BR112015010702A2 - suporte de tubo de evacuação de ar em uma turbomáquina - Google Patents

suporte de tubo de evacuação de ar em uma turbomáquina

Info

Publication number
BR112015010702A2
BR112015010702A2 BR112015010702A BR112015010702A BR112015010702A2 BR 112015010702 A2 BR112015010702 A2 BR 112015010702A2 BR 112015010702 A BR112015010702 A BR 112015010702A BR 112015010702 A BR112015010702 A BR 112015010702A BR 112015010702 A2 BR112015010702 A2 BR 112015010702A2
Authority
BR
Brazil
Prior art keywords
turbomachine
air evacuation
evacuation tube
intended
tube bracket
Prior art date
Application number
BR112015010702A
Other languages
English (en)
Other versions
BR112015010702B1 (pt
Inventor
Bensalah Boucif
Renon Olivier
Sultana Patrick
Durand Yannick
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BR112015010702A2 publication Critical patent/BR112015010702A2/pt
Publication of BR112015010702B1 publication Critical patent/BR112015010702B1/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M13/00—Crankcase ventilating or breathing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B2/00—Friction-grip releasable fastenings
    • F16B2/20—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening
    • F16B2/22—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material
    • F16B2/24—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal
    • F16B2/241—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal of sheet metal
    • F16B2/243—Clips, i.e. with gripping action effected solely by the inherent resistance to deformation of the material of the fastening of resilient material, e.g. rubbery material of metal of sheet metal internal, i.e. with spreading action
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L3/00—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets
    • F16L3/08—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing
    • F16L3/12—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing comprising a member substantially surrounding the pipe, cable or protective tubing
    • F16L3/1222—Supports for pipes, cables or protective tubing, e.g. hangers, holders, clamps, cleats, clips, brackets substantially surrounding the pipe, cable or protective tubing comprising a member substantially surrounding the pipe, cable or protective tubing the member having the form of a closed ring, e.g. used for the function of two adjacent pipe sections
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1/1 resumo “suporte de tubo de evacuação de ar em uma turbomáquina” a invenção se refere a um suporte (5) destinado a portar um tubo (4) de evacuação de ar carregado em óleo de uma turbomáquina, que compreende uma parte anular (9, 10) radialmente interna, destinada a ser montada em torno do dito tubo (4), e aletas (11) inclinadas em relação à direção axial (a) da parte anular (9, 10) e em relação ao plano radial, a periferia radialmente externa (12) das aletas (11) sendo destinada a ser fixada a um cone de ejeção (1) da turbomáquina.
BR112015010702-8A 2012-11-12 2013-11-04 Suporte destinado a portar um tubo de evacuação de ar, conjunto para uma turbomáquina e turbomáquina BR112015010702B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1260750A FR2997997B1 (fr) 2012-11-12 2012-11-12 Support de tube d'evacuation d'air dans une turbomachine
FR1260750 2012-11-12
PCT/FR2013/052625 WO2014072626A2 (fr) 2012-11-12 2013-11-04 Support de tube d'évacuation d'air dans une turbomachine

Publications (2)

Publication Number Publication Date
BR112015010702A2 true BR112015010702A2 (pt) 2017-07-11
BR112015010702B1 BR112015010702B1 (pt) 2021-08-03

Family

ID=47505153

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015010702-8A BR112015010702B1 (pt) 2012-11-12 2013-11-04 Suporte destinado a portar um tubo de evacuação de ar, conjunto para uma turbomáquina e turbomáquina

Country Status (9)

