FR3015553B1 - Aube comprenant une echasse, munie d'une seule portion en depression - Google Patents

Aube comprenant une echasse, munie d'une seule portion en depression Download PDF

Info

Publication number
FR3015553B1
FR3015553B1 FR1363374A FR1363374A FR3015553B1 FR 3015553 B1 FR3015553 B1 FR 3015553B1 FR 1363374 A FR1363374 A FR 1363374A FR 1363374 A FR1363374 A FR 1363374A FR 3015553 B1 FR3015553 B1 FR 3015553B1
Authority
FR
France
Prior art keywords
echasse
dawn
low pressure
depression
single portion
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
FR1363374A
Other languages
English (en)
Other versions
FR3015553A1 (fr
Inventor
Marco NUCCI
Damien Merlot
Jacky RODRIGUEZ
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1363374A priority Critical patent/FR3015553B1/fr
Priority to US14/579,426 priority patent/US20150176415A1/en
Priority to GB1423063.5A priority patent/GB2522999B/en
Publication of FR3015553A1 publication Critical patent/FR3015553A1/fr
Priority to US15/872,782 priority patent/US10458257B2/en
Application granted granted Critical
Publication of FR3015553B1 publication Critical patent/FR3015553B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F04D29/324—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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise

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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)

Abstract

L'échasse (6) de cette aube comporte un côté (7) et l'autre (18) pourvu d'une dépression (10). En concentrant cette dépression d'un seul côté, on obtient une échasse (6) plus rigide et résistante à allégement égal, les concentrations de contrainte dépendant de la profondeur de la dépression mais étant absentes du côté (7) plan. Les vibrations et déformations de flexion sont aussi réduites. Application aux aubes de turbomachine, notamment de compresseurs.
FR1363374A 2013-12-23 2013-12-23 Aube comprenant une echasse, munie d'une seule portion en depression Active FR3015553B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1363374A FR3015553B1 (fr) 2013-12-23 2013-12-23 Aube comprenant une echasse, munie d'une seule portion en depression
US14/579,426 US20150176415A1 (en) 2013-12-23 2014-12-22 Blade comprising a support, provided with a portion with a depression
GB1423063.5A GB2522999B (en) 2013-12-23 2014-12-23 Blade comprising a support, provided with a portion with a depression
US15/872,782 US10458257B2 (en) 2013-12-23 2018-01-16 Blade comprising a shank, provided with a depressed portion

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1363374 2013-12-23
FR1363374A FR3015553B1 (fr) 2013-12-23 2013-12-23 Aube comprenant une echasse, munie d'une seule portion en depression

Publications (2)

Publication Number Publication Date
FR3015553A1 FR3015553A1 (fr) 2015-06-26
FR3015553B1 true FR3015553B1 (fr) 2019-05-31

Family

ID=50290035

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1363374A Active FR3015553B1 (fr) 2013-12-23 2013-12-23 Aube comprenant une echasse, munie d'une seule portion en depression

Country Status (3)

Country Link
US (1) US20150176415A1 (fr)
FR (1) FR3015553B1 (fr)
GB (1) GB2522999B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3028574B1 (fr) 2014-11-17 2019-09-20 Safran Aircraft Engines Disque aubage monobloc pour soufflante de turbomachine comportant un evidement amont et ou aval conferant une plus grande flexibilite a ses aubes
FR3033359B1 (fr) 2015-03-02 2017-04-07 Snecma Disque aubage monobloc comportant un moyeu ayant une face evidee a laquelle est rapporte un organe de comblement
EP3263839A1 (fr) * 2016-06-29 2018-01-03 Siemens Aktiengesellschaft Procédé d'optimisation d'un design d'une aube et aube associée
FR3096727B1 (fr) * 2019-05-27 2021-06-25 Safran Helicopter Engines Aube de turbine dotée d’une cavité de fragilisation d’une section frangible
DE102021109844A1 (de) 2021-04-19 2022-10-20 MTU Aero Engines AG Gasturbinen-Schaufelanordnung

