GB663639A - Improvements in gas heaters and other heat exchangers - Google Patents

Improvements in gas heaters and other heat exchangers

Info

Publication number
GB663639A
GB663639A GB2502648A GB2502648A GB663639A GB 663639 A GB663639 A GB 663639A GB 2502648 A GB2502648 A GB 2502648A GB 2502648 A GB2502648 A GB 2502648A GB 663639 A GB663639 A GB 663639A
Authority
GB
United Kingdom
Prior art keywords
passages
air
another
annular
shell
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
GB2502648A
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.)
Peabody Engineering Corp
Original Assignee
Peabody Engineering Corp
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 Peabody Engineering Corp filed Critical Peabody Engineering Corp
Priority to GB2502648A priority Critical patent/GB663639A/en
Publication of GB663639A publication Critical patent/GB663639A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow

Landscapes

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

Abstract

663,639. Generating combustion products under pressure. PEABODY, Ltd. (Peabody Engineering Corporation). Sept. 24, 1948, No. 25026/48. Class 51 (i). [Also in Groups XI and XIII] An air or gas heater or other heat exchanger comprises an outer shell 10 and two concentric inner shells 35, 41 separated from the shell and one another by spaces which are divided by corrugated members 37, 43 into longitudinal passages, fluid flowing through the two sets of passages being heated by heat derived from the interior of the innermost shell 41. In the form shown, the two sets of passages communicate witn one another at one end, and the innermost shell is made in sections of successively increasing diameter. Air flows from an inlet 65 through the outer set of passages 36, and then partly through an annular air register 16 for combustion with fuel from a burner 31, and partly through the inner set of passages 40. Some of the air in these passages enters the combustion chamber through the annular gaps 44, which may have associated baffles 45, 46. The proportion of air passing to the burner and to the second set of passages is controlled by an annular damper 53 carried by screw-threaded rods 54. Louvres in the air register are adjustable simultaneously by a handle 20. In a modification, the two annular sets of passages between the shells do not communicate with one another. The air to be heated is introduced at the burner end and flows through the inner set of passages, and another gas or liquid flows through the outer set of passages. Liquid, gaseous or pulverulent fuel may be used.
GB2502648A 1948-09-24 1948-09-24 Improvements in gas heaters and other heat exchangers Expired GB663639A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2502648A GB663639A (en) 1948-09-24 1948-09-24 Improvements in gas heaters and other heat exchangers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2502648A GB663639A (en) 1948-09-24 1948-09-24 Improvements in gas heaters and other heat exchangers

Publications (1)

Publication Number Publication Date
GB663639A true GB663639A (en) 1951-12-27

Family

ID=10221017

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2502648A Expired GB663639A (en) 1948-09-24 1948-09-24 Improvements in gas heaters and other heat exchangers

Country Status (1)

Country Link
GB (1) GB663639A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1154224B (en) * 1956-08-30 1963-09-12 Kohlenscheidungs Ges Mit Besch Gas burners, especially for radiant steam generators
EP0031174B1 (en) * 1979-12-20 1984-08-22 BBC Aktiengesellschaft Brown, Boveri & Cie. Cooled gasturbine blade
FR2572463A1 (en) * 1984-10-30 1986-05-02 Snecma INJECTION SYSTEM WITH VARIABLE GEOMETRY.
FR2585770A1 (en) * 1985-08-02 1987-02-06 Snecma EXPANDED BOWL INJECTION DEVICE FOR TURBOMACHINE COMBUSTION CHAMBER
US4754600A (en) * 1986-03-20 1988-07-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Axial-centripetal swirler injection apparatus
WO1999061842A1 (en) * 1998-05-27 1999-12-02 Solar Turbines Incorporated Combustion air control system for a gas turbine engine
US6332313B1 (en) 1999-05-22 2001-12-25 Rolls-Royce Plc Combustion chamber with separate, valved air mixing passages for separate combustion zones

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1154224B (en) * 1956-08-30 1963-09-12 Kohlenscheidungs Ges Mit Besch Gas burners, especially for radiant steam generators
EP0031174B1 (en) * 1979-12-20 1984-08-22 BBC Aktiengesellschaft Brown, Boveri & Cie. Cooled gasturbine blade
FR2572463A1 (en) * 1984-10-30 1986-05-02 Snecma INJECTION SYSTEM WITH VARIABLE GEOMETRY.
EP0182687A1 (en) * 1984-10-30 1986-05-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Injection system with a variable geometry
US4766722A (en) * 1985-08-02 1988-08-30 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Enlarged bowl member for a turbojet engine combustion chamber
FR2585770A1 (en) * 1985-08-02 1987-02-06 Snecma EXPANDED BOWL INJECTION DEVICE FOR TURBOMACHINE COMBUSTION CHAMBER
EP0214003A1 (en) * 1985-08-02 1987-03-11 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Fuel injection nozzle with an enlarged screen for the combustion chamber of a gas turbine
US4754600A (en) * 1986-03-20 1988-07-05 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) Axial-centripetal swirler injection apparatus
WO1999061842A1 (en) * 1998-05-27 1999-12-02 Solar Turbines Incorporated Combustion air control system for a gas turbine engine
US6082093A (en) * 1998-05-27 2000-07-04 Solar Turbines Inc. Combustion air control system for a gas turbine engine
GB2352505A (en) * 1998-05-27 2001-01-31 Solar Turbines Inc Combustion air control system for a gas turbine engine
GB2352505B (en) * 1998-05-27 2002-07-03 Solar Turbines Inc Combustion air control system for a gas turbine engine
US6332313B1 (en) 1999-05-22 2001-12-25 Rolls-Royce Plc Combustion chamber with separate, valved air mixing passages for separate combustion zones

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