FR3027623B1 - Aube mobile de rotor a reponse acoustique reduite - Google Patents

Aube mobile de rotor a reponse acoustique reduite Download PDF

Info

Publication number
FR3027623B1
FR3027623B1 FR1460203A FR1460203A FR3027623B1 FR 3027623 B1 FR3027623 B1 FR 3027623B1 FR 1460203 A FR1460203 A FR 1460203A FR 1460203 A FR1460203 A FR 1460203A FR 3027623 B1 FR3027623 B1 FR 3027623B1
Authority
FR
France
Prior art keywords
dawn
acoustic response
reduced acoustic
mobile rotor
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.)
Active
Application number
FR1460203A
Other languages
English (en)
Other versions
FR3027623A1 (fr
Inventor
Norman Bruno Andre Jodet
Herve Rolland
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 FR1460203A priority Critical patent/FR3027623B1/fr
Priority to US14/918,241 priority patent/US10024176B2/en
Publication of FR3027623A1 publication Critical patent/FR3027623A1/fr
Application granted granted Critical
Publication of FR3027623B1 publication Critical patent/FR3027623B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/145Means for influencing boundary layers or secondary circulations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/16Form or construction for counteracting blade vibration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • F05D2260/961Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • F05D2260/962Preventing, counteracting or reducing vibration or noise by means of "anti-noise"
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Aube mobile de turbomachine comprenant un bord de fuite (20A) avec un état de surface modifié (22, 28) permettant d'altérer la vitesse de l'écoulement circulant autour de l'aube de façon à modifier l'interaction acoustique sur des éléments de structure (12) qui interagissent avec cet écoulement en aval de l'aube mobile.
FR1460203A 2014-10-23 2014-10-23 Aube mobile de rotor a reponse acoustique reduite Active FR3027623B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1460203A FR3027623B1 (fr) 2014-10-23 2014-10-23 Aube mobile de rotor a reponse acoustique reduite
US14/918,241 US10024176B2 (en) 2014-10-23 2015-10-20 Rotor blade with reduced acoustic response

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1460203A FR3027623B1 (fr) 2014-10-23 2014-10-23 Aube mobile de rotor a reponse acoustique reduite

Publications (2)

Publication Number Publication Date
FR3027623A1 FR3027623A1 (fr) 2016-04-29
FR3027623B1 true FR3027623B1 (fr) 2021-05-28

Family

ID=52102890

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1460203A Active FR3027623B1 (fr) 2014-10-23 2014-10-23 Aube mobile de rotor a reponse acoustique reduite

Country Status (2)

Country Link
US (1) US10024176B2 (fr)
FR (1) FR3027623B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20250154869A1 (en) * 2023-11-09 2025-05-15 Pratt & Whitney Canada Corp. Tailoring rotor blade sector configurations to tune gas turbine engine bladed rotor

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3741285A (en) * 1968-07-09 1973-06-26 A Kuethe Boundary layer control of flow separation and heat exchange
US4318669A (en) * 1980-01-07 1982-03-09 The United States Of America As Represented By The Secretary Of The Air Force Vane configuration for fluid wake re-energization
US4720239A (en) * 1982-10-22 1988-01-19 Owczarek Jerzy A Stator blades of turbomachines
DK174319B1 (da) * 2000-06-20 2002-12-02 Lm Glasfiber As Vindmøllevinge med støjdæmpningsmidler
DE102004009755A1 (de) * 2004-02-28 2005-09-15 Mtu Aero Engines Gmbh Gasturbinenschaufel
US8333552B2 (en) * 2008-06-20 2012-12-18 General Electric Company Combined acoustic absorber and heat exchanging outlet guide vanes
FR2937078B1 (fr) * 2008-10-13 2011-09-23 Snecma Aube de turbine a performances aerodynamiques ameliorees.
US20120103430A1 (en) * 2010-10-27 2012-05-03 Zuei-Ling Lin Method of reducing the object-traveling resistance
EP2746533B1 (fr) * 2012-12-19 2015-04-01 MTU Aero Engines GmbH Grille d'aube et turbomachine
US9581034B2 (en) * 2013-03-14 2017-02-28 Elliott Company Turbomachinery stationary vane arrangement for disk and blade excitation reduction and phase cancellation
DE102013206207A1 (de) * 2013-04-09 2014-10-09 MTU Aero Engines AG Schaufelblatt für eine Strömungsmaschine mit Hinterkantenprofilierung, Schaufel und integral beschaufelter Rotor
US10060441B2 (en) * 2015-05-26 2018-08-28 Pratt & Whitney Canada Corp. Gas turbine stator with winglets

Also Published As

Publication number Publication date
FR3027623A1 (fr) 2016-04-29
US10024176B2 (en) 2018-07-17
US20160115798A1 (en) 2016-04-28

Similar Documents

Publication Publication Date Title
EP3834471A4 (fr) Traitement amélioré sur la description de flux qos
FR3019855B1 (fr) Ensemble propulsif d'aeronef comprenant une vanne d'air a debit variable
MX382610B (es) Válvula de entrada para un compresor.
PL3339606T3 (pl) Turbinowy silnik gazowy o odwróconym przepływie
FR3016189B1 (fr) Dispositif de reduction epicycloidal pour l'entrainement en rotation des ensembles de pales d'une turbomachine a reducteur
GB2572680B (en) Outlet guide vane for turbomachine, made from several parts assembled together by attachment means outside the flow stream
FR3032244B1 (fr) Valve de regulation de debit.
FR3027951B1 (fr) Baignoire de sommet d'aubes d'une turbine de turbomachine
MX385877B (es) Dispositivo de procesamiento de disparo y proyector.
FR3046410B1 (fr) Assemblage pour turbomachine d'aeronef a helices contrarotatives non carenees, comprenant un fourreau de passage de servitudes a encombrement reduit
JP2018031263A5 (fr)
FR3033179B1 (fr) Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
EP3953545A4 (fr) Machine de déplacement de sièges de salle de spectacle, suspendus, actionnés par bord
FR3005096B1 (fr) Systeme pour commander le pas des pales d'une helice de turbomachine, et turbomachine a helice pour aeronef avec un tel systeme
FR3008750B1 (fr) Couvercle de compresseur centrifuge de turbomachine apte a etre fixe par l'aval pres de son bord amont, turbomachine comportant ce couvercle.
FR3027623B1 (fr) Aube mobile de rotor a reponse acoustique reduite
FR3038654B1 (fr) Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
FR3033180B1 (fr) Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
EP3894698C0 (fr) Régulation de flux de pale d'éolienne
EP3761888A4 (fr) Régulation de débit aortique trans-oesophagien
FR3057909B1 (fr) Turbomachine d'aeronef comprenant une zone fusible agencee sur un arbre pivotant
DK3870842T3 (da) Luftturbine med gennemstrømning
GB201617186D0 (en) Centrifugal pump flow modifier
GB201803189D0 (en) Non-positive displacement tangential flow turbine engine
FR3036092B1 (fr) Dispositif a arbre radial pour la commande de l'orientation des pales de soufflante d'une turbomachine a soufflante non carenee

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20160429

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12