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    • 49. 发明专利
    • Improvements in or relating to methods of, and apparatus for, the combustion of gaseous fuel
    • GB581091A
    • 1946-10-01
    • GB1339544
    • 1944-07-13
    • SELAS CORP OF AMERICA
    • F23C3/00F23D14/00
    • 581,091. Combustion chambers of furnaces. FORRESTER, H. J. C. (Selas Corporation of America). July 13, 1944, No. 13395. [Class 51 (i)] [Also in Group XI] A gas burner comprises a substantially closed chamber with an inlet having a number of small passages to which gas mixture is supplied, an inner lining of high temperature refractory material being formed with a single restricted outlet from which issues a stream of high temperature combustion products at a high velocity. As shown in Figs. 1 and 2, the burner comprises a metal shell 11 secured to a base 12 and enclosing the refractory body made in two parts 21, 22, the former having a single orifice 25. The inlet passages are formed by channels 28 in a refractory, threaded member 27, having a flattened head, screwed into a nipple connection 14. The outlet may be formed as a long, narrow slit in a projecting portion of the lining, or as a ring. The metal shell may be fitted with a jacket through which the fuel mixture passes to the inlet, and the inner walls of the lining may be ridged. Figs. 12, 13 and 14 show a form in which an elongated and irregular outlet 25e is located in a recess 49 in which the work may be placed. The base has a number of separate inlets 15e, the fuel mixture passing through passages 41e formed between thin plates stacked together ; cross ribs 46e are provided in the inlet chambers 34e. The combustion chamber 23e is elliptical in section and the casing is fitted with a cooling jacket 11e.