GB294577A - Improvements in low pressure liquid fuel burners - Google Patents

Improvements in low pressure liquid fuel burners

Info

Publication number
GB294577A
GB294577A GB21367/28A GB2136728A GB294577A GB 294577 A GB294577 A GB 294577A GB 21367/28 A GB21367/28 A GB 21367/28A GB 2136728 A GB2136728 A GB 2136728A GB 294577 A GB294577 A GB 294577A
Authority
GB
United Kingdom
Prior art keywords
casing
tube
propeller
cup
air
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
GB21367/28A
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.)
SIDNEY EDWARD MAJOR
Original Assignee
SIDNEY EDWARD MAJOR
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 SIDNEY EDWARD MAJOR filed Critical SIDNEY EDWARD MAJOR
Publication of GB294577A publication Critical patent/GB294577A/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
    • F23D11/04—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying action being obtained by centrifugal action

Abstract

294,577. Major, S. E., and Baker, E. F. July 26, 1927, [Convention date]. Spray burners.-A liquid fuel burner comprises a casing C containing an axially slidable fuel supply tube 4 carrying at its reduced end an atomizing cup 1 fitted with a propeller 5 which is rotated by air at low pressure entering at an inlet 8 and passing to the propeller past a valve 9 carried by the tube 4. The tube 4 is moved axially against the resistance of a spring 16 by a rod 14 operated by means of a cam 17 engaging a boss 20 on the end closure cap 13 of the casing. The movement of the fuel supply tube regulates the escape of air from the casing by adjusting the discharge aperture 21 between the cup 1 and the casing nozzle. The casing nozzle is formed by a perforated tapering annular projection 26 and a circular apertuned plate 27 enclosing an annular recess 25. The oil enters the cup from the tube 4 through a hollow screw 24. To relieve the end thrust on the propeller the space behind a plate 33 loosely fitting in a recess 32 in the valve 9 is connected to the atmosphere by a tube 31. Radial baffle plates may be arranged in the casing to deflect the air leaving the propeller before it issues from the outlet 21. The Specification as open to inspection under Sect. 91 (3) (a) states that the oil may be delivered directly into the cup through a supply tube passing through the side of the casing. This subject-matter does not appear in the Specification as accepted.
GB21367/28A 1927-07-26 1928-07-23 Improvements in low pressure liquid fuel burners Expired GB294577A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AU294577X 1927-07-26

Publications (1)

Publication Number Publication Date
GB294577A true GB294577A (en) 1929-07-11

Family

ID=3717532

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21367/28A Expired GB294577A (en) 1927-07-26 1928-07-23 Improvements in low pressure liquid fuel burners

Country Status (1)

Country Link
GB (1) GB294577A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1186971B (en) * 1957-03-02 1965-02-11 Eberspaecher J Heating device operated with liquid fuel
NL7412422A (en) * 1973-09-19 1975-03-21 Volvo Flygmotor Ab COMBUSTION CHAMBER FOR GAS TURBINE.
GB2224671A (en) * 1988-09-23 1990-05-16 Graco Inc "rotary atomizer"
GB2250697A (en) * 1988-09-23 1992-06-17 Graco Inc Rotary atomizer

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1186971B (en) * 1957-03-02 1965-02-11 Eberspaecher J Heating device operated with liquid fuel
NL7412422A (en) * 1973-09-19 1975-03-21 Volvo Flygmotor Ab COMBUSTION CHAMBER FOR GAS TURBINE.
GB2224671A (en) * 1988-09-23 1990-05-16 Graco Inc "rotary atomizer"
GB2250697A (en) * 1988-09-23 1992-06-17 Graco Inc Rotary atomizer
GB2224671B (en) * 1988-09-23 1992-12-23 Graco Inc Rotary atomizer
GB2250697B (en) * 1988-09-23 1992-12-23 Graco Inc Rotary atomizer

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