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2162588B (en) * 1984-07-30 1988-11-09 Gen Electric Gas turbine bladed disk assembly
US4595340A (en) * 1984-07-30 1986-06-17 General Electric Company Gas turbine bladed disk assembly
DE3743253A1 (de) * 1987-12-19 1989-06-29 Mtu Muenchen Gmbh Axial durchstroemtes laufschaufelgitter fuer verdichter oder turbinen
US5261790A (en) * 1992-02-03 1993-11-16 General Electric Company Retention device for turbine blade damper
US5435694A (en) * 1993-11-19 1995-07-25 General Electric Company Stress relieving mount for an axial blade
US8282354B2 (en) * 2008-04-16 2012-10-09 United Technologies Corporation Reduced weight blade for a gas turbine engine
US8727730B2 (en) * 2010-04-06 2014-05-20 General Electric Company Composite turbine bucket assembly
US9359905B2 (en) * 2012-02-27 2016-06-07 Solar Turbines Incorporated Turbine engine rotor blade groove
US9140132B2 (en) * 2012-05-31 2015-09-22 Solar Turbines Incorporated Turbine blade support
FR2997723B1 (fr) * 2012-11-06 2018-09-21 Safran Aircraft Engines Aube a pied munie de portions en depression
US9353629B2 (en) * 2012-11-30 2016-05-31 Solar Turbines Incorporated Turbine blade apparatus

Also Published As

Publication number Publication date
FR3015553A1 (fr) 2015-06-26
GB2522999A (en) 2015-08-12
GB2522999B (en) 2016-05-18
US20150176415A1 (en) 2015-06-25

Similar Documents

Publication Publication Date Title
FR3015553B1 (fr) Aube comprenant une echasse, munie d'une seule portion en depression
Storey The language of threats
PH12016500232A1 (en) Causing display of a notification
PH12016502423A1 (en) Synthetic transactions between communication endpoints
EP2998800A3 (fr) Composant horloger à pivot flexible
MX2016013727A (es) Ventilador de material compuesto.
GB201313165D0 (en) Composite Turbine Engine Blade with Structural Reinforcement
WO2015175044A3 (fr) Profil aérodynamique de moteur à turbine à gaz
WO2015178974A3 (fr) Surface portante de moteur à turbine à gaz
MX2018001336A (es) Medidor de flujo ultrasónico que tiene cubierta de carcasa.
BR112014010351A2 (pt) método de conexão de corpo de filamento de metal e dispositivo de conexão
ATE433055T1 (de) Propeller
MX2016005523A (es) Impulsor de compresor centrifugo con cuchillas que tienen un borde de arrastre con forma de s.
PL396520A1 (pl) Dyfuzor gazu wydechowego i turbina
FR3052822B1 (fr) Aube de turbomachine equipee d'un joint en elastomere
WO2015175045A3 (fr) Surface portante de moteur à turbine à gaz
CN106695625B8 (zh) 电子设备的装配治具及电子设备的装配工艺
RU2015107176A (ru) Подвижная лопатка турбины
FR2985785B1 (fr) Pale d'hydrolienne et hydrolienne comprenant au moins une telle pale
SA517381120B1 (ar) مضخة طرد مركزي متعددة المراحل بفواصل ضغط
EP3902988A4 (fr) Système turbo électrique, dont le rendement est augmenté par la présence d'un compresseur et d'une turbine sur des arbres séparés, et son principe de fonctionnement
TR201902659A2 (tr) Kompozi̇t biçak
WO2016150423A3 (fr) Dispositif pour stabiliser le courant d'entrée d'un réacteur lors d'essais au point fixe de réacteurs et/ou pour réduire les décollement des filets d'air et les variations de pression à l'entrée des réacteurs lors d'essais au point fixe, système d'assistance pour essais au point fixe pour des réacteurs d'aéronefs et utilisation d'un dispositif selon l'invention
TR201906263U5 (tr) Yüksek debi̇li̇, düşük enerji̇ sarfi̇yatli, mobi̇li̇ze su pompasi
PL124938U1 (pl) Kotwica talerzowa

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

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