GB1284440A - Improvements in or relating to gas turbine engines - Google Patents

Improvements in or relating to gas turbine engines

Info

Publication number
GB1284440A
GB1284440A GB6003569A GB6003569A GB1284440A GB 1284440 A GB1284440 A GB 1284440A GB 6003569 A GB6003569 A GB 6003569A GB 6003569 A GB6003569 A GB 6003569A GB 1284440 A GB1284440 A GB 1284440A
Authority
GB
United Kingdom
Prior art keywords
relating
improvements
gas turbine
turbine engines
dec
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
GB6003569A
Inventor
Denis Richard Carlisle
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 GB6003569A priority Critical patent/GB1284440A/en
Publication of GB1284440A publication Critical patent/GB1284440A/en
Application status is Expired legal-status Critical

Links

Classifications

    • 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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/36Supply of different fuels

Abstract

1284440 Spray burners ROLLS ROYCE Ltd 9 Dec 1969 60035/69 Heading F4T The subject matter is substantially identical with that of Specification 1284439 but the claims are directed to the fact that one nozzle can be connected selectively to a fuel or air supply.
GB6003569A 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines Expired GB1284440A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB6003569A GB1284440A (en) 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB6003569A GB1284440A (en) 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines
US3690093D US3690093A (en) 1969-12-09 1970-12-04 Fuel injector for a gas turbine engine
DE19702060158 DE2060158C3 (en) 1969-12-09 1970-12-07
FR7044353A FR2073176A5 (en) 1969-12-09 1970-12-09 Injector equipment fuel engine combustion gas turbine

Publications (1)

Publication Number Publication Date
GB1284440A true GB1284440A (en) 1972-08-09

Family

ID=10484880

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6003569A Expired GB1284440A (en) 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines

Country Status (4)

Country Link
US (1) US3690093A (en)
DE (1) DE2060158C3 (en)
FR (1) FR2073176A5 (en)
GB (1) GB1284440A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1377184A (en) * 1971-02-02 1974-12-11 Secr Defence Gas turbine engine combustion apparatus
US3768250A (en) * 1971-12-01 1973-10-30 Mitsubishi Heavy Ind Ltd Combustion apparatus for a gas turbine
US4327547A (en) * 1978-11-23 1982-05-04 Rolls-Royce Limited Fuel injectors
GB2050592B (en) * 1979-06-06 1983-03-16 Rolls Royce Gas turbine
GB2055186B (en) * 1979-08-01 1983-05-25 Rolls Royce Gas turbine engine dual fuel injector
GB2055187B (en) * 1979-08-01 1983-12-14 Rolls Royce Gaseous fuel injector for a gas turbine engine
US4344280A (en) * 1980-01-24 1982-08-17 Hitachi, Ltd. Combustor of gas turbine
JPS6233490B2 (en) * 1980-08-25 1987-07-21 Hitachi Ltd
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
DE3405400C2 (en) * 1984-01-26 1991-05-02 Jozsef 8000 Muenchen De Previcz
US5564271A (en) * 1994-06-24 1996-10-15 United Technologies Corporation Pressure vessel fuel nozzle support for an industrial gas turbine engine
US8499739B2 (en) * 2006-08-31 2013-08-06 Caterpillar Inc. Injector having tangentially oriented purge line
US8215100B2 (en) * 2007-03-02 2012-07-10 Caterpillar Inc. Regeneration device having external check valve
US20100095649A1 (en) * 2008-10-20 2010-04-22 General Electric Company Staged combustion systems and methods
US10012387B2 (en) * 2014-12-05 2018-07-03 General Electric Company Fuel supply system for a gas turbine engine
US9791153B2 (en) * 2015-02-27 2017-10-17 United Technologies Corporation Line replaceable fuel nozzle apparatus, system and method

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1877942A (en) * 1930-05-16 1932-09-20 Albert W Morse Combination gas and oil burner
US2595759A (en) * 1948-11-30 1952-05-06 Gen Electric Atomizing nozzle for spraying viscous liquids
US2635425A (en) * 1949-09-07 1953-04-21 Westinghouse Electric Corp Dual flow fuel nozzle system having means to inject air in response to low fuel pressure
US2907527A (en) * 1956-04-10 1959-10-06 Thompson Ramo Wooldridge Inc Nozzle
GB985739A (en) * 1963-11-11 1965-03-10 Rolls Royce Fuel injector for a gas turbine engine

Also Published As

Publication number Publication date
DE2060158C3 (en) 1981-07-23
US3690093A (en) 1972-09-12
DE2060158B2 (en) 1980-10-16
DE2060158A1 (en) 1972-06-08
FR2073176A5 (en) 1971-09-24

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Legal Events

Date Code Title Description
PS Patent sealed
PLE Entries relating assignments, transmissions, licences in the register of patents
PCNP Patent ceased through non-payment of renewal fee