FR3087829B1 - Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module - Google Patents

Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module Download PDF

Info

Publication number
FR3087829B1
FR3087829B1 FR1860004A FR1860004A FR3087829B1 FR 3087829 B1 FR3087829 B1 FR 3087829B1 FR 1860004 A FR1860004 A FR 1860004A FR 1860004 A FR1860004 A FR 1860004A FR 3087829 B1 FR3087829 B1 FR 3087829B1
Authority
FR
France
Prior art keywords
turbomachine
intermediate casing
module
measuring device
parameter measuring
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
FR1860004A
Other languages
English (en)
Other versions
FR3087829A1 (fr
Inventor
Renaud James Martet
Sebastien Jean Laurent Prestel
Cyril Verbrugge
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR1860004A priority Critical patent/FR3087829B1/fr
Publication of FR3087829A1 publication Critical patent/FR3087829A1/fr
Application granted granted Critical
Publication of FR3087829B1 publication Critical patent/FR3087829B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/02—Arrangement of sensing elements
    • F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
    • F01D17/085—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure to temperature
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/12—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to temperature
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1860004A 2018-10-29 2018-10-29 Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module Active FR3087829B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1860004A FR3087829B1 (fr) 2018-10-29 2018-10-29 Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1860004A FR3087829B1 (fr) 2018-10-29 2018-10-29 Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module

Publications (2)

Publication Number Publication Date
FR3087829A1 FR3087829A1 (fr) 2020-05-01
FR3087829B1 true FR3087829B1 (fr) 2022-11-11

Family

ID=65444143

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1860004A Active FR3087829B1 (fr) 2018-10-29 2018-10-29 Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module

Country Status (1)

Country Link
FR (1) FR3087829B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116718385B (zh) * 2023-08-07 2023-10-17 中国航发四川燃气涡轮研究院 一种核心机环境下中介机匣总压恢复系数确定方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4244222A (en) * 1979-02-01 1981-01-13 General Electric Company Instrumentation probe
US7056085B2 (en) * 2004-07-09 2006-06-06 General Electric Company Methods and apparatus for sensing parameters of air flows
US9863261B2 (en) * 2012-12-29 2018-01-09 United Technologies Corporation Component retention with probe
EP3363996B1 (fr) * 2017-02-16 2020-04-29 Ansaldo Energia Switzerland AG Agencement d'aube et moteur à turbine à gaz correspondant
FR3065527B1 (fr) * 2017-04-21 2020-11-20 Safran Aircraft Engines Dispositif de mesure de parametres d'un flux aerodynamique d'une turbomachine, secteur d'aubes instrumente equipe d'un tel dispositif de mesure et procede de fabrication d'un tel dispositif

Also Published As

Publication number Publication date
FR3087829A1 (fr) 2020-05-01

Similar Documents

Publication Publication Date Title
WO2015130363A3 (fr) Système et procédé de diagnostic de chambre de combustion de turbine à gaz
FR2897340B1 (fr) Dispositif d'alimentation en electricite et en air d'un avion au sol
EP2469082A3 (fr) Système et procédé de détection des anomalies dans les éoliennes
FR3024707B1 (fr) Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef
FR2989999B1 (fr) Dispositif de refroidissement comprenant un ventilateur axial a redressement de flux centripete et groupe electrogene correspondant.
EP2554795A3 (fr) Ensemble d'aubes statoriques pour une turbine à gaz
ATE532704T1 (de) Vorrichtung zum befestigen eines blatts mit variabler einstellung
EP2570631A3 (fr) Turbine à gaz comprenant un système de nébulisation et procédé d'opération
EP2674630A3 (fr) Broche d'alignement de turbomachine
MA48932A (fr) Pale d'éolienne dotée d'un dispositif de réduction de bruit
FR3087829B1 (fr) Carter intermediaire de turbomachine avec un dispositif de mesure de parametre aerodynamique, module de turbine comprenant un tel carter intermediaire et turbomachine equipee d'un tel module
MA53945A (fr) Montage d'un dispositif générateur de tourbillon sur une pale d'éolienne
FR3011484B1 (fr) Dispositif de separation d'air, dispositif d'inertage et aeronef comprenant un tel dispositif
PL422278A1 (pl) Urządzenie rejestrujące kolizje zwierząt latających z elektrowniami wiatrowymi i wskazujące miejsce ich upadku na podłoże zawierające przynajmniej jeden czujnik.
EP2833188A3 (fr) Appareil d'inspection de lame et procédé d'inspection de lame
GB2569017B (en) Device for measuring at least one parameter of an aerodynamic flow of a turbine engine equipped with a vibratory damping means and turbine engine
EP3369895A3 (fr) Système et procédé de surveillance d'un système de lubrification d'une turbomachine utilisant un modèle
EP3613947A3 (fr) Réducteur d'air turbulent pour moteur à turbine à gaz
EP2963276A3 (fr) Nacelle compacte avec une tuyère de soufflante profilée
FR3051014B1 (fr) Ensemble pour turbomachine comprenant un distributeur, un element de structure de turbomachine, et un dispositif de fixation
EP3020963A1 (fr) Procédé pour mesurer des paramètres de vent libre
FR3027973B1 (fr) Carter de turbomachine, comprenant un dispositif de guidage de l'air en rotation dans le carter
CA3081556A1 (fr) Systeme de transmission de donnees
FR3013766B1 (fr) Turbomachine comprenant un fourreau d'arbre et tube de fourreau associe
DK3414455T3 (da) En anordning til registrering af flyvende dyrs sammenstød med vindturbiner og angivelse af, hvor de faldt ned på jorden

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20200501

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6