GB701320A - Improvements in or relating to combustion equipment of gas-turbine engines - Google Patents

Improvements in or relating to combustion equipment of gas-turbine engines

Info

Publication number
GB701320A
GB701320A GB31665/50A GB3166550A GB701320A GB 701320 A GB701320 A GB 701320A GB 31665/50 A GB31665/50 A GB 31665/50A GB 3166550 A GB3166550 A GB 3166550A GB 701320 A GB701320 A GB 701320A
Authority
GB
United Kingdom
Prior art keywords
combustion equipment
turbine engines
gas
relating
gas turbine
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
GB31665/50A
Inventor
Francis Murray Johnson
John Bertram Holliday
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 GB31665/50A priority Critical patent/GB701320A/en
Publication of GB701320A publication Critical patent/GB701320A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/185—Liquid cooling
    • 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
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • 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
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

701,320. Gas turbine plant. ROLLS-ROYCE, Ltd. March 26, 1952 [Dec. 29, 1950], No. 31665/50. Drawings to Specification. Class 110 (3). [Also in Group XII] In combustion equipment of gas turbine engines, (see Group XII), the fuel supply may be preheated byepassing it through the hollow turbine inlet nozzle guide vanes which are thereby cooled.
GB31665/50A 1950-12-29 1950-12-29 Improvements in or relating to combustion equipment of gas-turbine engines Expired GB701320A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB31665/50A GB701320A (en) 1950-12-29 1950-12-29 Improvements in or relating to combustion equipment of gas-turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB31665/50A GB701320A (en) 1950-12-29 1950-12-29 Improvements in or relating to combustion equipment of gas-turbine engines

Publications (1)

Publication Number Publication Date
GB701320A true GB701320A (en) 1953-12-23

Family

ID=10326555

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31665/50A Expired GB701320A (en) 1950-12-29 1950-12-29 Improvements in or relating to combustion equipment of gas-turbine engines

Country Status (1)

Country Link
GB (1) GB701320A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1029195B (en) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Tube combustion chamber for internal combustion turbines, in particular aircraft internal combustion turbines
DE1029196B (en) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Annular combustion chamber for internal combustion turbines, especially aircraft internal combustion turbines
US2955420A (en) * 1955-09-12 1960-10-11 Phillips Petroleum Co Jet engine operation
US2974487A (en) * 1957-10-19 1961-03-14 Bristol Siddeley Engines Ltd Combustion system for a gas turbine engine
US3026675A (en) * 1958-08-22 1962-03-27 Snecma Device for the air intake into the primary zone of a combustion chamber in a turbo-machine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955420A (en) * 1955-09-12 1960-10-11 Phillips Petroleum Co Jet engine operation
DE1029195B (en) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Tube combustion chamber for internal combustion turbines, in particular aircraft internal combustion turbines
DE1029196B (en) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Annular combustion chamber for internal combustion turbines, especially aircraft internal combustion turbines
US2974487A (en) * 1957-10-19 1961-03-14 Bristol Siddeley Engines Ltd Combustion system for a gas turbine engine
US3026675A (en) * 1958-08-22 1962-03-27 Snecma Device for the air intake into the primary zone of a combustion chamber in a turbo-machine

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