DE69530557D1 - Brennkammerbauweise - Google Patents

Brennkammerbauweise

Info

Publication number
DE69530557D1
DE69530557D1 DE69530557T DE69530557T DE69530557D1 DE 69530557 D1 DE69530557 D1 DE 69530557D1 DE 69530557 T DE69530557 T DE 69530557T DE 69530557 T DE69530557 T DE 69530557T DE 69530557 D1 DE69530557 D1 DE 69530557D1
Authority
DE
Germany
Prior art keywords
combustion chamber
chamber design
design
combustion
chamber
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 - Fee Related
Application number
DE69530557T
Other languages
English (en)
Other versions
DE69530557T2 (de
Inventor
Leighton Jones
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 PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE69530557D1 publication Critical patent/DE69530557D1/de
Application granted granted Critical
Publication of DE69530557T2 publication Critical patent/DE69530557T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K25/00Uniting components to form integral members, e.g. turbine wheels and shafts, caulks with inserts, with or without shaping of the components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50Combustion chambers comprising an annular flame tube within an annular casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/13Parts of turbine combustion chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/30Retaining components in desired mutual position

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Plates (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Ceramic Products (AREA)
DE69530557T 1994-12-08 1995-11-28 Brennkammerbauweise Expired - Fee Related DE69530557T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9425038 1994-12-08
GB9425038A GB2295887A (en) 1994-12-08 1994-12-08 Combustor assembly

Publications (2)

Publication Number Publication Date
DE69530557D1 true DE69530557D1 (de) 2003-06-05
DE69530557T2 DE69530557T2 (de) 2004-04-08

Family

ID=10765796

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69530557T Expired - Fee Related DE69530557T2 (de) 1994-12-08 1995-11-28 Brennkammerbauweise

Country Status (4)

Country Link
US (1) US5609031A (de)
EP (1) EP0716267B1 (de)
DE (1) DE69530557T2 (de)
GB (1) GB2295887A (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6212753B1 (en) * 1997-11-25 2001-04-10 General Electric Company Complaint joint for interfacing dissimilar metals in X-ray tubes
FR2825779B1 (fr) * 2001-06-06 2003-08-29 Snecma Moteurs Chambre de combustion munie d'un systeme de fixation de fond de chambre
FR2897417A1 (fr) * 2006-02-10 2007-08-17 Snecma Sa Chambre de combustion annulaire d'une turbomachine
FR2897923B1 (fr) * 2006-02-27 2008-06-06 Snecma Sa Chambre de combustion annulaire a fond amovible
PL2748444T3 (pl) * 2011-08-22 2019-11-29 Majed Toqan Komora spalania cylindryczno-pierścieniowa z rozstawionymi, stycznymi dyszami paliwowo-powietrznymi do zastosowania w silnikach turbinowych
EP2748531B1 (de) * 2011-08-22 2017-12-06 CPS-Holding Limited Injektionsverfahren von Verbrennungsedukten in eine Brennkammer
CN104053883B (zh) * 2011-08-22 2017-02-15 马吉德·托甘 混合用于在燃气涡轮发动机内燃烧的燃烧反应物的方法
US9651258B2 (en) 2013-03-15 2017-05-16 Rolls-Royce Corporation Shell and tiled liner arrangement for a combustor
US10168052B2 (en) 2013-09-04 2019-01-01 United Technologies Corporation Combustor bulkhead heat shield
US10935240B2 (en) 2015-04-23 2021-03-02 Raytheon Technologies Corporation Additive manufactured combustor heat shield
US20170059165A1 (en) 2015-08-28 2017-03-02 Rolls-Royce High Temperature Composites Inc. Cmc cross-over tube
EP3299720B1 (de) * 2016-09-22 2020-11-04 Ansaldo Energia IP UK Limited Brennkammerfrontanordnung für eine gasturbine
US10663167B2 (en) * 2017-06-16 2020-05-26 General Electric Company Combustor assembly with CMC combustor dome
DE102018213925A1 (de) 2018-08-17 2020-02-20 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerbaugruppe mit Schindelbauteil und Positonierungshilfe
US11215367B2 (en) 2019-10-03 2022-01-04 Raytheon Technologies Corporation Mounting a ceramic component to a non-ceramic component in a gas turbine engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2858673A (en) * 1955-06-28 1958-11-04 Gen Electric Sectional liner structure for combustor
US3854503A (en) * 1971-08-05 1974-12-17 Lucas Industries Ltd Flame tubes
GB1423052A (en) * 1973-03-27 1976-01-28 British Leyland Uk Ltd Combustion chamber assembly for a gas turbine engine
US3880575A (en) * 1974-04-15 1975-04-29 Gen Motors Corp Ceramic combustion liner
US4363208A (en) * 1980-11-10 1982-12-14 General Motors Corporation Ceramic combustor mounting
US4843825A (en) * 1988-05-16 1989-07-04 United Technologies Corporation Combustor dome heat shield
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
JPH0375414A (ja) * 1989-08-15 1991-03-29 Nissan Motor Co Ltd ガスタービン燃焼器
GB9018014D0 (en) * 1990-08-16 1990-10-03 Rolls Royce Plc Gas turbine engine combustor
DE69306025T2 (de) * 1992-03-30 1997-05-28 Gen Electric Konstruktion eines Brennkammerdomes
US5307637A (en) * 1992-07-09 1994-05-03 General Electric Company Angled multi-hole film cooled single wall combustor dome plate

Also Published As

Publication number Publication date
EP0716267A2 (de) 1996-06-12
GB2295887A (en) 1996-06-12
US5609031A (en) 1997-03-11
GB9425038D0 (en) 1995-02-15
EP0716267A3 (de) 1999-01-13
EP0716267B1 (de) 2003-05-02
DE69530557T2 (de) 2004-04-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee