FR2669686B1 - Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine. - Google Patents

Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.

Info

Publication number
FR2669686B1
FR2669686B1 FR909014850A FR9014850A FR2669686B1 FR 2669686 B1 FR2669686 B1 FR 2669686B1 FR 909014850 A FR909014850 A FR 909014850A FR 9014850 A FR9014850 A FR 9014850A FR 2669686 B1 FR2669686 B1 FR 2669686B1
Authority
FR
France
Prior art keywords
reconstructing
shoes
platforms
blades
blower rotor
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 - Fee Related
Application number
FR909014850A
Other languages
English (en)
Other versions
FR2669686A1 (fr
Inventor
Michel Brioude
Antoine
Philippe Chereau
Jacky Naudet
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 FR909014850A priority Critical patent/FR2669686B1/fr
Priority to EP91403182A priority patent/EP0488874B1/fr
Priority to DE69105099T priority patent/DE69105099T2/de
Priority to US07/799,326 priority patent/US5161949A/en
Publication of FR2669686A1 publication Critical patent/FR2669686A1/fr
Application granted granted Critical
Publication of FR2669686B1 publication Critical patent/FR2669686B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F04D29/26—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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR909014850A 1990-11-28 1990-11-28 Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine. Expired - Fee Related FR2669686B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR909014850A FR2669686B1 (fr) 1990-11-28 1990-11-28 Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.
EP91403182A EP0488874B1 (fr) 1990-11-28 1991-11-26 Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine
DE69105099T DE69105099T2 (de) 1990-11-28 1991-11-26 Gebläserotor mit Schaufeln ohne Plattform und Stromlinien rekonstruierenden Füllstücken.
US07/799,326 US5161949A (en) 1990-11-28 1991-11-27 Rotor fitted with spacer blocks between the blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR909014850A FR2669686B1 (fr) 1990-11-28 1990-11-28 Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.

Publications (2)

Publication Number Publication Date
FR2669686A1 FR2669686A1 (fr) 1992-05-29
FR2669686B1 true FR2669686B1 (fr) 1994-09-02

Family

ID=9402665

Family Applications (1)

Application Number Title Priority Date Filing Date
FR909014850A Expired - Fee Related FR2669686B1 (fr) 1990-11-28 1990-11-28 Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.

Country Status (4)

