GB1445015A - Gas turbine engines - Google Patents

Gas turbine engines

Info

Publication number
GB1445015A
GB1445015A GB5732673A GB5732673A GB1445015A GB 1445015 A GB1445015 A GB 1445015A GB 5732673 A GB5732673 A GB 5732673A GB 5732673 A GB5732673 A GB 5732673A GB 1445015 A GB1445015 A GB 1445015A
Authority
GB
United Kingdom
Prior art keywords
shaft
engine
turbine
power
drive
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
GB5732673A
Other languages
English (en)
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB1445015A publication Critical patent/GB1445015A/en
Expired legal-status Critical Current

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
    • 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
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Rolling Contact Bearings (AREA)
GB5732673A 1972-12-26 1973-12-11 Gas turbine engines Expired GB1445015A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00318280A US3823553A (en) 1972-12-26 1972-12-26 Gas turbine with removable self contained power turbine module

Publications (1)

Publication Number Publication Date
GB1445015A true GB1445015A (en) 1976-08-04

Family

ID=23237476

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5732673A Expired GB1445015A (en) 1972-12-26 1973-12-11 Gas turbine engines

Country Status (8)

Country Link
US (1) US3823553A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS5727292B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BE (1) BE809056A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA986731A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2364431C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2211589B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1445015A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1002233B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3041157A1 (de) * 1979-11-03 1981-05-07 Rolls-Royce Ltd., London Gasturbinentriebwerk
GB2219046A (en) * 1988-05-13 1989-11-29 United Technologies Corp Disassembly of a modular fan gas turbine engine
US20220290617A1 (en) * 2019-09-27 2022-09-15 Safran Aircraft Engines Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contact

