BE677221A - - Google Patents

Info

Publication number
BE677221A
BE677221A BE677221DA BE677221A BE 677221 A BE677221 A BE 677221A BE 677221D A BE677221D A BE 677221DA BE 677221 A BE677221 A BE 677221A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE677221A publication Critical patent/BE677221A/xx

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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F01D25/183—Sealing means
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/72—Sealings
    • F16C33/76—Sealings of ball or roller bearings
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Of Bearings (AREA)
BE677221D 1965-03-01 1966-03-01 BE677221A (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US435924A US3312448A (en) 1965-03-01 1965-03-01 Seal arrangement for preventing leakage of lubricant in gas turbine engines

Publications (1)

Publication Number Publication Date
BE677221A true BE677221A (pl) 1966-08-01

Family

ID=23730382

Family Applications (1)

Application Number Title Priority Date Filing Date
BE677221D BE677221A (pl) 1965-03-01 1966-03-01

Country Status (7)

Country Link
US (1) US3312448A (pl)
BE (1) BE677221A (pl)
CH (1) CH464608A (pl)
DE (1) DE1297939B (pl)
GB (1) GB1092820A (pl)
NL (1) NL6602620A (pl)
SE (1) SE324483B (pl)

Families Citing this family (66)

* Cited by examiner, † Cited by third party
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US3850544A (en) * 1973-11-02 1974-11-26 Gen Electric Mounting arrangement for a bearing of axial flow turbomachinery having variable pitch stationary blades
US4183207A (en) * 1978-03-07 1980-01-15 Avco Corporation Oil-conducting strut for turbine engines
US4671734A (en) * 1984-10-12 1987-06-09 The Boeing Company Dual turbine drive
FR2631386A1 (fr) * 1988-05-11 1989-11-17 Snecma Turbomachine comportant une grille d'entree incorporant des tubes de passage d'huile
US5746574A (en) * 1997-05-27 1998-05-05 General Electric Company Low profile fluid joint
US6102577A (en) * 1998-10-13 2000-08-15 Pratt & Whitney Canada Corp. Isolated oil feed
US7278516B2 (en) * 2004-03-09 2007-10-09 Honeywell International, Inc. Apparatus and method for bearing lubrication in turbine engines
US7610763B2 (en) * 2006-05-09 2009-11-03 United Technologies Corporation Tailorable design configuration topologies for aircraft engine mid-turbine frames
US8312726B2 (en) * 2007-12-21 2012-11-20 United Technologies Corp. Gas turbine engine systems involving I-beam struts
US10132196B2 (en) 2007-12-21 2018-11-20 United Technologies Corporation Gas turbine engine systems involving I-beam struts
US20100132377A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Fabricated itd-strut and vane ring for gas turbine engine
US8061969B2 (en) * 2008-11-28 2011-11-22 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US20100132371A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8347635B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitey Canada Corp. Locking apparatus for a radial locator for gas turbine engine mid turbine frame
US8245518B2 (en) * 2008-11-28 2012-08-21 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8091371B2 (en) * 2008-11-28 2012-01-10 Pratt & Whitney Canada Corp. Mid turbine frame for gas turbine engine
US8347500B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitney Canada Corp. Method of assembly and disassembly of a gas turbine mid turbine frame
US8099962B2 (en) * 2008-11-28 2012-01-24 Pratt & Whitney Canada Corp. Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine
US8231142B2 (en) * 2009-02-17 2012-07-31 Pratt & Whitney Canada Corp. Fluid conduit coupling with leakage detection
US20100275572A1 (en) * 2009-04-30 2010-11-04 Pratt & Whitney Canada Corp. Oil line insulation system for mid turbine frame
US20120023967A1 (en) * 2010-07-30 2012-02-02 Dede Brian C Auxiliary power unit with hot section fire enclosure arrangement
US9316117B2 (en) 2012-01-30 2016-04-19 United Technologies Corporation Internally cooled spoke
WO2013162982A1 (en) 2012-04-27 2013-10-31 General Electric Company Half-spoolie metal seal integral with tube
US9328626B2 (en) 2012-08-21 2016-05-03 United Technologies Corporation Annular turbomachine seal and heat shield
ITMI20130848A1 (it) * 2013-05-24 2014-11-25 Ansaldo Energia Spa Cassa di scarico di un gruppo turbina
US10711631B2 (en) * 2014-12-24 2020-07-14 Raytheon Technologies Corporation Turbine engine with guide vanes forward of its fan blades
US9995171B2 (en) * 2015-01-16 2018-06-12 United Technologies Corporation Cooling passages for a mid-turbine frame
