UA85173C2 - Дренажная труба дегазации для вала компрессора низкого давления - Google Patents

Дренажная труба дегазации для вала компрессора низкого давления

Info

Publication number
UA85173C2
UA85173C2 UAA200506419A UAA200506419A UA85173C2 UA 85173 C2 UA85173 C2 UA 85173C2 UA A200506419 A UAA200506419 A UA A200506419A UA A200506419 A UAA200506419 A UA A200506419A UA 85173 C2 UA85173 C2 UA 85173C2
Authority
UA
Ukraine
Prior art keywords
tube
turbomachine
low
pressure shaft
drain tube
Prior art date
Application number
UAA200506419A
Other languages
English (en)
Ukrainian (uk)
Inventor
Бруно Дамбран
Аймерік Угоні
Клод МОН
Жан-Люк Супізон
Original Assignee
Снекма
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 Снекма filed Critical Снекма
Publication of UA85173C2 publication Critical patent/UA85173C2/ru

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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • 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
    • F01D25/18—Lubricating arrangements
    • F01D25/20—Lubricating arrangements using lubrication pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)

Abstract

Дренажная труба (18) предназначена для установки коаксиально внутри вала (2) турбокомпрессора низкого давления и имеет полую металлическую цилиндрическую часть, длина которой, в сущности, равна длине вала, внутри которого установлена названная труба. Внешняя поверхность металлической части покрыта по меньшей мере на части ее длины композитным материалом на основе волокон (20), которые ориентированы, в сущности, продольно и придают трубе прочности на изгиб.
UAA200506419A 2004-06-29 2005-06-29 Дренажная труба дегазации для вала компрессора низкого давления UA85173C2 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0407139A FR2872218B1 (fr) 2004-06-29 2004-06-29 Tube de degazage pour arbre basse-pression de turbomachine

Publications (1)

Publication Number Publication Date
UA85173C2 true UA85173C2 (ru) 2009-01-12

Family

ID=34948187

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200506419A UA85173C2 (ru) 2004-06-29 2005-06-29 Дренажная труба дегазации для вала компрессора низкого давления

Country Status (9)

Country Link
US (1) US20060254250A1 (ru)
EP (1) EP1626160B1 (ru)
JP (1) JP4667137B2 (ru)
CA (1) CA2510670C (ru)
DE (1) DE602005024088D1 (ru)
ES (1) ES2354163T3 (ru)
FR (1) FR2872218B1 (ru)
RU (1) RU2369779C2 (ru)
UA (1) UA85173C2 (ru)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2970715B1 (fr) * 2011-01-21 2014-10-17 Snecma Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant
FR3030626B1 (fr) * 2014-12-19 2016-12-30 Snecma Dispositif d'accouplement en rotation robuste entre arbres tournants
FI127614B (en) * 2017-04-07 2018-10-15 Patria Aerostructures Oy COMPOSITE ELEMENT AND METHOD FOR MANUFACTURING IT
US20180313225A1 (en) * 2017-04-26 2018-11-01 General Electric Company Methods of cleaning a component within a turbine engine
FR3164504A1 (fr) * 2024-07-09 2026-01-16 Safran Aircraft Engines Systeme d’accouplement ameliore de deux pieces de turbomachine d’aeronef, de preference deux arbres de turbomachine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693248A (en) * 1950-05-03 1954-11-02 Gen Motors Corp Lubrication system
US3518021A (en) * 1968-04-04 1970-06-30 Gen Electric Thrust bearing for compressor
US3901281A (en) * 1972-12-27 1975-08-26 Us Air Force Aircraft fuel line
DE2945272C2 (de) * 1978-11-13 1982-06-09 Ishikawajima-Harima Jukogyo K.K., Tokyo Abgasturbolader
US4272971A (en) * 1979-02-26 1981-06-16 Rockwell International Corporation Reinforced tubular structure
US4383802A (en) * 1981-07-06 1983-05-17 Dunham-Bush, Inc. Oil equalization system for parallel connected compressors
SE463041B (sv) * 1985-11-26 1990-10-01 Stal Refrigeration Ab Regleringsanordning i kyl- och vaermepumpsystem foer reglering av oljetryck och -floede till en oljeinsprutad kompressor med oljefoerraad paa hoegtryckssidan
IT1264905B1 (it) * 1993-07-09 1996-10-17 Saipem Spa Metodo per posare condotte sottomarine in acque profonde
RU2117826C1 (ru) * 1995-03-27 1998-08-20 Акционерное общество открытого типа "А.Люлька-Сатурн" Статор компрессора газотурбинного двигателя
US6354334B1 (en) * 2000-02-25 2002-03-12 Fernand Ellyin Fiber-reinforced composite wrapped steel liner
US6488469B1 (en) * 2000-10-06 2002-12-03 Pratt & Whitney Canada Corp. Mixed flow and centrifugal compressor for gas turbine engine
FR2817289B1 (fr) * 2000-11-30 2003-01-31 Snecma Moteurs Dispositif de centrage d'un tube dans un arbre de turbine
RU2231689C2 (ru) * 2002-05-27 2004-06-27 Открытое акционерное общество "Компрессорный комплекс" Маслосистема газового турбокомпрессора
US7377110B2 (en) * 2004-03-31 2008-05-27 United Technologies Corporation Deoiler for a lubrication system

Also Published As

Publication number Publication date
CA2510670C (fr) 2013-02-19
EP1626160B1 (fr) 2010-10-13
DE602005024088D1 (de) 2010-11-25
ES2354163T3 (es) 2011-03-10
US20060254250A1 (en) 2006-11-16
CA2510670A1 (fr) 2005-12-29
JP4667137B2 (ja) 2011-04-06
FR2872218B1 (fr) 2006-09-29
FR2872218A1 (fr) 2005-12-30
JP2006017121A (ja) 2006-01-19
RU2369779C2 (ru) 2009-10-10
EP1626160A3 (fr) 2007-06-27
EP1626160A2 (fr) 2006-02-15
RU2005120512A (ru) 2007-01-10

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