FR3040077B1 - Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion - Google Patents

Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Info

Publication number
FR3040077B1
FR3040077B1 FR1557701A FR1557701A FR3040077B1 FR 3040077 B1 FR3040077 B1 FR 3040077B1 FR 1557701 A FR1557701 A FR 1557701A FR 1557701 A FR1557701 A FR 1557701A FR 3040077 B1 FR3040077 B1 FR 3040077B1
Authority
FR
France
Prior art keywords
turbopropulser
turbomachine
airborne
turbo
turbo airborne
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
FR1557701A
Other languages
English (en)
Other versions
FR3040077A1 (fr
Inventor
Suzanne Madeleine Coustillas
Kamel Benderradji
Blaise Bergon
Alain Marc Lucien Bromann
Lilian Yann Dumas
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 FR1557701A priority Critical patent/FR3040077B1/fr
Publication of FR3040077A1 publication Critical patent/FR3040077A1/fr
Application granted granted Critical
Publication of FR3040077B1 publication Critical patent/FR3040077B1/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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/003Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical seals
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243Flange connections; Bolting arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1557701A 2015-08-12 2015-08-12 Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion Active FR3040077B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1557701A FR3040077B1 (fr) 2015-08-12 2015-08-12 Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1557701A FR3040077B1 (fr) 2015-08-12 2015-08-12 Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Publications (2)

Publication Number Publication Date
FR3040077A1 FR3040077A1 (fr) 2017-02-17
FR3040077B1 true FR3040077B1 (fr) 2017-08-11

Family

ID=54608743

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1557701A Active FR3040077B1 (fr) 2015-08-12 2015-08-12 Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion

Country Status (1)

Country Link
FR (1) FR3040077B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6273671B1 (en) * 1999-07-30 2001-08-14 Allison Advanced Development Company Blade clearance control for turbomachinery
US7967558B2 (en) * 2007-01-19 2011-06-28 United Technologies Corporation Hybrid seal assembly for a fan-turbine rotor of a tip turbine engine
FR2991387B1 (fr) * 2012-06-01 2016-03-04 Snecma Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
FR3008750B1 (fr) * 2013-07-18 2015-07-17 Snecma Couvercle de compresseur centrifuge de turbomachine apte a etre fixe par l'aval pres de son bord amont, turbomachine comportant ce couvercle.

Also Published As

Publication number Publication date
FR3040077A1 (fr) 2017-02-17

Similar Documents

Publication Publication Date Title
PL3792465T3 (pl) Architektura wielowirnikowego silnika turbinowego
BR112017023549A2 (pt) composições de endófito complexo isolado e métodos para melhorar características de planta.
GB201613989D0 (en) Turbine shroud assembly
EA201790064A1 (ru) Пестицидные композиции
DK3350452T3 (da) Turbomaskineskovlhjul med høj stivhed, turbomaskine, herunder skovlhjulet, og fremgangsmåde til fremstilling
FR3003303B1 (fr) Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
FR2989426B1 (fr) Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
FR3050229B1 (fr) Carter d'echappement de turbomachine
FR3026717B1 (fr) Atterrisseur d'aeronef.
DK3506921T3 (da) Depotsystemer, der omfatter glatirameracetat
GB201613926D0 (en) Inter-stage cooling for a turbomachine
FR3051854B1 (fr) Carter d'echappement de turbomachine
GB201605323D0 (en) Gas turbine engine fan assembly
EP3216988B8 (fr) Centrale à turbine à vapeur
DE112017001088A5 (de) Gasturbinensystem
EP3258063A4 (fr) Turbine à flux axial
EP3514336A4 (fr) Système de protection contre la survitesse d'une turbine à vapeur, et turbine à vapeur
EP3249157A4 (fr) Turbine à vapeur
FR2961850B1 (fr) Turbine pour une turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
EP3284915A4 (fr) Turbine à vapeur
GB201505243D0 (en) Turbomachinery blade
FR3027015B1 (fr) Atterrisseur d'aeronef.
FR2991387B1 (fr) Turbomachine, telle qu'un turboreacteur ou un turbopropulseur d'avion
GB2567103B (en) Turbo engine rotor disc
DE112017001143A5 (de) Gasturbinensystem

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20170217

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: 20180809

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