FR3008185B1 - Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine - Google Patents

Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine

Info

Publication number
FR3008185B1
FR3008185B1 FR1356520A FR1356520A FR3008185B1 FR 3008185 B1 FR3008185 B1 FR 3008185B1 FR 1356520 A FR1356520 A FR 1356520A FR 1356520 A FR1356520 A FR 1356520A FR 3008185 B1 FR3008185 B1 FR 3008185B1
Authority
FR
France
Prior art keywords
insert
external surface
aerodynamic profile
test blade
turbomachine test
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
FR1356520A
Other languages
English (en)
Other versions
FR3008185A1 (fr
Inventor
Sylvain Dousseaud
Gregory Nicolas Gerald Gillant
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 FR1356520A priority Critical patent/FR3008185B1/fr
Priority to US14/322,180 priority patent/US9695693B2/en
Priority to GB1411896.2A priority patent/GB2518486B/en
Publication of FR3008185A1 publication Critical patent/FR3008185A1/fr
Application granted granted Critical
Publication of FR3008185B1 publication Critical patent/FR3008185B1/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
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
    • 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
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/14—Testing gas-turbine engines or jet-propulsion engines
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/08—Aerodynamic models
    • 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
    • F05D2260/83—Testing, e.g. methods, components or tools therefor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1356520A 2013-07-03 2013-07-03 Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine Active FR3008185B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1356520A FR3008185B1 (fr) 2013-07-03 2013-07-03 Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine
US14/322,180 US9695693B2 (en) 2013-07-03 2014-07-02 Insert with an external surface which is part of at least one aerodynamic profile of a turbomachine test blade
GB1411896.2A GB2518486B (en) 2013-07-03 2014-07-03 Insert comprising an external surface forming part of at least one aerodynamic profile of a turbine engine test vane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1356520A FR3008185B1 (fr) 2013-07-03 2013-07-03 Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine

Publications (2)

Publication Number Publication Date
FR3008185A1 FR3008185A1 (fr) 2015-01-09
FR3008185B1 true FR3008185B1 (fr) 2017-02-10

Family

ID=49546520

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1356520A Active FR3008185B1 (fr) 2013-07-03 2013-07-03 Insert comprenant une surface externe faisant partie d'au moins un profil aerodynamique d'une aube de test de turbomachine

Country Status (3)

Country Link
US (1) US9695693B2 (fr)
FR (1) FR3008185B1 (fr)
GB (1) GB2518486B (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2993927B1 (fr) 2012-07-27 2014-08-22 Snecma Piece de modification du profil d'une veine aerodynamique
BE1022512B1 (fr) * 2014-11-17 2016-05-18 Techspace Aero S.A. Banc d'essai pour turbomachine axiale avec eolienne verticale
FR3034038B1 (fr) * 2015-03-23 2017-11-17 Snecma Procede de fabrication d'une aube temoin pour etalonnage d'un controle tomographique et aube temoin en resultant
CN104849014A (zh) * 2015-05-05 2015-08-19 中国南方航空工业(集团)有限公司 用于空心叶片空气冷气流量试验的流量夹具
CN108267302B (zh) * 2016-12-30 2020-01-14 中国航发商用航空发动机有限责任公司 一种测试风扇叶片榫头强度的试验件
FR3081370B1 (fr) * 2018-05-22 2020-06-05 Safran Aircraft Engines Corps d'aube et aube en materiau composite ayant un renfort fibreux compose d'un tissage tridimensionnel et de fibres courtes et leur procede de fabrication

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4118147A (en) * 1976-12-22 1978-10-03 General Electric Company Composite reinforcement of metallic airfoils
DE3625867C2 (de) 1986-07-31 1995-10-19 Elstner Erich F Prof Dr Verwendung von Tetrachlordecaoxid in der Ophthalmologie
WO2004011887A2 (fr) * 2002-03-25 2004-02-05 Fleming And Associates, Inc. Stabilisateur de flux pour plate-forme d'essai de flux
EP1489264A1 (fr) * 2003-06-18 2004-12-22 Siemens Aktiengesellschaft Aube constituèe des modules
EP1640562A1 (fr) * 2004-09-23 2006-03-29 Siemens Aktiengesellschaft Procédé de syntonisation de fréquence d'une aube de turbine et aube de turbine
US7452182B2 (en) * 2005-04-07 2008-11-18 Siemens Energy, Inc. Multi-piece turbine vane assembly
US7789621B2 (en) * 2005-06-27 2010-09-07 Rolls-Royce North American Technologies, Inc. Gas turbine engine airfoil
US7841834B1 (en) 2006-01-27 2010-11-30 Florida Turbine Technologies, Inc. Method and leading edge replacement insert for repairing a turbine engine blade
US8033790B2 (en) * 2008-09-26 2011-10-11 Siemens Energy, Inc. Multiple piece turbine engine airfoil with a structural spar
US9085989B2 (en) 2011-12-23 2015-07-21 General Electric Company Airfoils including compliant tip

Also Published As

Publication number Publication date
US20150017005A1 (en) 2015-01-15
GB2518486B (en) 2020-07-29
GB2518486A (en) 2015-03-25
FR3008185A1 (fr) 2015-01-09
GB201411896D0 (en) 2014-08-20
US9695693B2 (en) 2017-07-04

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