GB703914A - Improvements relating to fuel combustion apparatus - Google Patents

Improvements relating to fuel combustion apparatus

Info

Publication number
GB703914A
GB703914A GB25305/50A GB2530550A GB703914A GB 703914 A GB703914 A GB 703914A GB 25305/50 A GB25305/50 A GB 25305/50A GB 2530550 A GB2530550 A GB 2530550A GB 703914 A GB703914 A GB 703914A
Authority
GB
United Kingdom
Prior art keywords
chamber
air
combustion
combustion chamber
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
GB25305/50A
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 GB25305/50A priority Critical patent/GB703914A/en
Publication of GB703914A publication Critical patent/GB703914A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Abstract

703,914. Liquid fuel combustion chambers. FRASER, R. P. Oct. 4, 1951 [Oct. 17, 1950], No. 25305/50. Class 51 (1) In a fuel combustion apparatus comprising a chamber in the front wall of which is axially mounted a liquid fuel atomizing device adapted to project a wide angled spray means are provided to direct secondary combustion air inwardly and contra to the flow of the atomized fuel stream through passages in the rear wall of the chamber. In the apparatus shown the combustion chamber is of two opposite cones 2, 3 enclosed in outer cylindrical casings 5, 6. A mixture of primary air and fuel is ejected by the burner 7 and secondary air is blown into the chamber in a contra direction to that of the fuel mixture via a set of inlet directing guides 17 and a series of nozzles 11 the secondary air being preheated in the chamber 4 formed between the cone 3 and the casing 6 which it enters through the inlet 9<SP>1</SP>. Secondary air is also supplied to the combustion chamber through the inlet 9, the chamber formed between the cone 2 and casing 5, guides 17 and the nozzles 12. Air from the latter chamber is also caused to circulate around and thereby cool the igniter 10 and an inspection tube (not shown) before entering the combustion chamber. Air is also passed to the combustion chamber via the passages 16. The combustion chamber is lined with refractory and the nozzles 11, 12 may be of refractory or may be refractory lined steel tubes. The hot gases issuing from the outlet 8 may be used in drying apparatus. The size of the combustion chamber may be varied by the inclusion of a cylindrical portion between the end conical portions. Specification 664,676, [Group XI], is referred to.
GB25305/50A 1950-10-17 1950-10-17 Improvements relating to fuel combustion apparatus Expired GB703914A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB25305/50A GB703914A (en) 1950-10-17 1950-10-17 Improvements relating to fuel combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25305/50A GB703914A (en) 1950-10-17 1950-10-17 Improvements relating to fuel combustion apparatus

Publications (1)

Publication Number Publication Date
GB703914A true GB703914A (en) 1954-02-10

Family

ID=10225552

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25305/50A Expired GB703914A (en) 1950-10-17 1950-10-17 Improvements relating to fuel combustion apparatus

Country Status (1)

Country Link
GB (1) GB703914A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2762656A (en) * 1951-10-11 1956-09-11 Reginald P Fraser Liquid atomizer
US2927632A (en) * 1955-02-09 1960-03-08 Fraser Reginald Percy Fuel combustion apparatus and the production of controlled gaseous effluents therefrom
CN108534179A (en) * 2018-06-08 2018-09-14 哈尔滨工业大学 Burner

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2762656A (en) * 1951-10-11 1956-09-11 Reginald P Fraser Liquid atomizer
US2927632A (en) * 1955-02-09 1960-03-08 Fraser Reginald Percy Fuel combustion apparatus and the production of controlled gaseous effluents therefrom
CN108534179A (en) * 2018-06-08 2018-09-14 哈尔滨工业大学 Burner

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