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

Improvements in or relating to gas turbine engines

Info

Publication number
GB1284440A
GB1284440A GB60035/69A GB6003569A GB1284440A GB 1284440 A GB1284440 A GB 1284440A GB 60035/69 A GB60035/69 A GB 60035/69A GB 6003569 A GB6003569 A GB 6003569A GB 1284440 A GB1284440 A GB 1284440A
Authority
GB
United Kingdom
Prior art keywords
relating
gas turbine
turbine engines
heading
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
GB60035/69A
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 GB60035/69A priority Critical patent/GB1284440A/en
Priority to US95124A priority patent/US3690093A/en
Priority to DE2060158A priority patent/DE2060158C3/en
Priority to FR7044353A priority patent/FR2073176A5/en
Publication of GB1284440A publication Critical patent/GB1284440A/en
Expired legal-status Critical Current

Links

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Air Supply (AREA)

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.
GB60035/69A 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines Expired GB1284440A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB60035/69A GB1284440A (en) 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines
US95124A US3690093A (en) 1969-12-09 1970-12-04 Fuel injector for a gas turbine engine
DE2060158A DE2060158C3 (en) 1969-12-09 1970-12-07 Fuel injector for a gas turbine jet engine
FR7044353A FR2073176A5 (en) 1969-12-09 1970-12-09 FUEL INJECTOR GAS TURBINE ENGINE COMBUSTION EQUIPMENT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB60035/69A GB1284440A (en) 1969-12-09 1969-12-09 Improvements in or relating to gas turbine engines

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
GB60035/69A 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 (27)

* 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
GB2055187B (en) * 1979-08-01 1983-12-14 Rolls Royce Gaseous fuel injector for a gas turbine engine
GB2055186B (en) * 1979-08-01 1983-05-25 Rolls Royce Gas turbine engine dual fuel injector
US4344280A (en) * 1980-01-24 1982-08-17 Hitachi, Ltd. Combustor of gas turbine
JPS5741524A (en) * 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
DE3405400A1 (en) * 1984-01-26 1985-08-01 József 8000 München Previcz Mixture-forming valve for the introduction of a fuel-air mixture into the intake line of a combustion system
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
US11692488B2 (en) 2020-11-04 2023-07-04 Delavan Inc. Torch igniter cooling system
US11473505B2 (en) 2020-11-04 2022-10-18 Delavan Inc. Torch igniter cooling system
US11608783B2 (en) 2020-11-04 2023-03-21 Delavan, Inc. Surface igniter cooling system
US11635027B2 (en) * 2020-11-18 2023-04-25 Collins Engine Nozzles, Inc. Fuel systems for torch ignition devices
US11421602B2 (en) 2020-12-16 2022-08-23 Delavan Inc. Continuous ignition device exhaust manifold
US11635210B2 (en) 2020-12-17 2023-04-25 Collins Engine Nozzles, Inc. Conformal and flexible woven heat shields for gas turbine engine components
US11486309B2 (en) 2020-12-17 2022-11-01 Delavan Inc. Axially oriented internally mounted continuous ignition device: removable hot surface igniter
US11754289B2 (en) 2020-12-17 2023-09-12 Delavan, Inc. Axially oriented internally mounted continuous ignition device: removable nozzle
US12092333B2 (en) 2020-12-17 2024-09-17 Collins Engine Nozzles, Inc. Radially oriented internally mounted continuous ignition device
US11680528B2 (en) 2020-12-18 2023-06-20 Delavan Inc. Internally-mounted torch igniters with removable igniter heads
US11209164B1 (en) 2020-12-18 2021-12-28 Delavan Inc. Fuel injector systems for torch igniters

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

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLE Entries relating assignments, transmissions, licences in the register of patents
PCNP Patent ceased through non-payment of renewal fee