeller Co Propeller
US3734642A (en) * 1971-06-29 1973-05-22 United Aircraft Corp Aerodynamic blade root end attachment
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
US5102300A (en) * 1988-10-07 1992-04-07 United Technologies Corporation Pinned airfoil propeller assembly
FR2682722B1 (fr) * 1991-10-16 1994-01-21 Jeumont Schneider Moyens pour l'ancrage d'une piece par rapport a une autre.
US6102664A (en) * 1995-12-14 2000-08-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blading system and method for controlling structural vibrations
FR2970943B1 (fr) * 2011-01-31 2014-02-28 Eurocopter France Pale et procede de fabrication de ladite pale
FR2984847B1 (fr) * 2011-12-23 2013-12-27 Ratier Figeac Soc Pale a ancrage redondant dans un moyeu, helice, turbopropulseur et aeronef
FR2984848B1 (fr) * 2011-12-23 2016-01-15 Ratier Figeac Soc Pale d'helice avec caissons et longerons de renfort et helice comprenant au moins une telle pale
GB201211133D0 (en) * 2012-06-22 2012-08-08 Rolls Royce Plc A catcher ring arrangement
US9505489B2 (en) * 2013-03-13 2016-11-29 Bell Helicopter Textron Inc. Flexing clevis arrangement bolted joint attachment for flexible rotor hub with high offset and high flapping

Also Published As

Publication number Publication date
FR3021030A1 (fr) 2015-11-20
US9840921B2 (en) 2017-12-12
US20150330233A1 (en) 2015-11-19

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