GB1289128A - - Google Patents

Info

Publication number
GB1289128A
GB1289128A GB1289128DA GB1289128A GB 1289128 A GB1289128 A GB 1289128A GB 1289128D A GB1289128D A GB 1289128DA GB 1289128 A GB1289128 A GB 1289128A
Authority
GB
United Kingdom
Prior art keywords
flange
skirt
define
wall
flame tube
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
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 filed Critical
Publication of GB1289128A publication Critical patent/GB1289128A/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
    • F23R3/04—Air inlet arrangements

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)

Abstract

1289128 Gas turbine engine combustion equipment JOSEPH LUCAS (INDUSTRIES) Ltd 25 June 1970 [28 March 1969] 16410/69 Heading F1L The invention relates to gas turbine engine combustion equipment in which the flame tube comprises a skirt formed at the joint of two sheet metal elements which form part of the wall of the flame tube. The flame tube shown is of annular form and comprises elements 10, 11 which are welded together where they overlap, the element 10 being formed with an extension which is joggled so as to form an inwardly displaced flange 12. A metal strip 14 is secured to the flange 12 and constitutes the skirt. The flange 12 and the wall element 11 define a space 13 into which air may flow through openings 17. Similarly the skirt 14 and the wall element 10 define a space 15 into which air may flow through openings 16. In Fig.2 the end-wall 111 is joggled to define the flange 112 and the skirt 114 is formed by a strip secured to the flange.
GB1289128D 1969-03-28 1969-03-28 Expired GB1289128A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1641069 1969-03-28

Publications (1)

Publication Number Publication Date
GB1289128A true GB1289128A (en) 1972-09-13

Family

ID=10076823

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1289128D Expired GB1289128A (en) 1969-03-28 1969-03-28

Country Status (1)

Country Link
GB (1) GB1289128A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee