GB661498A - Improvements in or relating to combustion chambers, particularly for gas turbines - Google Patents

Improvements in or relating to combustion chambers, particularly for gas turbines

Info

Publication number
GB661498A
GB661498A GB13884/49A GB1388449A GB661498A GB 661498 A GB661498 A GB 661498A GB 13884/49 A GB13884/49 A GB 13884/49A GB 1388449 A GB1388449 A GB 1388449A GB 661498 A GB661498 A GB 661498A
Authority
GB
United Kingdom
Prior art keywords
mixing air
chamber
distributer
rotational
same
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
GB13884/49A
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.)
Rheinmetall Air Defence AG
Maschinenfabrik Oerlikon AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Maschinenfabrik Oerlikon AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG, Maschinenfabrik Oerlikon AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of GB661498A publication Critical patent/GB661498A/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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex

Landscapes

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

Abstract

661,498. Generating combustion products under pressure. MASCHINENFABRIK OERLIKON. May 24, 1949 [Oct,. 26. 1948], No. 13884/49. Class 51. (i). In a combustion chamber for gaseous, powdered or liquid fuel particularly for gas turbines and having a fuel injector 2 on the axis, the primary, secondary and mixing air flow into a distribution chamber 5 from which the mixing air is projected along the wall of the combustion chamber helicoidally through a distributer 4 and due to centrifugal force tends to bear against the wall of the chamber to form a heat-insulating layer. The secondary air flows through a distributer which gives it either a rotational movement in the same or the opposite direction to that of the mixing air or a non-rotational forward movement parallel to the axis of the chamber. Primary air flows through the inlet 3 and is also given either a rotational movement in the same or the opposite direction to that of the mixing air or a non- rotational forward movement. Additional mixing air may be supplied through a distributer which gives it a rotational movement in the 'same direction as the mixing air.
GB13884/49A 1948-10-26 1949-05-24 Improvements in or relating to combustion chambers, particularly for gas turbines Expired GB661498A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH661498X 1948-10-26

Publications (1)

Publication Number Publication Date
GB661498A true GB661498A (en) 1951-11-21

Family

ID=4526927

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13884/49A Expired GB661498A (en) 1948-10-26 1949-05-24 Improvements in or relating to combustion chambers, particularly for gas turbines

Country Status (4)

Country Link
BE (1) BE490776A (en)
CH (1) CH274976A (en)
FR (1) FR993342A (en)
GB (1) GB661498A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1131947B (en) * 1959-03-28 1962-06-20 Maschf Augsburg Nuernberg Ag Combustion process for gas turbine combustion chambers and equipment for carrying out the process
CH428324A (en) * 1964-05-21 1967-01-15 Prvni Brnenska Strojirna Combustion chamber
FR2605053A1 (en) * 1986-10-14 1988-04-15 Gen Electric MULTIPLE COMBUSTIBLE AIRCRAFT AND ITS PROPULSION SYSTEM
DE4226028A1 (en) * 1992-08-06 1994-02-10 Asea Brown Boveri Process for operating a gas turbine plant

Also Published As

Publication number Publication date
BE490776A (en)
FR993342A (en) 1951-10-30
CH274976A (en) 1951-04-30

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