[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

FR3107717B1 - Degassing tube for a turbomachine - Google Patents

Degassing tube for a turbomachine Download PDF

Info

Publication number
FR3107717B1
FR3107717B1 FR2001963A FR2001963A FR3107717B1 FR 3107717 B1 FR3107717 B1 FR 3107717B1 FR 2001963 A FR2001963 A FR 2001963A FR 2001963 A FR2001963 A FR 2001963A FR 3107717 B1 FR3107717 B1 FR 3107717B1
Authority
FR
France
Prior art keywords
degassing tube
turbomachine
tube
slot
degassing
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
FR2001963A
Other languages
French (fr)
Other versions
FR3107717A1 (en
Inventor
Clément Raphaël Laroche
Damien Greuet
Eric Abadie
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 FR2001963A priority Critical patent/FR3107717B1/en
Publication of FR3107717A1 publication Critical patent/FR3107717A1/en
Application granted granted Critical
Publication of FR3107717B1 publication Critical patent/FR3107717B1/en
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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18Lubricating arrangements
    • 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
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • 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
    • F05D2240/00Components
    • F05D2240/60Shafts
    • F05D2240/61Hollow

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)

Abstract

L’invention concerne un tube de dégazage (1) s’étendant selon un axe (X) et destiné à être monté à l’intérieur d’un arbre (2) d’une turbomachine, le tube de dégazage (1) comportant au moins une partie de centrage (4) apte à venir en appui sur une paroi radialement interne (7) de l’arbre (2), caractérisé en ce que ledit tube (1) comporte au moins une fente (9) s’étendant axialement au niveau de la partie de centrage (4), le tube de dégazage (1) comportant des premiers moyens d’étanchéité (10) souples aptes à obturer de façon étanche ladite fente (9). Figure à publier avec l’abrégé : figure 3The invention relates to a degassing tube (1) extending along an axis (X) and intended to be mounted inside a shaft (2) of a turbomachine, the degassing tube (1) comprising at at least one centering part (4) able to bear against a radially internal wall (7) of the shaft (2), characterized in that the said tube (1) comprises at least one slot (9) extending axially at the level of the centering part (4), the degassing tube (1) comprising first flexible sealing means (10) capable of sealing off said slot (9). Figure to be published with abstract: Figure 3

FR2001963A 2020-02-27 2020-02-27 Degassing tube for a turbomachine Active FR3107717B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2001963A FR3107717B1 (en) 2020-02-27 2020-02-27 Degassing tube for a turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2001963 2020-02-27
FR2001963A FR3107717B1 (en) 2020-02-27 2020-02-27 Degassing tube for a turbomachine

Publications (2)

Publication Number Publication Date
FR3107717A1 FR3107717A1 (en) 2021-09-03
FR3107717B1 true FR3107717B1 (en) 2022-09-09

Family

ID=70614164

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2001963A Active FR3107717B1 (en) 2020-02-27 2020-02-27 Degassing tube for a turbomachine

Country Status (1)

Country Link
FR (1) FR3107717B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9322293B2 (en) * 2010-03-26 2016-04-26 Snecma Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe
FR2991386B1 (en) * 2012-06-05 2014-07-18 Snecma TURBOMACHINE COMPRISING FASTENING MEANS BEFORE A DEHUILING TUBE
JP6455179B2 (en) * 2015-01-26 2019-01-23 株式会社Ihi Center vent tube alignment mechanism and center vent tube support device

Also Published As

Publication number Publication date
FR3107717A1 (en) 2021-09-03

Similar Documents

Publication Publication Date Title
CA2416150A1 (en) Diffuser for terrestrial or aeronautic gas turbine engines
FR3081211B1 (en) TURBOMACHINE COMBUSTION CHAMBER SET
FR3098247B1 (en) TURBOMACHINE JET TRUMP
KR20150130027A (en) prevention apparatus of back flow possible installation in exhaust pipe of an internal combustion engine
FR3107717B1 (en) Degassing tube for a turbomachine
FR3120663B1 (en) ASSEMBLY COMPRISING A BLADE AND AN ANGULAR BLADE SETTING SYSTEM
FR3010728A1 (en) NUT FOR TIGHTENING AND OIL DRAIN, AND TURBOMACHINE
FR3107087B1 (en) Accessory relay box for a turbomachine
FR3072422B1 (en) COMBUSTION CHAMBER MODULE FOR A TURBOMACHINE
FR3103240B1 (en) IMPELLER FOR A TURBOMACHINE EPICYCLOIDAL GEAR SPEED REDUCER SATELLITE CARRIER
EP0416977A1 (en) Rotary combustion engine
FR3112820B1 (en) AIRCRAFT TURBOMACHINE WITH VARIABLE-PITCHED PROPELLER BLADE
FR3023591A1 (en) "INTERNAL COMBUSTION ENGINE HAVING A MOTOR BLOCK WITH AN OIL DEFLECTOR"
FR3075507B1 (en) ROTATING ELECTRIC MACHINE COOLED BY A HEAT TRANSFER FLUID
FR3016410A1 (en) PUMP BODY INTEGRATED IN THE CASING OF A LIQUID COOLING ENGINE
FR3115827B1 (en) Fixing an ejection cone in a turbomachine nozzle
FR3095418B1 (en) Nacelle air inlet and nacelle having such an air inlet
FR3092869B1 (en) TURBOMACHINE DISTRIBUTORS INCLUDING A CONTACT INSERT
FR3092136B1 (en) BLOWER HOUSING FOR AN AIRCRAFT TURBOMACHINE
FR3100601B1 (en) TURBOMACHINE COMBUSTION CHAMBER CASE
FR3135769B1 (en) Box for driving accessories
US11788542B2 (en) Tandem seal pump
FR3084699B1 (en) THERMAL EXCHANGER FOR TURBOMACHINE AND ASSOCIATED MANUFACTURING PROCESS
FR3125505B1 (en) TURBOMACHINE PROPELLER BLADE PITCH CHANGE SYSTEM
FR3107311A1 (en) Set for a turbomachine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20210903

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5