FR2685732B1 - Aube de turbomachine en materiau composite. - Google Patents

Aube de turbomachine en materiau composite.

Info

Publication number
FR2685732B1
FR2685732B1 FR9116358A FR9116358A FR2685732B1 FR 2685732 B1 FR2685732 B1 FR 2685732B1 FR 9116358 A FR9116358 A FR 9116358A FR 9116358 A FR9116358 A FR 9116358A FR 2685732 B1 FR2685732 B1 FR 2685732B1
Authority
FR
France
Prior art keywords
turbomachine
blade
composite material
composite
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
FR9116358A
Other languages
English (en)
Other versions
FR2685732A1 (fr
Inventor
Gerard Chez Madame Aube Lauzeille
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9116358A priority Critical patent/FR2685732B1/fr
Priority to GB9226331A priority patent/GB2262966B/en
Priority to US07/999,359 priority patent/US5292231A/en
Publication of FR2685732A1 publication Critical patent/FR2685732A1/fr
Application granted granted Critical
Publication of FR2685732B1 publication Critical patent/FR2685732B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR9116358A 1991-12-31 1991-12-31 Aube de turbomachine en materiau composite. Expired - Lifetime FR2685732B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR9116358A FR2685732B1 (fr) 1991-12-31 1991-12-31 Aube de turbomachine en materiau composite.
GB9226331A GB2262966B (en) 1991-12-31 1992-12-17 Turbomachine blade made of composite material
US07/999,359 US5292231A (en) 1991-12-31 1992-12-31 Turbomachine blade made of composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9116358A FR2685732B1 (fr) 1991-12-31 1991-12-31 Aube de turbomachine en materiau composite.

Publications (2)

Publication Number Publication Date
FR2685732A1 FR2685732A1 (fr) 1993-07-02
FR2685732B1 true FR2685732B1 (fr) 1994-02-25

Family

ID=9420679

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9116358A Expired - Lifetime FR2685732B1 (fr) 1991-12-31 1991-12-31 Aube de turbomachine en materiau composite.

Country Status (3)

