GB1369503A - Air supply control arrangement for a flame tube for a gas turbine engine - Google Patents

Air supply control arrangement for a flame tube for a gas turbine engine

Info

Publication number
GB1369503A
GB1369503A GB434371A GB434371A GB1369503A GB 1369503 A GB1369503 A GB 1369503A GB 434371 A GB434371 A GB 434371A GB 434371 A GB434371 A GB 434371A GB 1369503 A GB1369503 A GB 1369503A
Authority
GB
United Kingdom
Prior art keywords
chamber
gas turbine
turbine engine
control arrangement
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
GB434371A
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries Ltd
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 Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB434371A priority Critical patent/GB1369503A/en
Publication of GB1369503A publication Critical patent/GB1369503A/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

Landscapes

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

Abstract

1369503 Gas turbine engine combustion equipment testing JOSEPH LUCAS (INDUSTRIES) Ltd 31 Jan 1972 [ 10 Feb 1971] 4343/71 Heading F1L The invention relates to an air supply control arrangement for testing the effects of swirling air-flow on a flame tube of a gas turbine engine. The combustion apparatus comprises a casing in which the flame tube 10 is disposed, the casing having an annular inlet 11. The control arrangement 12 comprises an annular chamber 13 having an inlet 14 and an annular outlet 15 which is aligned with the inlet 11. A plurality of second inlets are provided into the chamber 13 each being adopted to direct air into the chamber transversely of the axis whereby air leaving the outlet 15 has a swirling motion about the axis of the chamber. The second inlets are defined by a plurality of vanes 17 which lie in planes parallel to the axis of the chamber. Air is supplied to the second inlets through a passage 18.
GB434371A 1972-01-31 1972-01-31 Air supply control arrangement for a flame tube for a gas turbine engine Expired GB1369503A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB434371A GB1369503A (en) 1972-01-31 1972-01-31 Air supply control arrangement for a flame tube for a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB434371A GB1369503A (en) 1972-01-31 1972-01-31 Air supply control arrangement for a flame tube for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1369503A true GB1369503A (en) 1974-10-09

Family

ID=9775399

Family Applications (1)

Application Number Title Priority Date Filing Date
GB434371A Expired GB1369503A (en) 1972-01-31 1972-01-31 Air supply control arrangement for a flame tube for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB1369503A (en)

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Legal Events

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