Country Link
US (1) US9863278B2 (pt)
EP (1) EP2917519B1 (pt)
JP (1) JP6251752B2 (pt)
CN (1) CN104822912B (pt)
BR (1) BR112015010702B1 (pt)
CA (1) CA2891072C (pt)
FR (1) FR2997997B1 (pt)
RU (1) RU2646167C2 (pt)
WO (1) WO2014072626A2 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD777021S1 (en) * 2014-03-25 2017-01-24 Airbus Defence And Space Limited Clamp
EP3017874B2 (en) 2014-11-06 2022-02-09 Raytheon Technologies Corporation Cold spray nozzles
JP6455179B2 (ja) 2015-01-26 2019-01-23 株式会社Ihi センターベントチューブ調芯機構及びセンターベントチューブ支持装置
FR3043138B1 (fr) * 2015-11-04 2019-09-13 Safran Aircraft Engines Tube de degazage et cone d'ejection pour une turbomachine, ainsi que leur outillage de montage
US10203114B2 (en) 2016-03-04 2019-02-12 General Electric Company Sleeve assemblies and methods of fabricating same
US10228141B2 (en) 2016-03-04 2019-03-12 General Electric Company Fuel supply conduit assemblies
US20170254540A1 (en) * 2016-03-04 2017-09-07 General Electric Company Spacers and conduit assemblies having the same
FR3064302B1 (fr) * 2017-03-23 2019-06-07 Safran Aircraft Engines Appuis centraux de tubes servitude a retour elastique
US11473431B2 (en) * 2019-03-12 2022-10-18 Raytheon Technologies Corporation Energy dissipating damper
US11028728B2 (en) 2019-03-22 2021-06-08 Raytheon Technologies Corporation Strut dampening assembly and method of making same
FR3121181B1 (fr) * 2021-03-26 2023-09-29 Safran Aircraft Engines Tube d’ejection comportant des pattes circonferentielles
FR3135754A1 (fr) * 2022-05-18 2023-11-24 Safran Aircraft Engines Supportage d’un stator d’une machine électrique en aval d’une turbine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19852603A1 (de) * 1998-11-14 2000-05-18 Asea Brown Boveri Verfahren zur Montage eines Abgasgehäuses für eine Wärmekraftmaschine, vorzugsweise eine Gasturbinenanlage
US6792758B2 (en) * 2002-11-07 2004-09-21 Siemens Westinghouse Power Corporation Variable exhaust struts shields
US7384199B2 (en) * 2004-08-27 2008-06-10 General Electric Company Apparatus for centering rotor assembly bearings
US7464536B2 (en) * 2005-07-07 2008-12-16 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2920194B1 (fr) * 2007-08-23 2014-02-21 Airbus France Cone d'ejection des gaz pour turboreacteur d'aeronef equipe d'un dispositif de generation de turbulences de flux primaire limitant le bruit de jet
FR2926604B1 (fr) * 2008-01-23 2010-03-26 Snecma Centrage d'une piece a l'interieur d'un arbre de rotor dans une turbomachine
US8061983B1 (en) * 2008-06-20 2011-11-22 Florida Turbine Technoligies, Inc. Exhaust diffuser strut with stepped trailing edge
FR2933130B1 (fr) * 2008-06-25 2012-02-24 Snecma Carter structural pour turbomachine
US20110016881A1 (en) * 2009-07-21 2011-01-27 Jose Luis Ruiz Gas turbine with exhaust gas casing and method for producing a gas turbine
CH702182A1 (de) * 2009-11-02 2011-05-13 Alstom Technology Ltd Gasturbine mit abgasgehäuse sowie verfahren zum herstellen einer solchen gasturbine.
CH703309A1 (de) * 2010-06-10 2011-12-15 Alstom Technology Ltd Abgasgehäuse für eine gasturbine sowie verfahren zum herstellen eines solchen abgasgehäuses.
DE102011008921A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenabgaskonus
PL221113B1 (pl) * 2012-01-25 2016-02-29 Gen Electric Układy dyfuzora wydechowego turbiny
FR3042812B1 (fr) * 2015-10-23 2019-06-14 Safran Aircraft Engines Tube central de ventilation pre-charge

Also Published As

Publication number Publication date
JP6251752B2 (ja) 2017-12-20
US9863278B2 (en) 2018-01-09
US20150300206A1 (en) 2015-10-22
EP2917519B1 (fr) 2018-08-15
FR2997997B1 (fr) 2014-12-26
CN104822912A (zh) 2015-08-05
EP2917519A2 (fr) 2015-09-16
CA2891072A1 (fr) 2014-05-15
FR2997997A1 (fr) 2014-05-16
CA2891072C (fr) 2020-12-01
CN104822912B (zh) 2018-07-27
RU2015122125A (ru) 2017-01-10
JP2015535048A (ja) 2015-12-07
WO2014072626A3 (fr) 2014-07-03
BR112015010702B1 (pt) 2021-08-03
WO2014072626A2 (fr) 2014-05-15
RU2646167C2 (ru) 2018-03-01

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 04/11/2013, OBSERVADAS AS CONDICOES LEGAIS.