FR2930641B1 - COMPONENT TESTING MACHINE OF A TURBOMACHINE - Google Patents

COMPONENT TESTING MACHINE OF A TURBOMACHINE

Info

Publication number
FR2930641B1
FR2930641B1 FR0802290A FR0802290A FR2930641B1 FR 2930641 B1 FR2930641 B1 FR 2930641B1 FR 0802290 A FR0802290 A FR 0802290A FR 0802290 A FR0802290 A FR 0802290A FR 2930641 B1 FR2930641 B1 FR 2930641B1
Authority
FR
France
Prior art keywords
turbomachine
oil
testing machine
component testing
collector
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
FR0802290A
Other languages
French (fr)
Other versions
FR2930641A1 (en
Inventor
Thierry Cayre
Ion Fintescu
Laurent Gille
Serge Rene Morreale
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 FR0802290A priority Critical patent/FR2930641B1/en
Publication of FR2930641A1 publication Critical patent/FR2930641A1/en
Application granted granted Critical
Publication of FR2930641B1 publication Critical patent/FR2930641B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00—Testing of engines
    • G01M15/14—Testing gas-turbine engines or jet-propulsion engines
    • 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
    • F16N—LUBRICATING
    • F16N7/00—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/30—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated the oil being fed or carried along by another fluid
    • F16N7/32—Mist lubrication
    • 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
    • F16N—LUBRICATING
    • F16N7/00—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/38—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated with a separate pump; Central lubrication systems
    • F16N7/40—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated with a separate pump; Central lubrication systems in a closed circulation system

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

Machine (10) d'essai de composants (10, 22, 24, 26) d'une turbomachine, ces composants étant situés dans des enceintes (14, 16, 18) comportant des amenées d'air sous pression, des arrivées d'huile, des retours d'huile vers un réservoir (34), et des tubes de dégazage (50) débouchant dans un collecteur (46) relié à un module de déshuilage (32), ces tubes de dégazage débouchant au dessus du niveau (54) de l'huile contenue dans le collecteur, et le collecteur comprenant une sortie d'huile (57) reliée avec la sortie d'huile (78) du module de déshuilage au réservoir.Machine (10) for testing components (10, 22, 24, 26) of a turbomachine, these components being located in enclosures (14, 16, 18) comprising pressurized air supplies, oil, oil returns to a tank (34), and degassing tubes (50) opening into a manifold (46) connected to a deoiling module (32), these degassing tubes opening above the level (54 ) of the oil contained in the collector, and the collector comprising an oil outlet (57) connected with the oil outlet (78) from the de-oiling module to the tank.

FR0802290A 2008-04-24 2008-04-24 COMPONENT TESTING MACHINE OF A TURBOMACHINE Active FR2930641B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0802290A FR2930641B1 (en) 2008-04-24 2008-04-24 COMPONENT TESTING MACHINE OF A TURBOMACHINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0802290A FR2930641B1 (en) 2008-04-24 2008-04-24 COMPONENT TESTING MACHINE OF A TURBOMACHINE

Publications (2)

Publication Number Publication Date
FR2930641A1 FR2930641A1 (en) 2009-10-30
FR2930641B1 true FR2930641B1 (en) 2010-04-30

Family

ID=40091320

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0802290A Active FR2930641B1 (en) 2008-04-24 2008-04-24 COMPONENT TESTING MACHINE OF A TURBOMACHINE

Country Status (1)

Country Link
FR (1) FR2930641B1 (en)

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE901017C (en) * 1949-02-04 1954-01-07 English Electric Co Ltd Gas turbine with lubricating and sealing device on the bearing
US2613498A (en) * 1949-10-25 1952-10-14 Gen Electric Oil separation and reclaiming means for gas turbine power plants
US3800913A (en) * 1972-08-04 1974-04-02 Caterpillar Tractor Co Recirculating oil system
DE2601133A1 (en) * 1976-01-14 1977-07-21 Motoren Turbinen Union SYSTEM FOR SUPPLYING A COMBUSTION MACHINE WITH LUBRICATING OIL
DE3137947C2 (en) * 1980-09-26 1983-10-27 Rolls-Royce Ltd., London Lubricating oil system for gas turbine engines suitable for any flight maneuver
US5004407A (en) * 1989-09-26 1991-04-02 Sundstrand Corporation Method of scavenging air and oil and gear pump therefor
US6463819B1 (en) * 2000-10-24 2002-10-15 Pratt & Whitney Canada Corp. Uninterruptible oil supply system
US6470666B1 (en) * 2001-04-30 2002-10-29 General Electric Company Methods and systems for preventing gas turbine engine lube oil leakage
US7836675B2 (en) * 2006-02-21 2010-11-23 General Electric Company Supercore sump vent pressure control
FR2903757B1 (en) * 2006-07-11 2011-05-20 Snecma LUBRICATING OIL RECOVERY CIRCUIT OF A BEARING OF A TURBOMACHINE ELEMENT.

Also Published As

Publication number Publication date
FR2930641A1 (en) 2009-10-30

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