GB579511A - Improvements in or relating to jet-propulsion apparatus for aircraft - Google Patents

Improvements in or relating to jet-propulsion apparatus for aircraft

Info

Publication number
GB579511A
GB579511A GB674242A GB674242A GB579511A GB 579511 A GB579511 A GB 579511A GB 674242 A GB674242 A GB 674242A GB 674242 A GB674242 A GB 674242A GB 579511 A GB579511 A GB 579511A
Authority
GB
United Kingdom
Prior art keywords
chamber
combustion chambers
aircraft
tubes
air
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
GB674242A
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 GB674242A priority Critical patent/GB579511A/en
Publication of GB579511A publication Critical patent/GB579511A/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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/54—Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

579,511. Gas turbines. ELLIOTT, A. G. May 18, 1942, No. 6742. [Class 110 (iii)] A gas turbine plant for jet propulsion of an aircraft, comprises a double entry centrifugal compressor 14 delivering into an annular series of tubes 21 which merge into an undivided annular chamber 22. Combustion chambers 25, open at the rear end, are mounted in line with the tubes 21. The chamber 22 has an end cover 23 with a domed portion 123, for each combustion chamber, carrying a fuel injection nozzle 24. Vanes 29 cause a turbulent entry into the combustion chambers of the air passing from the annular chamber 22, jets of air are provided by nozzles 30 and secondary air is introduced at the forward ends of the combustion chambers through holes 31.
GB674242A 1942-05-18 1942-05-18 Improvements in or relating to jet-propulsion apparatus for aircraft Expired GB579511A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB674242A GB579511A (en) 1942-05-18 1942-05-18 Improvements in or relating to jet-propulsion apparatus for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB674242A GB579511A (en) 1942-05-18 1942-05-18 Improvements in or relating to jet-propulsion apparatus for aircraft

Publications (1)

Publication Number Publication Date
GB579511A true GB579511A (en) 1946-08-07

Family

ID=9819948

Family Applications (1)

Application Number Title Priority Date Filing Date
GB674242A Expired GB579511A (en) 1942-05-18 1942-05-18 Improvements in or relating to jet-propulsion apparatus for aircraft

Country Status (1)

Country Link
GB (1) GB579511A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1029618B (en) * 1952-05-06 1958-05-08 Sc Techn H C Eth Alfred Buechi Turbine jet engine
GB2117052A (en) * 1982-03-20 1983-10-05 Penny Turbines Ltd Noel Gas turbine engine
JP2009074793A (en) * 2007-09-24 2009-04-09 Snecma Arrangement of injection system at end wall of aircraft engine combustion chamber

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1029618B (en) * 1952-05-06 1958-05-08 Sc Techn H C Eth Alfred Buechi Turbine jet engine
GB2117052A (en) * 1982-03-20 1983-10-05 Penny Turbines Ltd Noel Gas turbine engine
JP2009074793A (en) * 2007-09-24 2009-04-09 Snecma Arrangement of injection system at end wall of aircraft engine combustion chamber

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