Country Link
US (1) US5292231A (fr)
FR (1) FR2685732B1 (fr)
GB (1) GB2262966B (fr)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573377A (en) * 1995-04-21 1996-11-12 General Electric Company Assembly of a composite blade root and a rotor
US5720597A (en) * 1996-01-29 1998-02-24 General Electric Company Multi-component blade for a gas turbine
SE506358C2 (sv) * 1996-04-17 1997-12-08 Flaekt Ab Rotorblad för fastsättning på ett nav i en rotor, såsom en skovel för fastsättning på ett fläktnav
US5735673A (en) * 1996-12-04 1998-04-07 United Technologies Corporation Turbine engine rotor blade pair
US5725353A (en) * 1996-12-04 1998-03-10 United Technologies Corporation Turbine engine rotor disk
DE19708825C2 (de) * 1997-03-05 2001-11-15 Deutsch Zentr Luft & Raumfahrt Vorrichtung zum Fördern eines Mediums
JP4060981B2 (ja) * 1998-04-08 2008-03-12 本田技研工業株式会社 ガスタービンの静翼構造体及びそのユニット
GB9828484D0 (en) 1998-12-24 1999-02-17 Rolls Royce Plc Improvements in or relating to bladed structures for fluid flow propulsion engines
US6290466B1 (en) 1999-09-17 2001-09-18 General Electric Company Composite blade root attachment
US6676080B2 (en) * 2000-07-19 2004-01-13 Aero Composites, Inc. Composite airfoil assembly
FR2817192B1 (fr) * 2000-11-28 2003-08-08 Snecma Moteurs Ensemble forme par au moins une pale et une plate-forme de fixation de la pale, pour une turbomachine, et procede pour sa fabrication
US6569194B1 (en) * 2000-12-28 2003-05-27 Advanced Cardiovascular Systems, Inc. Thermoelastic and superelastic Ni-Ti-W alloy
US6857856B2 (en) * 2002-09-27 2005-02-22 Florida Turbine Technologies, Inc. Tailored attachment mechanism for composite airfoils
US7300255B2 (en) * 2002-09-27 2007-11-27 Florida Turbine Technologies, Inc. Laminated turbomachine airfoil with jacket and method of making the airfoil
US20050158171A1 (en) * 2004-01-15 2005-07-21 General Electric Company Hybrid ceramic matrix composite turbine blades for improved processibility and performance
SE0700823L (sv) * 2007-03-30 2008-10-01 Volvo Aero Corp Komponent för en gasturbinmotor, jetmotor försedd med en sådan komponent, samt en flygmaskin försedd med en sådan jetmotor
FR2918347B1 (fr) 2007-07-02 2010-05-07 Eurocopter France Pale munie d'un longeron a enroulement horizontal et procede de fabrication d'un tel longeron
US8206118B2 (en) * 2008-01-04 2012-06-26 United Technologies Corporation Airfoil attachment
US8123463B2 (en) * 2008-07-31 2012-02-28 General Electric Company Method and system for manufacturing a blade
FR2941487B1 (fr) * 2009-01-28 2011-03-04 Snecma Aube de turbomachine en materiau composite a pied renforce
EP2322763A1 (fr) * 2009-11-17 2011-05-18 Siemens Aktiengesellschaft Aube de turbine ou de compresseur
US8801886B2 (en) 2010-04-16 2014-08-12 General Electric Company Ceramic composite components and methods of fabricating the same
US8794925B2 (en) 2010-08-24 2014-08-05 United Technologies Corporation Root region of a blade for a gas turbine engine
FR2970943B1 (fr) 2011-01-31 2014-02-28 Eurocopter France Pale et procede de fabrication de ladite pale
US9115584B2 (en) * 2012-04-24 2015-08-25 General Electric Company Resistive band for turbomachine blade
US10633985B2 (en) 2012-06-25 2020-04-28 General Electric Company System having blade segment with curved mounting geometry
FR2997127A1 (fr) * 2012-10-22 2014-04-25 Snecma Aubes de turbine haute pression en composites a matrice ceramique
WO2015057369A1 (fr) * 2013-10-14 2015-04-23 United Technologies Corporation Superposition de couches de fixation de pale par coin
CA2936196A1 (fr) 2014-01-16 2015-07-23 General Electric Company Cale de reduction de contrainte de pied de pale composite
US9963979B2 (en) 2014-11-17 2018-05-08 Rolls-Royce North American Technologies Inc. Composite components for gas turbine engines
US10563523B2 (en) 2015-04-08 2020-02-18 Rolls-Royce Corporation Method for fabricating a ceramic matrix composite rotor blade
US10207471B2 (en) * 2016-05-04 2019-02-19 General Electric Company Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article
US10753368B2 (en) * 2016-08-23 2020-08-25 Raytheon Technologies Corporation Multi-piece non-linear airfoil
US10352273B2 (en) * 2016-11-08 2019-07-16 Rohr, Inc. Track beam with composite lug
FR3063514B1 (fr) * 2017-03-02 2019-04-12 Safran Aube de turbomachine et procede pour sa fabrication

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB493145A (en) * 1937-03-31 1938-09-30 Bruno Jablonsky Pressed articles, particularly airscrew blades, of laminated wood and method of manufacturing the same
GB755253A (en) * 1954-02-24 1956-08-22 Armstrong Siddeley Motors Ltd Plastic blades, particularly for a compressor rotor of a gas turbine engine
GB1211082A (en) * 1967-08-02 1970-11-04 Dowty Rotol Ltd Blades, suitable for propellers, compressors, fans and the like
US3737250A (en) * 1971-06-16 1973-06-05 Us Navy Fiber blade attachment
US4040770A (en) * 1975-12-22 1977-08-09 General Electric Company Transition reinforcement of composite blade dovetails
US4037990A (en) * 1976-06-01 1977-07-26 General Electric Company Composite turbomachinery rotor
US4098559A (en) * 1976-07-26 1978-07-04 United Technologies Corporation Paired blade assembly
US4343593A (en) * 1980-01-25 1982-08-10 The United States Of America As Represented By The Secretary Of The Air Force Composite blade for turbofan engine fan
DE3802774A1 (de) * 1988-01-30 1989-08-10 Mtu Muenchen Gmbh Laufschaufel fuer einen triebwerksrotor
US5149319A (en) * 1990-09-11 1992-09-22 Unger Evan C Methods for providing localized therapeutic heat to biological tissues and fluids
IT1240175B (it) * 1990-04-06 1993-11-27 Agusta Spa Pala per elicottero

Also Published As

Publication number Publication date
FR2685732A1 (fr) 1993-07-02
US5292231A (en) 1994-03-08
GB9226331D0 (en) 1993-02-10
GB2262966B (en) 1994-10-05
GB2262966A (en) 1993-07-07

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Legal Events

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TP Transmission of property
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