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GB919303A - Improvements relating to reheat systems for gas turbine engines - Google Patents

Improvements relating to reheat systems for gas turbine engines

Info

Publication number
GB919303A
GB919303A GB3538260A GB3538260A GB919303A GB 919303 A GB919303 A GB 919303A GB 3538260 A GB3538260 A GB 3538260A GB 3538260 A GB3538260 A GB 3538260A GB 919303 A GB919303 A GB 919303A
Authority
GB
United Kingdom
Prior art keywords
segment
gas turbine
reheat
controlled
turbine engines
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
GB3538260A
Inventor
Arthur Henry Lefebvre
Robert Arthur Rice
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 GB3538260A priority Critical patent/GB919303A/en
Publication of GB919303A publication Critical patent/GB919303A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants

Landscapes

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

Abstract

919,303. Generating combustion products under pressure. ROLLS-ROYCE Ltd. Sept. 6, 1961 [Oct. 14, 1960], No. 35382/60. Class 51 (1). [Also in Group XXVI] A gas turbine reheat system comprises one or more reheat stabilizers each of which is formed by a circular gutter divided into separate sections and has its own individually controllable separate fuel supply. Two rings 20, 21 of segmental stabilizer gutters in a jet pipe are fed with fuel from injector nozzles through radial pipes 22, 23, each pipe being associated with a segment and controlled by a valve 24 or 25, supplied by a main fuel manifold 26 controlled by a cock 27. Each segment may be separated from the adjacent segment by an air gap, a baffle plate or both.
GB3538260A 1960-10-14 1960-10-14 Improvements relating to reheat systems for gas turbine engines Expired GB919303A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3538260A GB919303A (en) 1960-10-14 1960-10-14 Improvements relating to reheat systems for gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3538260A GB919303A (en) 1960-10-14 1960-10-14 Improvements relating to reheat systems for gas turbine engines

Publications (1)

Publication Number Publication Date
GB919303A true GB919303A (en) 1963-02-20

Family

ID=10377119

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3538260A Expired GB919303A (en) 1960-10-14 1960-10-14 Improvements relating to reheat systems for gas turbine engines

Country Status (1)

Country Link
GB (1) GB919303A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2330867A1 (en) * 1975-11-04 1977-06-03 Gen Electric REMOVABLE FLAME STABILIZER

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2330867A1 (en) * 1975-11-04 1977-06-03 Gen Electric REMOVABLE FLAME STABILIZER

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