FR2526866B1 - Moyen en vue de controler la pression de balayage d'air dans le compartiment des paliers des turbines a gaz - Google Patents

Moyen en vue de controler la pression de balayage d'air dans le compartiment des paliers des turbines a gaz

Info

Publication number
FR2526866B1
FR2526866B1 FR8307106A FR8307106A FR2526866B1 FR 2526866 B1 FR2526866 B1 FR 2526866B1 FR 8307106 A FR8307106 A FR 8307106A FR 8307106 A FR8307106 A FR 8307106A FR 2526866 B1 FR2526866 B1 FR 2526866B1
Authority
FR
France
Prior art keywords
controlling
gas turbines
bearing compartment
air scan
scan pressure
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.)
Expired
Application number
FR8307106A
Other languages
English (en)
Other versions
FR2526866A1 (fr
Inventor
James Reynolds Norris
Harrison Reynolds Picard
Claude Peter Rotondo
John Daniel Robinson Jr
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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
Priority claimed from US06/377,758 external-priority patent/US4441311A/en
Priority claimed from US06/377,746 external-priority patent/US4433539A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of FR2526866A1 publication Critical patent/FR2526866A1/fr
Application granted granted Critical
Publication of FR2526866B1 publication Critical patent/FR2526866B1/fr
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
FR8307106A 1982-05-13 1983-04-29 Moyen en vue de controler la pression de balayage d'air dans le compartiment des paliers des turbines a gaz Expired FR2526866B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/377,758 US4441311A (en) 1982-05-13 1982-05-13 Means for controlling the air scavenge pressure in the bearing compartment of a gas turbine engine
US06/377,746 US4433539A (en) 1982-05-13 1982-05-13 Means for controlling air scavenge pressure in the bearing compartment of gas turbines

Publications (2)

Publication Number Publication Date
FR2526866A1 FR2526866A1 (fr) 1983-11-18
FR2526866B1 true FR2526866B1 (fr) 1988-09-09

Family

ID=27007944

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8307106A Expired FR2526866B1 (fr) 1982-05-13 1983-04-29 Moyen en vue de controler la pression de balayage d'air dans le compartiment des paliers des turbines a gaz

Country Status (2)

Country Link
FR (1) FR2526866B1 (fr)
GB (1) GB2119858B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3826217A1 (de) * 1988-08-02 1990-02-08 Mtu Muenchen Gmbh Gasturbine mit einer verdichterseitigen lagerkammer
US20030097872A1 (en) * 2001-11-29 2003-05-29 Granitz Charles Robert System for reducing oil consumption in gas turbine engines
GB201412869D0 (en) 2014-07-21 2014-09-03 Rolls Royce Plc Pressure controlled chamber
US10520035B2 (en) * 2016-11-04 2019-12-31 United Technologies Corporation Variable volume bearing compartment
FR3075308B1 (fr) * 2017-12-14 2020-07-03 Safran Aircraft Engines Enceinte de lubrification d'au moins un palier d'une turbomachine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB702931A (en) * 1951-04-18 1954-01-27 Bristol Aeroplane Co Ltd Improvements in or relating to rotary machines comprising fluid compressing means
US2672010A (en) * 1951-07-14 1954-03-16 United Aircraft Corp Pressurized lubrication system for gas turbines
US2991845A (en) * 1959-04-10 1961-07-11 Westinghouse Electric Corp Lubrication system for a gas turbine engine
US3027971A (en) * 1960-04-13 1962-04-03 Jr Albert E Ketler Engine lubrication system
DE1207713B (de) * 1962-02-13 1965-12-23 Boelkow Gmbh Einrichtung zum Abdichten und Schmieren von hochbeanspruchten Wellenlagern
US3378104A (en) * 1966-03-08 1968-04-16 Gen Electric Air-oil separators for use in gas turbine engines
US3722624A (en) * 1971-06-07 1973-03-27 Gen Electric Bearing seal and oil tank ventilation system
CH557952A (de) * 1972-11-08 1975-01-15 Bbc Sulzer Turbomaschinen Gasturbinenanlage.

Also Published As

Publication number Publication date
GB2119858A (en) 1983-11-23
FR2526866A1 (fr) 1983-11-18
GB2119858B (en) 1985-05-30

Similar Documents

Publication Publication Date Title
JPS57193747A (en) Variable area exhaust nozzle assembled body for gas turbine engine
IT1163508B (it) Guarnizione di tenuta all'aria esterna rivestita in ceramica per motori a turbina a gas
GB2226086B (en) Gas turbine engine frame
GB2096699B (en) Controlling the inlet pressure of a combustion engine
GB8921450D0 (en) Improvements in or relating to gas turbine engines
IT1125926B (it) Struttura di supporto della guarnizione di tenuta all'aria esterna per motori a turbina a gas
JPS566024A (en) Air inlet port for gas turbine engine
FR2485090B1 (fr) Joint d'etancheite entre le rotor de turbine d'un moteur a turbine a gaz et la structure statique dudit moteur
IT1124668B (it) Tenuta per l'aria di raffreddamento di turbomotori a gas
AT384279B (de) Einrichtung zur regelung des verbrennungsluftverh|ltnisses bei einem gasmotor mit magerer betriebsweise
ES512224A0 (es) "valvula de recirculacion de los gases de escape y procedimiento para controlar la valvula".
GB8624833D0 (en) Intake for turbopropeller gas turbine engine
FR2545538B1 (fr) Propulseur a turbines a gaz avec des dispositifs pour minimiser l'interstice des aubes
EP0210070A3 (en) Air inlet filter for gas turbine engine
FR2557209B1 (fr) Structure de stator destinee a supporter un joint d'etancheite a l'air exterieur dans un moteur a turbine a gaz.
GB2095335B (en) Gas turbine engine air intake system
ITMI931182A1 (it) Dispositivo per l'azionamento di almeno un dispositivo di turbolenza comandante la portata di aria per la combustione di un bruciatore per propulsori a turbine a gas
FR2526866B1 (fr) Moyen en vue de controler la pression de balayage d'air dans le compartiment des paliers des turbines a gaz
IT1207299B (it) Uniforme di un letto catalizzaotre dispositivo per l'alimentazione con un gas di scarico da depurare.
HK73483A (en) Inlet air flow passage arrangement in diesel engines
IT1153044B (it) Presa d'aria per motore a turbina a gas
GB2158883B (en) Gas turbine engine cooling air supply
JPS57140527A (en) Engine using liquified air and liquified natural gas
USD273696S (en) Water purification ionic gas generator
USD273411S (en) Water purification ionic gas generator

Legal Events

Date Code Title Description
ST Notification of lapse