GB9623195D0 - Gas turbine engine combustor - Google Patents

Gas turbine engine combustor

Info

Publication number
GB9623195D0
GB9623195D0 GBGB9623195.6A GB9623195A GB9623195D0 GB 9623195 D0 GB9623195 D0 GB 9623195D0 GB 9623195 A GB9623195 A GB 9623195A GB 9623195 D0 GB9623195 D0 GB 9623195D0
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
engine combustor
combustor
gas
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.)
Pending
Application number
GBGB9623195.6A
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
Priority to GBGB9623195.6A priority Critical patent/GB9623195D0/en
Publication of GB9623195D0 publication Critical patent/GB9623195D0/en
Priority to EP19970308248 priority patent/EP0841520B1/en
Priority to DE1997619671 priority patent/DE69719671T2/en
Pending legal-status Critical Current

Links

GBGB9623195.6A 1996-11-07 1996-11-07 Gas turbine engine combustor Pending GB9623195D0 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GBGB9623195.6A GB9623195D0 (en) 1996-11-07 1996-11-07 Gas turbine engine combustor
EP19970308248 EP0841520B1 (en) 1996-11-07 1997-10-17 Gas turbine engine combustor
DE1997619671 DE69719671T2 (en) 1996-11-07 1997-10-17 Gas turbine combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9623195.6A GB9623195D0 (en) 1996-11-07 1996-11-07 Gas turbine engine combustor

Publications (1)

Publication Number Publication Date
GB9623195D0 true GB9623195D0 (en) 1997-01-08

Family

ID=10802586

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB9623195.6A Pending GB9623195D0 (en) 1996-11-07 1996-11-07 Gas turbine engine combustor

Country Status (3)

Country Link
EP (1) EP0841520B1 (en)
DE (1) DE69719671T2 (en)
GB (1) GB9623195D0 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10048864A1 (en) 2000-10-02 2002-04-11 Rolls Royce Deutschland Combustion chamber head for a gas turbine
US6923002B2 (en) 2003-08-28 2005-08-02 General Electric Company Combustion liner cap assembly for combustion dynamics reduction
US8312627B2 (en) * 2006-12-22 2012-11-20 General Electric Company Methods for repairing combustor liners
FR3033028B1 (en) * 2015-02-25 2019-12-27 Safran Helicopter Engines COMBUSTION CHAMBER OF A TURBOMACHINE COMPRISING A PENETRANT PART WITH OPENING
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4914918A (en) * 1988-09-26 1990-04-10 United Technologies Corporation Combustor segmented deflector
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
DE4427222A1 (en) * 1994-08-01 1996-02-08 Bmw Rolls Royce Gmbh Heat shield for a gas turbine combustor
DE19508111A1 (en) * 1995-03-08 1996-09-12 Bmw Rolls Royce Gmbh Heat shield arrangement for a gas turbine combustor

Also Published As

Publication number Publication date
EP0841520A2 (en) 1998-05-13
EP0841520B1 (en) 2003-03-12
DE69719671D1 (en) 2003-04-17
EP0841520A3 (en) 1999-11-03
DE69719671T2 (en) 2003-08-14

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