Country Link
US (1) US5161949A (fr)
EP (1) EP0488874B1 (fr)
DE (1) DE69105099T2 (fr)
FR (1) FR2669686B1 (fr)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
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US5277548A (en) * 1991-12-31 1994-01-11 United Technologies Corporation Non-integral rotor blade platform
GB9208409D0 (en) * 1992-04-16 1992-06-03 Rolls Royce Plc Rotors for gas turbine engines
FR2716502B1 (fr) * 1994-02-23 1996-04-05 Snecma Garniture d'étanchéité entre des aubes et des plates-formes intermédiaires.
FR2739136B1 (fr) * 1995-09-21 1997-10-31 Snecma Agencement amortissant pour des aubes de rotor
FR2739135B1 (fr) * 1995-09-21 1997-10-31 Snecma Agencement amortisseur monte entre des aubes de rotor
US6447250B1 (en) * 2000-11-27 2002-09-10 General Electric Company Non-integral fan platform
JP4807113B2 (ja) * 2006-03-14 2011-11-02 株式会社Ｉｈｉ ファンのダブテール構造
GB0614640D0 (en) * 2006-07-22 2006-08-30 Rolls Royce Plc An annulus filler seal
US7762781B1 (en) 2007-03-06 2010-07-27 Florida Turbine Technologies, Inc. Composite blade and platform assembly
US7766609B1 (en) * 2007-05-24 2010-08-03 Florida Turbine Technologies, Inc. Turbine vane endwall with float wall heat shield
CN101255873B (zh) * 2008-02-28 2010-06-09 大连海事大学 压气机动叶叶尖小翼
GB0814718D0 (en) * 2008-08-13 2008-09-17 Rolls Royce Plc Annulus filler
US8137072B2 (en) * 2008-10-31 2012-03-20 Solar Turbines Inc. Turbine blade including a seal pocket
US8393869B2 (en) 2008-12-19 2013-03-12 Solar Turbines Inc. Turbine blade assembly including a damper
US8616849B2 (en) * 2009-02-18 2013-12-31 Pratt & Whitney Canada Corp. Fan blade platform
US8568102B2 (en) 2009-02-18 2013-10-29 Pratt & Whitney Canada Corp. Fan blade anti-fretting insert
US8066479B2 (en) * 2010-04-05 2011-11-29 Pratt & Whitney Rocketdyne, Inc. Non-integral platform and damper for an airfoil
FR2965843B1 (fr) * 2010-10-06 2012-11-09 Snecma Rotor pour turbomachine
EP2447476A3 (fr) 2010-11-01 2017-11-15 Rolls-Royce plc Pièce de remplissage annulaire pour un disque de rotor de turbine à gaz
US10036261B2 (en) * 2012-04-30 2018-07-31 United Technologies Corporation Blade dovetail bottom
US9650901B2 (en) 2012-05-31 2017-05-16 Solar Turbines Incorporated Turbine damper
US9279332B2 (en) 2012-05-31 2016-03-08 Solar Turbines Incorporated Turbine damper
US9528376B2 (en) * 2012-09-13 2016-12-27 General Electric Company Compressor fairing segment
US9303519B2 (en) * 2012-10-31 2016-04-05 Solar Turbines Incorporated Damper for a turbine rotor assembly
US9347325B2 (en) * 2012-10-31 2016-05-24 Solar Turbines Incorporated Damper for a turbine rotor assembly
US10145268B2 (en) * 2013-03-15 2018-12-04 United Technologies Corporation Injection molded composite fan platform
FR3003294B1 (fr) * 2013-03-15 2018-03-30 Safran Aircraft Engines Soufflante de turbomoteur a flux multiple, et turbomoteur equipe d'une telle soufflante
FR3021691B1 (fr) * 2014-06-03 2016-06-24 Snecma Rotor pour turbomachine comportant des aubes a plates-formes raportees
US10197009B2 (en) * 2014-07-30 2019-02-05 Pratt & Whitney Canada Corp. Gas turbine engine ejector
US9995162B2 (en) * 2014-10-20 2018-06-12 United Technologies Corporation Seal and clip-on damper system and device
US10156151B2 (en) 2014-10-23 2018-12-18 Rolls-Royce North American Technologies Inc. Composite annulus filler
FR3035677B1 (fr) * 2015-04-29 2017-05-12 Snecma Aube munie de plateformes possedant des portions d'accrochage
FR3038653B1 (fr) * 2015-07-08 2017-08-04 Snecma Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
US10662784B2 (en) 2016-11-28 2020-05-26 Raytheon Technologies Corporation Damper with varying thickness for a blade
US10677073B2 (en) 2017-01-03 2020-06-09 Raytheon Technologies Corporation Blade platform with damper restraint
US10731479B2 (en) * 2017-01-03 2020-08-04 Raytheon Technologies Corporation Blade platform with damper restraint
US11118458B2 (en) * 2017-10-27 2021-09-14 MTU Aero Engines AG Combination for sealing a gap between turbomachine blades and for reducing vibrations of the turbomachine blades
FR3091563B1 (fr) * 2019-01-04 2023-01-20 Safran Aircraft Engines Joint d’étanchéité amélioré de plateforme inter-aubes
CN114439551B (zh) * 2020-10-30 2024-05-10 中国航发商用航空发动机有限责任公司 航空发动机
CN113217461B (zh) * 2021-05-12 2022-08-16 中南大学 一种叶片、其造型方法和制造方法及压气机
FR3126446A1 (fr) * 2021-09-01 2023-03-03 Safran Aircraft Engines Amortisseur déformable pour roue mobile de turbomachine
US20230194096A1 (en) * 2021-12-17 2023-06-22 Pratt & Whitney Canada Corp. Exhaust system for a gas turbine engine and method for using same

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE540433A (fr) * 1954-08-12
US3294364A (en) * 1962-01-02 1966-12-27 Gen Electric Rotor assembly
GB981476A (en) * 1963-11-04 1965-01-27 Rolls Royce Gas turbine engine vane assembly
CH494896A (de) * 1968-08-09 1970-08-15 Sulzer Ag Halterung von Laufschaufeln im Rotor einer Turbomaschine
GB1259750A (en) * 1970-07-23 1972-01-12 Rolls Royce Rotor for a fluid flow machine
BE791375A (fr) * 1971-12-02 1973-03-01 Gen Electric Deflecteur et amortisseur pour ailettes de turbomachines
GB2006883B (en) * 1977-10-27 1982-02-24 Rolls Royce Fan or compressor stage for a gas turbine engine
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
FR2639402B1 (fr) * 1988-11-23 1990-12-28 Snecma Disque ailete de rotor de turbomachine
US4872810A (en) * 1988-12-14 1989-10-10 United Technologies Corporation Turbine rotor retention system

Also Published As

Publication number Publication date
EP0488874A1 (fr) 1992-06-03
DE69105099D1 (de) 1994-12-15
FR2669686A1 (fr) 1992-05-29
EP0488874B1 (fr) 1994-11-09
DE69105099T2 (de) 1995-04-20
US5161949A (en) 1992-11-10

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