GB543918A - Improvements and relating to combustion chambers - Google Patents

Improvements and relating to combustion chambers

Info

Publication number
GB543918A
GB543918A GB15797/40A GB1579740A GB543918A GB 543918 A GB543918 A GB 543918A GB 15797/40 A GB15797/40 A GB 15797/40A GB 1579740 A GB1579740 A GB 1579740A GB 543918 A GB543918 A GB 543918A
Authority
GB
United Kingdom
Prior art keywords
conduits
combustion chamber
combustion
suspended
annular space
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
GB15797/40A
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.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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 Brown Boveri und Cie AG Germany, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Publication of GB543918A publication Critical patent/GB543918A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

543,918. Combustion chambers. AKT.-GES. BROWN, BOVERI, & CIE. Oct. 28, 1940, No. 15797. Convention date, Sept. 29, 1939. [Class 51 (i)] A combustion chamber 4, Fig. 1, for generating .gases for heating and power purposes, is formed of a number of overlapping sheet metal conduits 8 through the spaces between which air is supplied at high velocity from an annular space 5 enclosed between the wall 6 of the combustion chamber and an outer casing 7. Part of the air supplied by a conduit 1 passes direct to the combustion chamber to support combustion of fuel from the nozzle 3 and the remainder passes to the annular space 5. The conduits 8 are suspended in such a manner that they may expand freely and are spaced apart by ribs 13 as shown in Fig. 2. The conduits may be suspended by links 10 or flexible metal strips. Fig. 5 shows radial strips 12 on the conduits engaging with rails 11 on the casing 7. The conduits may be conical or cylindrical and stepped as shown at 15 in Fig. 7. Each conduit section 8 may be formed of several parts as shown at 14 in Fig. 5.
GB15797/40A 1939-09-29 1940-10-28 Improvements and relating to combustion chambers Expired GB543918A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH543918X 1939-09-29

Publications (1)

Publication Number Publication Date
GB543918A true GB543918A (en) 1942-03-19

Family

ID=4519243

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15797/40A Expired GB543918A (en) 1939-09-29 1940-10-28 Improvements and relating to combustion chambers

Country Status (1)

Country Link
GB (1) GB543918A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172987A (en) * 1972-12-19 1986-10-01 Gen Electric Combustion chamber construction
GB2256899A (en) * 1991-05-10 1992-12-23 Mtu Muenchen Gmbh Nozzle wall construction.
EP1887209A2 (en) 2006-07-25 2008-02-13 United Technologies Corporation Hanger system for a cooling liner within a gas turbine engine exhaust duct
EP1887208A2 (en) 2006-07-25 2008-02-13 United Technologies Corporation Attachment hanger system for a cooling liner within a gas turbine engine exhaust duct
EP2093487A3 (en) * 2008-02-21 2013-11-27 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber with ceramic flame tube
EP2927594A3 (en) * 2014-03-11 2016-02-17 Rolls-Royce Deutschland Ltd & Co KG Combustion chamber of a gas turbine

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2172987A (en) * 1972-12-19 1986-10-01 Gen Electric Combustion chamber construction
GB2256899A (en) * 1991-05-10 1992-12-23 Mtu Muenchen Gmbh Nozzle wall construction.
GB2256899B (en) * 1991-05-10 1995-02-08 Mtu Muenchen Gmbh Nozzle wall
EP1887209A2 (en) 2006-07-25 2008-02-13 United Technologies Corporation Hanger system for a cooling liner within a gas turbine engine exhaust duct
EP1887208A2 (en) 2006-07-25 2008-02-13 United Technologies Corporation Attachment hanger system for a cooling liner within a gas turbine engine exhaust duct
EP1887208A3 (en) * 2006-07-25 2010-11-17 United Technologies Corporation Attachment hanger system for a cooling liner within a gas turbine engine exhaust duct
EP1887209A3 (en) * 2006-07-25 2010-11-17 United Technologies Corporation Hanger system for a cooling liner within a gas turbine engine exhaust duct
EP2093487A3 (en) * 2008-02-21 2013-11-27 Rolls-Royce Deutschland Ltd & Co KG Gas turbine combustion chamber with ceramic flame tube
EP2927594A3 (en) * 2014-03-11 2016-02-17 Rolls-Royce Deutschland Ltd & Co KG Combustion chamber of a gas turbine
US9366436B2 (en) 2014-03-11 2016-06-14 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine

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