GB9722228D0 - A process for dismantling the front end bearing housing or low pressure compressor shaft component of an aircraft engine - Google Patents

A process for dismantling the front end bearing housing or low pressure compressor shaft component of an aircraft engine

Info

Publication number
GB9722228D0
GB9722228D0 GB9722228A GB9722228A GB9722228D0 GB 9722228 D0 GB9722228 D0 GB 9722228D0 GB 9722228 A GB9722228 A GB 9722228A GB 9722228 A GB9722228 A GB 9722228A GB 9722228 D0 GB9722228 D0 GB 9722228D0
Authority
GB
United Kingdom
Prior art keywords
dismantling
low pressure
bearing housing
pressure compressor
end bearing
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.)
Withdrawn
Application number
GB9722228A
Other versions
GB2320527A (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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
BMW Rolls Royce GmbH
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 BMW Rolls Royce GmbH filed Critical BMW Rolls Royce GmbH
Publication of GB9722228D0 publication Critical patent/GB9722228D0/en
Publication of GB2320527A publication Critical patent/GB2320527A/en
Withdrawn legal-status Critical Current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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9722228A 1996-10-21 1997-10-21 Dismantling or assembling turbine engine front end bearing housing or LP compressor component Withdrawn GB2320527A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1996143336 DE19643336C2 (en) 1996-10-21 1996-10-21 Method for dismantling the front bearing housing or LP compressor shaft part of an aircraft engine

Publications (2)

Publication Number Publication Date
GB9722228D0 true GB9722228D0 (en) 1997-12-17
GB2320527A GB2320527A (en) 1998-06-24

Family

ID=7809300

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9722228A Withdrawn GB2320527A (en) 1996-10-21 1997-10-21 Dismantling or assembling turbine engine front end bearing housing or LP compressor component

Country Status (2)

Country Link
DE (1) DE19643336C2 (en)
GB (1) GB2320527A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101608556B (en) * 2008-06-19 2011-12-14 上海电气电站设备有限公司 Large ground low-pressure internal cylinder
DE102011009770B4 (en) * 2011-01-28 2017-06-29 Lufthansa Technik Ag Method and device for changing a sealing plate and / or a bearing unit in an aircraft engine
RU2593053C2 (en) * 2011-02-09 2016-07-27 Сименс Акциенгезелльшафт Method of removing bearing housing with gas turbine rotor, as well as tubular shaft for continuation of rotor
US10605167B2 (en) 2011-04-15 2020-03-31 United Technologies Corporation Gas turbine engine front center body architecture
EP3779130A1 (en) * 2011-10-17 2021-02-17 Raytheon Technologies Corporation Method of servicing a gas turbine engine and gas turbine engine front center body architecture
EP2610439A1 (en) * 2011-12-30 2013-07-03 Siemens Aktiengesellschaft Method for pulling and/or inserting a turbine bearing and device for performing the method
DE102014210297A1 (en) * 2014-05-30 2015-12-03 Lufthansa Technik Ag Dismantling process for a gas turbine
DE102018112448A1 (en) * 2018-05-24 2019-11-28 Lufthansa Technik Ag Tool for holding the high-pressure shaft of an aircraft engine
DE102019218993A1 (en) * 2019-12-05 2021-06-10 MTU Aero Engines AG SUPPORT ARRANGEMENT FOR HANGING AN AIRCRAFT ENGINE OR MODULE FOR ASSEMBLY OR REVISION PURPOSES
US11725542B2 (en) 2021-07-29 2023-08-15 Pratt & Whitney Canada Corp. Gas turbine engine disassembly / assembly methods
US11926008B2 (en) 2021-12-27 2024-03-12 Pratt & Whitney Canada Corp. Tools and methods for assembling a seal device of a gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1409902A (en) * 1972-05-24 1975-10-15 Rolls Royce Stationary gas turbine power plant mounting apparatus
DE2719850C3 (en) * 1977-05-04 1981-06-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Device for the maintenance of gas turbine engines, in particular gas turbine jet engines
US4451979A (en) * 1980-10-27 1984-06-05 Elliott Turbomachinery Company, Inc. Assembly and disassembly apparatus for use with a rotary machine
US4570053A (en) * 1983-05-04 1986-02-11 General Electric Company Apparatus for heating a turbine wheel
US5220784A (en) * 1991-06-27 1993-06-22 Allied-Signal Inc. Gas turbine engine module assembly
FR2712037B1 (en) * 1993-11-03 1995-12-08 Snecma Compressor turbomachine, the rotor of which has a removable upstream stage.

Also Published As

Publication number Publication date
GB2320527A (en) 1998-06-24
DE19643336A1 (en) 1998-04-23
DE19643336C2 (en) 2002-03-28

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)