GB597205A - Improvements in method and apparatus for the combustion of fuel - Google Patents

Improvements in method and apparatus for the combustion of fuel

Info

Publication number
GB597205A
GB597205A GB27075/45A GB2707545A GB597205A GB 597205 A GB597205 A GB 597205A GB 27075/45 A GB27075/45 A GB 27075/45A GB 2707545 A GB2707545 A GB 2707545A GB 597205 A GB597205 A GB 597205A
Authority
GB
United Kingdom
Prior art keywords
under pressure
combustion chamber
products under
combustion products
annular passages
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
GB27075/45A
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.)
RALPH CADY BRIERLY
Original Assignee
RALPH CADY BRIERLY
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 RALPH CADY BRIERLY filed Critical RALPH CADY BRIERLY
Publication of GB597205A publication Critical patent/GB597205A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls

Landscapes

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

Abstract

597,205. Generating combustion products under pressure. BONVILLIAN, C. A., BRIERLY, R. C., and LETVIN, S. Sept. 6, 1943, No. 27075/45. Convention date, March 13, 1943. Divided out of 597,151. Drawings to Specification. [Class 51 (i)] [Also in Group XIII] In fluid-fuel fired apparatus for generating combustion products under pressure for.use in gas turbine systems or for superheating steam, vaporizing chemical substances &c. comprising a combustion chamber formed of a number of co-axial truncated conical members spaced to provide annular passages communicating with a surrounding jacket, secondary air is supplied to the combustion chamber through the annular passages adjacent the burner end while a substance other 'than air is delivered into the gas stream through one or more of the passages near the cutlet end. The apparatus described is substantially the same as that shown in Figs. 7 to 10 of the drawings accompanying Specification 597,151.
GB27075/45A 1943-03-13 1943-09-06 Improvements in method and apparatus for the combustion of fuel Expired GB597205A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US597205XA 1943-03-13 1943-03-13

Publications (1)

Publication Number Publication Date
GB597205A true GB597205A (en) 1948-01-20

Family

ID=22024812

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27075/45A Expired GB597205A (en) 1943-03-13 1943-09-06 Improvements in method and apparatus for the combustion of fuel

Country Status (1)

Country Link
GB (1) GB597205A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2669090A (en) * 1951-01-13 1954-02-16 Lanova Corp Combustion chamber
US2968918A (en) * 1949-08-22 1961-01-24 California Inst Res Found Rocket motor shell construction
DE1155877B (en) * 1958-04-24 1963-10-17 Willi Keil Oil burner
US3572031A (en) * 1969-07-11 1971-03-23 United Aircraft Corp Variable area cooling passages for gas turbine burners

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968918A (en) * 1949-08-22 1961-01-24 California Inst Res Found Rocket motor shell construction
US2669090A (en) * 1951-01-13 1954-02-16 Lanova Corp Combustion chamber
DE1155877B (en) * 1958-04-24 1963-10-17 Willi Keil Oil burner
US3572031A (en) * 1969-07-11 1971-03-23 United Aircraft Corp Variable area cooling passages for gas turbine burners

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