GB892890A - Annular combustion chamber reinforcing means - Google Patents

Annular combustion chamber reinforcing means

Info

Publication number
GB892890A
GB892890A GB3801658A GB3801658A GB892890A GB 892890 A GB892890 A GB 892890A GB 3801658 A GB3801658 A GB 3801658A GB 3801658 A GB3801658 A GB 3801658A GB 892890 A GB892890 A GB 892890A
Authority
GB
United Kingdom
Prior art keywords
chamber
turbine
combustion chamber
casing
annular combustion
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
GB3801658A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3801658A priority Critical patent/GB892890A/en
Publication of GB892890A publication Critical patent/GB892890A/en
Expired legal-status Critical Current

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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

892,890. Generating combustion products under pressure. PURVIS, J. T. Nov. 25, 1958, No. 38016/58. Class 51 (1). In a gas turbine having a large diameter annular combustion chamber, coaxial with the turbine, the outer wall of the chamber is supported, at its central circumference, by brackets mounted on the inner surface of the turbine outer casing and on the outer surface of the combustion chamber. Limited radial movement of the chamber outer wall is permitted by the brackets which each consist of two mutually engaging parts, T-shaped member 6, mounted on chamber 2 by welding at 6b, and U-shaped member 5, mounted on the turbine casing (not shown) by welding at the base 5a. The legs 5b and 5c of member 5 have inwardly directed flanges 5e which are bent under the head 6c of member 6 and spaced from it to permit relative radial movement of the casing and chamber.
GB3801658A 1958-11-25 1958-11-25 Annular combustion chamber reinforcing means Expired GB892890A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3801658A GB892890A (en) 1958-11-25 1958-11-25 Annular combustion chamber reinforcing means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3801658A GB892890A (en) 1958-11-25 1958-11-25 Annular combustion chamber reinforcing means

Publications (1)

Publication Number Publication Date
GB892890A true GB892890A (en) 1962-04-04

Family

ID=10400606

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3801658A Expired GB892890A (en) 1958-11-25 1958-11-25 Annular combustion chamber reinforcing means

Country Status (1)

Country Link
GB (1) GB892890A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117102A (en) * 1982-03-20 1983-10-05 Rolls Royce Improvements in or relating to mounting arrangements for combustion equipment
US5067324A (en) * 1990-04-04 1991-11-26 United Technologies Corporation Engine nozzle liner retainer
CN102635875A (en) * 2011-02-09 2012-08-15 西门子公司 Combustion chamber casing

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2117102A (en) * 1982-03-20 1983-10-05 Rolls Royce Improvements in or relating to mounting arrangements for combustion equipment
US5067324A (en) * 1990-04-04 1991-11-26 United Technologies Corporation Engine nozzle liner retainer
CN102635875A (en) * 2011-02-09 2012-08-15 西门子公司 Combustion chamber casing
CN102635875B (en) * 2011-02-09 2016-05-04 西门子公司 Combustion box

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