Families Citing this family (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1438195A (en) * 1973-08-08 1976-06-03 Penny Turbines Ltd Noel Mounting for attaching a tubular member in co-axial registration with an aperture in a wall
DE2525950A1 (de) * 1975-06-11 1976-12-16 Motoren Turbinen Union Gasturbinentriebwerk in baukastenbauweise
US4030288A (en) * 1975-11-10 1977-06-21 Caterpillar Tractor Co. Modular gas turbine engine assembly
US4083180A (en) * 1976-10-01 1978-04-11 Caterpillar Tractor Co. Gas turbine engine internal insulation
US4201426A (en) * 1978-04-27 1980-05-06 General Electric Company Bearing clamping assembly for a gas turbine engine
US4592204A (en) * 1978-10-26 1986-06-03 Rice Ivan G Compression intercooled high cycle pressure ratio gas generator for combined cycles
US4251987A (en) * 1979-08-22 1981-02-24 General Electric Company Differential geared engine
JPS5644426A (en) * 1979-09-14 1981-04-23 Ngk Spark Plug Co Ltd Supercharger
FR2544387B1 (fr) * 1983-04-15 1985-06-14 Snecma Appareillage pour le transfert d'un module de turbine complet d'une machine d'equilibrage a un moteur et vice versa, et procede pour la mise en oeuvre dudit appareillage
US4611464A (en) * 1984-05-02 1986-09-16 United Technologies Corporation Rotor assembly for a gas turbine engine and method of disassembly
US4685286A (en) * 1984-05-02 1987-08-11 United Technologies Corporation Method of disassembly for a gas turbine engine
US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
DE3614182A1 (de) * 1985-04-29 1986-11-06 Teledyne Industries, Inc., Los Angeles, Calif. Turbine
JPS6296399U (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1985-12-07 1987-06-19
US4744214A (en) * 1987-06-29 1988-05-17 United Technologies Corporation Engine modularity
FR2644844B1 (fr) * 1989-03-23 1994-05-06 Snecma Suspension du rotor de la turbine basse pression d'une turbomachine a double corps
US5205513A (en) * 1991-09-26 1993-04-27 General Electric Company Method and system for the removal of large turbine engines
US5226788A (en) * 1991-12-23 1993-07-13 General Electric Company Turbine heat shield and bolt retainer assembly
US5211541A (en) 1991-12-23 1993-05-18 General Electric Company Turbine support assembly including turbine heat shield and bolt retainer assembly
US5537814A (en) * 1994-09-28 1996-07-23 General Electric Company High pressure gas generator rotor tie rod system for gas turbine engine
EP0844369B1 (en) * 1996-11-23 2002-01-30 ROLLS-ROYCE plc A bladed rotor and surround assembly
US6053697A (en) * 1998-06-26 2000-04-25 General Electric Company Trilobe mounting with anti-rotation apparatus for an air duct in a gas turbine rotor
SE519323C2 (sv) * 2001-06-28 2003-02-11 Volvo Aero Ab Moduluppbyggd gasturbin
US7409819B2 (en) * 2004-10-29 2008-08-12 General Electric Company Gas turbine engine and method of assembling same
GB0502324D0 (en) * 2005-03-14 2005-03-16 Rolls Royce Plc A multi-shaft arrangement for a turbine engine
US7510371B2 (en) * 2005-06-06 2009-03-31 General Electric Company Forward tilted turbine nozzle
US7513102B2 (en) * 2005-06-06 2009-04-07 General Electric Company Integrated counterrotating turbofan
US7594388B2 (en) * 2005-06-06 2009-09-29 General Electric Company Counterrotating turbofan engine
FR2889561B1 (fr) * 2005-08-02 2010-10-29 Snecma Systeme d'etancheite de la chambre de lubrification arriere d'un turboreacteur
US20070220895A1 (en) * 2005-09-19 2007-09-27 General Electric Company Methods and apparatus for housing gas turbine engines
FR2906846B1 (fr) * 2006-10-06 2008-12-26 Snecma Sa Canal de transition entre deux etages de turbine
US8162605B2 (en) * 2008-01-14 2012-04-24 United Technologies Corporation Gas turbine engine case
FR2932227B1 (fr) * 2008-06-09 2011-07-01 Snecma Turboreacteur double flux
FR2944558B1 (fr) * 2009-04-17 2014-05-02 Snecma Moteur a turbine a gaz double corps pourvu d'un palier de turbine bp supplementaire.
US8517687B2 (en) * 2010-03-10 2013-08-27 United Technologies Corporation Gas turbine engine compressor and turbine section assembly utilizing tie shaft
US20110219784A1 (en) * 2010-03-10 2011-09-15 St Mary Christopher Compressor section with tie shaft coupling and cantilever mounted vanes
US8459943B2 (en) * 2010-03-10 2013-06-11 United Technologies Corporation Gas turbine engine rotor sections held together by tie shaft, and with blade rim undercut
US20110219781A1 (en) * 2010-03-10 2011-09-15 Daniel Benjamin Gas turbine engine with tie shaft for axial high pressure compressor rotor
US9212557B2 (en) 2011-08-31 2015-12-15 United Technologies Corporation Assembly and method preventing tie shaft unwinding
US8932011B2 (en) * 2011-10-06 2015-01-13 United Technologies Corporation Shaft assembly for a gas turbine engine
US20130156584A1 (en) * 2011-12-16 2013-06-20 Carney R. Anderson Compressor rotor with internal stiffening ring of distinct material
US20130195647A1 (en) * 2012-01-31 2013-08-01 Marc J. Muldoon Gas turbine engine bearing arrangement including aft bearing hub geometry
US9476320B2 (en) 2012-01-31 2016-10-25 United Technologies Corporation Gas turbine engine aft bearing arrangement
US20130340435A1 (en) * 2012-01-31 2013-12-26 Gregory M. Savela Gas turbine engine aft spool bearing arrangement and hub wall configuration
US20150226125A1 (en) * 2012-09-26 2015-08-13 United Technologies Corporation Combined high pressure turbine case and turbine intermediate case
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
CN108223429B (zh) * 2017-09-30 2021-03-30 中国航发沈阳发动机研究所 整环不断盘的风扇机匣
US11725542B2 (en) 2021-07-29 2023-08-15 Pratt & Whitney Canada Corp. Gas turbine engine disassembly / assembly methods
CN115324741B (zh) * 2022-08-12 2025-08-15 中国航发沈阳发动机研究所 一种涡扇发动机高空左边界加力接通控制方法及装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2444363A (en) * 1944-08-30 1948-06-29 United Aircraft Corp Helical spline torque indicator
US2747367A (en) * 1950-03-21 1956-05-29 United Aircraft Corp Gas turbine power plant supporting structure
US2757857A (en) * 1951-06-19 1956-08-07 United Aircraft Corp Locking means between compressor and turbine
US2862356A (en) * 1954-07-16 1958-12-02 Rolls Royce Bearing arrangements for gas-turbine engines
US2971334A (en) * 1955-01-04 1961-02-14 Solar Aircraft Co Gas turbine engine adaptable for multi-purpose use
US2851246A (en) * 1956-10-24 1958-09-09 United Aircraft Corp Turbine or compressor construction and method of assembly
US2916874A (en) * 1957-01-31 1959-12-15 United Aircraft Corp Engine construction
US3088278A (en) * 1957-05-01 1963-05-07 Avco Mfg Corp Gas turbine engine
DE1128706B (de) * 1957-05-01 1962-04-26 Avco Mfg Corp Gasturbinenanlage mit einer sich durch die Verdichterantriebs-turbine erstreckenden Antriebswelle der Nutzleistungsturbine
GB846329A (en) * 1957-12-12 1960-08-31 Napier & Son Ltd Combustion turbine power units
DE1091818B (de) * 1958-02-10 1960-10-27 United Aircraft Corp Schmiervorrichtung fuer eine innerhalb einer drehbaren Hohlwelle liegende Schmierstelle
GB1139941A (en) * 1965-03-30 1969-01-15 Rolls Royce Engine drive

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3041157A1 (de) * 1979-11-03 1981-05-07 Rolls-Royce Ltd., London Gasturbinentriebwerk
GB2219046A (en) * 1988-05-13 1989-11-29 United Technologies Corp Disassembly of a modular fan gas turbine engine
US20220290617A1 (en) * 2019-09-27 2022-09-15 Safran Aircraft Engines Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contact
US12110829B2 (en) * 2019-09-27 2024-10-08 Safran Aircraft Engines Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contact

Also Published As

Publication number Publication date
DE2364431C2 (de) 1984-04-19
JPS4996112A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1974-09-11
IT1002233B (it) 1976-05-20
JPS5727292B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1982-06-09
FR2211589A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1974-07-19
BE809056A (fr) 1974-04-16
DE2364431A1 (de) 1974-06-27
US3823553A (en) 1974-07-16
CA986731A (en) 1976-04-06
FR2211589B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1980-09-05

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
746 Register noted 'licences of right' (sect. 46/1977)
PE20 Patent expired after termination of 20 years

Effective date: 19931210