GB843712A - Burner construction - Google Patents

Burner construction

Info

Publication number
GB843712A
GB843712A GB2292/58A GB229258A GB843712A GB 843712 A GB843712 A GB 843712A GB 2292/58 A GB2292/58 A GB 2292/58A GB 229258 A GB229258 A GB 229258A GB 843712 A GB843712 A GB 843712A
Authority
GB
United Kingdom
Prior art keywords
passages
fuel
air
port
space
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
GB2292/58A
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.)
Bloom Engineering Co Inc
Original Assignee
Bloom Engineering Co Inc
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 Bloom Engineering Co Inc filed Critical Bloom Engineering Co Inc
Publication of GB843712A publication Critical patent/GB843712A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space

Landscapes

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

Abstract

843,712. Burners. BLOOM ENGINEERING CO. Inc. Jan. 23, 1958 [April 11, 1957], No. 2292/58. Class 75(1). A burner construction for use with a flaring port in a furnace comprises a tubular body 18 having a tip portion 19 from which extends a cylindrical wall 21 defining a recess 22 accommodating a refractory block 27, the front of the recess conforming to the size of the rear of the port 16, the wall 21 being spaced from the body 18, means for supply fuel and combustion air to the space 26 so formed and a plurality of discharge passages 25 to provide tangential discharge in front of but adjacent the flaring face 29 of the port. Fuel, which may be gas or atomized oil, is supplied by a pipe 38 leading to exits 39 into the space 26. Air passes from an inlet 31 through a chamber 30 to an annular passage leading to the space 26. In a modification, Fig. 3 (not shown), the passages 25 are replaced by separate passages for fuel and air. Alternatively, passages for the fuel may open into the passages 25, air only being supplied to the outer ends of these.
GB2292/58A 1957-04-11 1958-01-23 Burner construction Expired GB843712A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US843712XA 1957-04-11 1957-04-11

Publications (1)

Publication Number Publication Date
GB843712A true GB843712A (en) 1960-08-10

Family

ID=22184529

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2292/58A Expired GB843712A (en) 1957-04-11 1958-01-23 Burner construction

Country Status (1)

Country Link
GB (1) GB843712A (en)

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