GB266416A - Improvements in burners for pulverised and gaseous fuel - Google Patents

Improvements in burners for pulverised and gaseous fuel

Info

Publication number
GB266416A
GB266416A GB2641625A GB2641625A GB266416A GB 266416 A GB266416 A GB 266416A GB 2641625 A GB2641625 A GB 2641625A GB 2641625 A GB2641625 A GB 2641625A GB 266416 A GB266416 A GB 266416A
Authority
GB
United Kingdom
Prior art keywords
inlet
nozzle
passages
gas
casing
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
GB2641625A
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 GB2641625A priority Critical patent/GB266416A/en
Publication of GB266416A publication Critical patent/GB266416A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D1/00Burners for combustion of pulverulent fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/14Special features of gas burners
    • F23D2900/14002Special features of gas burners of premix or non premix types, specially adapted for the combustion of low heating value [LHV] gas

Landscapes

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

Abstract

266,416. Vedder, W. Oct. 22, 1925. Pulverulent fuel, gas, and blowpipe burners.- A burner, particularly for inferior pulverulent fuel, comprises a central fuel supply pipe b, surrounded by three groups of spiral passages pl, p<2>, p<3>, communicating respectively with a chamber h having an inlet g, through ports q with a chamber d<1> having an inlet d, and with the atmosphere through inlets, formed in the end wall k of the casing a and controlled by a hit-and-miss valve m. To assist the combustion of the pulverulent fuel, the burner is supplied with a rich gas through the inlet g and with air through the valve w or with compressed air through the inlet d or it is supplied with a poor gas through the inlet d and with compressed air through the inlet g, the valve m being closed. The gas may be used alone, the tube b being closed. The passages p<1> are of smaller cross-sectional area than the passages p<2>, p<3>. The pulverulent fuel is given a whirling and spreading motion by means of downwardly and tangentially arranged passages t leading from the chamber h or by means of spiral ribs arranged between the flared end of the tube b and a central conical spreader. The lower nozzle portion of the casing a may be provided with a cooling jacket and may be fixed and terminate in a cylindrical portion having an inwardly directed flange at the outer end or it may be conical and terminate in a flared outlet A<2>. In the latter case, the bulged top A<1> of the jacketed nozzle A may be supported by a plate D, secured to a curved flange a<2> on the casing a, so that the nozzle may be swung in a plane by rotating a rod B, which is connected by a universal joint B<1> to the nozzle and is threaded through a nut C trunnionmounted in a bracket C<2> on the plate D. A second rod B may be provided for adjusting the nozzle in a plane at right angles.
GB2641625A 1925-10-22 1925-10-22 Improvements in burners for pulverised and gaseous fuel Expired GB266416A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2641625A GB266416A (en) 1925-10-22 1925-10-22 Improvements in burners for pulverised and gaseous fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2641625A GB266416A (en) 1925-10-22 1925-10-22 Improvements in burners for pulverised and gaseous fuel

Publications (1)

Publication Number Publication Date
GB266416A true GB266416A (en) 1927-02-22

Family

ID=10243309

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2641625A Expired GB266416A (en) 1925-10-22 1925-10-22 Improvements in burners for pulverised and gaseous fuel

Country Status (1)

Country Link
GB (1) GB266416A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2123945A (en) * 1982-07-14 1984-02-08 Mitsui Shipbuilding Eng Method of burning low calorific gas and burner for low calorific gas

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2123945A (en) * 1982-07-14 1984-02-08 Mitsui Shipbuilding Eng Method of burning low calorific gas and burner for low calorific gas

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