US10000293B2 (en) 2015-01-23 2018-06-19 General Electric Company Gas-electric propulsion system for an aircraft
FR3036437B1 (fr) * 2015-05-22 2017-05-05 Snecma Ensemble de turbomachine pour lubrifier un support de palier
US9683458B2 (en) 2015-08-20 2017-06-20 Pratt & Whitney Canada Corp. Oil scupper system for bearing housing of gas turbine engine
US9821917B2 (en) 2015-09-21 2017-11-21 General Electric Company Aft engine for an aircraft
US9884687B2 (en) 2015-09-21 2018-02-06 General Electric Company Non-axis symmetric aft engine
US9637217B2 (en) 2015-09-21 2017-05-02 General Electric Company Aircraft having an aft engine
US9815560B2 (en) * 2015-09-21 2017-11-14 General Electric Company AFT engine nacelle shape for an aircraft
US9957055B2 (en) 2015-09-21 2018-05-01 General Electric Company Aft engine for an aircraft
US10017270B2 (en) 2015-10-09 2018-07-10 General Electric Company Aft engine for an aircraft
US9764848B1 (en) 2016-03-07 2017-09-19 General Electric Company Propulsion system for an aircraft
US10392119B2 (en) 2016-04-11 2019-08-27 General Electric Company Electric propulsion engine for an aircraft
US10392120B2 (en) 2016-04-19 2019-08-27 General Electric Company Propulsion engine for an aircraft
US10252810B2 (en) 2016-04-19 2019-04-09 General Electric Company Propulsion engine for an aircraft
US10676205B2 (en) 2016-08-19 2020-06-09 General Electric Company Propulsion engine for an aircraft
US10800539B2 (en) * 2016-08-19 2020-10-13 General Electric Company Propulsion engine for an aircraft
US11105340B2 (en) 2016-08-19 2021-08-31 General Electric Company Thermal management system for an electric propulsion engine
US10093428B2 (en) 2016-08-22 2018-10-09 General Electric Company Electric propulsion system
US10308366B2 (en) 2016-08-22 2019-06-04 General Electric Company Embedded electric machine
US10487839B2 (en) 2016-08-22 2019-11-26 General Electric Company Embedded electric machine
US10071811B2 (en) 2016-08-22 2018-09-11 General Electric Company Embedded electric machine
US10520035B2 (en) 2016-11-04 2019-12-31 United Technologies Corporation Variable volume bearing compartment
US20180128122A1 (en) * 2016-11-04 2018-05-10 United Technologies Corporation Apparatus and method for providing fluid to a bearing damper
US10830139B2 (en) 2017-02-06 2020-11-10 Raytheon Technologies Corporation Fitting for multiwall tube
US10393303B2 (en) 2017-02-06 2019-08-27 United Technologies Corporation Threaded fitting for tube
US10385710B2 (en) 2017-02-06 2019-08-20 United Technologies Corporation Multiwall tube and fitting for bearing oil supply
US10465828B2 (en) 2017-02-06 2019-11-05 United Technologies Corporation Tube fitting
US10822103B2 (en) 2017-02-10 2020-11-03 General Electric Company Propulsor assembly for an aircraft
US11149578B2 (en) 2017-02-10 2021-10-19 General Electric Company Propulsion system for an aircraft
US10793281B2 (en) 2017-02-10 2020-10-06 General Electric Company Propulsion system for an aircraft
US10137981B2 (en) 2017-03-31 2018-11-27 General Electric Company Electric propulsion system for an aircraft
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
US10737797B2 (en) * 2017-07-21 2020-08-11 General Electric Company Vertical takeoff and landing aircraft
US10612415B2 (en) * 2017-08-29 2020-04-07 United Technologies Corporation Fluid communication between a stationary structure and a rotating structure
US10767867B2 (en) * 2018-03-21 2020-09-08 Raytheon Technologies Corporation Bearing support assembly
US10781710B2 (en) * 2018-07-17 2020-09-22 Raytheon Technologies Corporation Sealing configuration to reduce air leakage
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine
US11319836B2 (en) * 2019-08-14 2022-05-03 Pratt & Whitney Canada Corp. Lubricant drain conduit for gas turbine engine
US11352979B2 (en) * 2020-04-24 2022-06-07 Raytheon Technologies Corporation Housing less front bearing compartment for gas turbine engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB623615A (en) * 1947-05-06 1949-05-19 Frederick William Walton Morle Improvements in or relating to gas-turbine-engines
DE909692C (de) * 1951-10-16 1954-04-22 Svenska Turbinfab Ab Radialturbine fuer elastisches Treibmittel mit mehrere konzentrische Kammern enthaltendem Aufnehmer

Also Published As

Publication number Publication date
DE1297939B (de) 1969-06-19
GB1092820A (en) 1967-11-29
CH464608A (de) 1968-10-31
SE324483B (pl) 1970-06-01
NL6602620A (pl) 1966-09-02
US3312448A (en) 1967-04-04

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