GB1059199A – Flame tube
– Google Patents
GB1059199A – Flame tube
– Google Patents
Flame tube
Info
Publication number
GB1059199A
GB1059199A
GB44503/65A
GB4450365A
GB1059199A
GB 1059199 A
GB1059199 A
GB 1059199A
GB 44503/65 A
GB44503/65 A
GB 44503/65A
GB 4450365 A
GB4450365 A
GB 4450365A
GB 1059199 A
GB1059199 A
GB 1059199A
Authority
GB
United Kingdom
Prior art keywords
supplied
cooling air
upstream section
flame tube
combustion
Prior art date
1965-10-20
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
GB44503/65A
Inventor
Martin Land
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.)
1965-10-20
Filing date
1965-10-20
Publication date
1967-02-15
1965-10-20
Application filed by Rolls Royce PLC
filed
Critical
Rolls Royce PLC
1965-10-20
Priority to GB44503/65A
priority
Critical
patent/GB1059199A/en
1966-10-12
Priority to US586298A
priority
patent/US3385054A/en
1966-10-18
Priority to FR80461A
priority
patent/FR1496982A/en
1967-02-15
Publication of GB1059199A
publication
Critical
patent/GB1059199A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
Classifications
F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
Abstract
1,059,199. Gas turbine combustion chambers. ROLLS-ROYCE Ltd. Oct. 20, 1965, No. 44503/65. Heading F1L. A gas turbine engine combustion chamber flame tube having a series of axially consecutive sections 20 with annular cooling air gaps 21 therebetween each containing a corrugated spacer 22 has a one piece part-spherical ceramic member 30 mounted in the upstream section 20 by means of expansion joints 31. The member 30 may be made of sintered silicon nitride and is not supplied with cooling air on its interior surface so that it is maintained very hot by the primary combustion occurring within it, thus promoting combustion. A fuel/primary air mixture is supplied through inlet 24 past swirler 25. Cooling air is supplied to upstream section 20 through apertures 32. In a modification, the downstream end of member 30 extends to the downstream end of the upstream section 20. The construction is applicable also to an annular flame tube.
GB44503/65A
1965-10-20
1965-10-20
Flame tube
Expired
GB1059199A
(en)
Priority Applications (3)
Application Number
Priority Date
Filing Date
Title
GB44503/65A
GB1059199A
(en)
1965-10-20
1965-10-20
Flame tube
US586298A
US3385054A
(en)
1965-10-20
1966-10-12
Flame tube
FR80461A
FR1496982A
(en)
1965-10-20
1966-10-18
Flame tube for combustion chamber of a turbo-reactor
Applications Claiming Priority (1)
Application Number
Priority Date
Filing Date
Title
GB44503/65A
GB1059199A
(en)
1965-10-20
1965-10-20
Flame tube
Publications (1)
Publication Number
Publication Date
GB1059199A
true
GB1059199A
(en)
1967-02-15
Family
ID=10433609
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB44503/65A
Expired
GB1059199A
(en)
1965-10-20
1965-10-20
Flame tube
Country Status (2)
Country
Link
US
(1)
US3385054A
(en)
GB
(1)
GB1059199A
(en)
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
JPS5334247B1
(en)
*
1971-06-11
1978-09-19
Families Citing this family (7)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
JPS5418561Y2
(en)
*
1975-07-08
1979-07-12
WO1981002762A1
(en)
*
1980-03-19
1981-10-01
J Bailey
Vaporizing combustor tube
FR2599821B1
(en)
*
1986-06-04
1988-09-02
Snecma
COMBUSTION CHAMBER FOR TURBOMACHINES WITH MIXING HOLES PROVIDING THE POSITIONING OF THE HOT WALL ON THE COLD WALL
US5144793A
(en)
*
1990-12-24
1992-09-08
United Technologies Corporation
Integrated connector/airtube for a turbomachine’s combustion chamber walls
US6397603B1
(en)
*
2000-05-05
2002-06-04
The United States Of America As Represented By The Secretary Of The Air Force
Conbustor having a ceramic matrix composite liner
US8745989B2
(en)
*
2009-04-09
2014-06-10
Pratt & Whitney Canada Corp.
Reverse flow ceramic matrix composite combustor
CN105737204B
(en)
*
2016-03-04
2018-01-26
武汉英康汇通电气有限公司
A kind of whirlwind burner inner liner and its turbogenerator
Family Cites Families (4)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
US2686655A
(en)
*
1949-09-02
1954-08-17
Maschf Augsburg Nuernberg Ag
Joint between ceramic and metallic parts
US2602292A
(en)
*
1951-03-31
1952-07-08
Gen Electric
Fuel-air mixing device
US2958194A
(en)
*
1951-09-24
1960-11-01
Power Jets Res & Dev Ltd
Cooled flame tube
US2956399A
(en)
*
1956-11-16
1960-10-18
Clair M Beighley
Fluid cooled homogeneous ceramic rocket motor wall structure
1965
1965-10-20
GB
GB44503/65A
patent/GB1059199A/en
not_active
Expired
1966
1966-10-12
US
US586298A
patent/US3385054A/en
not_active
Expired – Lifetime
Cited By (1)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
JPS5334247B1
(en)
*
1971-06-11
1978-09-19
Also Published As
Publication number
Publication date
US3385054A
(en)
1968-05-28
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None