GB619353A - Liquid-fuel combustion chamber - Google Patents

Liquid-fuel combustion chamber

Info

Publication number
GB619353A
GB619353A GB3586946A GB3586946A GB619353A GB 619353 A GB619353 A GB 619353A GB 3586946 A GB3586946 A GB 3586946A GB 3586946 A GB3586946 A GB 3586946A GB 619353 A GB619353 A GB 619353A
Authority
GB
United Kingdom
Prior art keywords
tubes
combustion
primary
air
fuel
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
GB3586946A
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB3586946A priority Critical patent/GB619353A/en
Publication of GB619353A publication Critical patent/GB619353A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

619,353. Generating combustion products under pressure. ARMSTRONG SIDDELEY MOTORS, Ltd., and ALLEN, S. Dec. 4, 1946, No. 35869. [Class 51 (i)] Fuel and primary combustion air are admitted at the ends 18 of J-shaped tubes 19 which are surrounded by the burning gases issuing from the backwardly turned ends 20. The quantity of primary air is regulated in agreement with the fuel supply by means of a disc valve 25. Secondary air passes into the chamber 12, containing the tubes 19, through annular openings 34, 35 and, in the construction shown in end view in Fig. 4, through fish-tail burner-like tubes 39 with their down-stream ends reduced to diametral slots 40. The rest of the compressor delivery passes through the annular space 14 to mix with the products of completed combustion. The primary air valve 25 may be coupled with the engine throttle with means for giving an altitude correction. Specifications 577,865 and 603,485 are referred to.
GB3586946A 1946-12-04 1946-12-04 Liquid-fuel combustion chamber Expired GB619353A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3586946A GB619353A (en) 1946-12-04 1946-12-04 Liquid-fuel combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3586946A GB619353A (en) 1946-12-04 1946-12-04 Liquid-fuel combustion chamber

Publications (1)

Publication Number Publication Date
GB619353A true GB619353A (en) 1949-03-08

Family

ID=10382451

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3586946A Expired GB619353A (en) 1946-12-04 1946-12-04 Liquid-fuel combustion chamber

Country Status (1)

Country Link
GB (1) GB619353A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
US2930191A (en) * 1953-01-29 1960-03-29 Phillips Petroleum Co Air-fuel control in prevaporizer type combustion chambers
US4024702A (en) * 1970-09-23 1977-05-24 Perry David Hudson Combustion products pressure generators continuous burner type and engines
US4534166A (en) * 1980-10-01 1985-08-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flow modifying device
US4561257A (en) * 1981-05-20 1985-12-31 Rolls-Royce Limited Gas turbine engine combustion apparatus

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2621477A (en) * 1948-06-03 1952-12-16 Power Jets Res & Dev Ltd Combustion apparatus having valve controlled passages for preheating the fuel-air mixture
US2930191A (en) * 1953-01-29 1960-03-29 Phillips Petroleum Co Air-fuel control in prevaporizer type combustion chambers
US4024702A (en) * 1970-09-23 1977-05-24 Perry David Hudson Combustion products pressure generators continuous burner type and engines
US4534166A (en) * 1980-10-01 1985-08-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flow modifying device
US4561257A (en) * 1981-05-20 1985-12-31 Rolls-Royce Limited Gas turbine engine combustion apparatus

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