GB715387A - Improvements in or relating to combustion chambers for gas turbines or other prime movers - Google Patents

Improvements in or relating to combustion chambers for gas turbines or other prime movers

Info

Publication number
GB715387A
GB715387A GB1387951A GB1387951A GB715387A GB 715387 A GB715387 A GB 715387A GB 1387951 A GB1387951 A GB 1387951A GB 1387951 A GB1387951 A GB 1387951A GB 715387 A GB715387 A GB 715387A
Authority
GB
United Kingdom
Prior art keywords
disposed
partition
passage
air inlet
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
GB1387951A
Inventor
Robert Francis Darling
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.)
Parsons and Marine Engineering Turbine Research and Development Association
Original Assignee
Parsons and Marine Engineering Turbine Research and Development Association
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
Priority to NL84788D priority Critical patent/NL84788C/xx
Application filed by Parsons and Marine Engineering Turbine Research and Development Association filed Critical Parsons and Marine Engineering Turbine Research and Development Association
Priority to GB1387951A priority patent/GB715387A/en
Priority to US287211A priority patent/US2777291A/en
Priority to CH302683D priority patent/CH302683A/en
Publication of GB715387A publication Critical patent/GB715387A/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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers

Abstract

715,387. Generating combustion products under pressure. PARSONS & MARINE ENGINEERING TURBINE RESEARCH & DEVELOPMENT ASSOCIATIION. April 9, 1952 [June 12, 1951], No. 13879/51. Class 51 (1) Combustion apparatus for a gas turbine or other prime mover comprises an outer cylindrical member a and an inner partition member extending lengthwise therein, aligned openings being formed in the two members in which flame tubes e are disposed, a cover c and a fuel sprayer k being associated with the end of each flame tube. In Figs. 1. and 4, the outer cylindrical member a is lined with refractory material b, and the partition member p, which is lined with refractory material q, extends obliquely therein forming two D-section passages g, h, the passage q being in communication with the air inlet i and the passage h with the combustion gas outlet j. A valve or shutter n is disposed in the partition p to allow air to pass directly to the passage or mixing chamber h. The flame tubes may be connected by pipes o and that nearest the air inlet may be provided with an igniter. In the embodiment shown in Fig. 6, the partition member is constituted by a cylindrical duct p concentric with the outer member a. Flame tubes e are horizontally disposed on both sides of the apparatus. The air inlet is indicated at i and the gas outlet at j, , a valve or shutter n being disposed at the end of the cylindrical partition to allow some air to pass straight into the mixing chamber.
GB1387951A 1951-06-12 1952-04-09 Improvements in or relating to combustion chambers for gas turbines or other prime movers Expired GB715387A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
NL84788D NL84788C (en) 1951-06-12
GB1387951A GB715387A (en) 1952-04-09 1952-04-09 Improvements in or relating to combustion chambers for gas turbines or other prime movers
US287211A US2777291A (en) 1951-06-12 1952-05-10 Combustion chamber with removable flame tubes
CH302683D CH302683A (en) 1951-06-12 1952-05-23 Incinerator.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1387951A GB715387A (en) 1952-04-09 1952-04-09 Improvements in or relating to combustion chambers for gas turbines or other prime movers

Publications (1)

Publication Number Publication Date
GB715387A true GB715387A (en) 1954-09-15

Family

ID=32321111

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1387951A Expired GB715387A (en) 1951-06-12 1952-04-09 Improvements in or relating to combustion chambers for gas turbines or other prime movers

Country Status (1)

Country Link
GB (1) GB715387A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2410737A1 (en) * 1977-12-01 1979-06-29 United Technologies Corp BURNER FOR GAS TURBINE
EP0109523A1 (en) * 1982-10-19 1984-05-30 Kraftwerk Union Aktiengesellschaft Gas turbine combustion chamber
EP4056827A4 (en) * 2019-11-08 2023-11-22 Toshiba Energy Systems & Solutions Corporation Gas turbine combustor structure

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2410737A1 (en) * 1977-12-01 1979-06-29 United Technologies Corp BURNER FOR GAS TURBINE
EP0109523A1 (en) * 1982-10-19 1984-05-30 Kraftwerk Union Aktiengesellschaft Gas turbine combustion chamber
EP4056827A4 (en) * 2019-11-08 2023-11-22 Toshiba Energy Systems & Solutions Corporation Gas turbine combustor structure
US11892169B2 (en) 2019-11-08 2024-02-06 Toshiba Energy Systems & Solutions Corporation Gas turbine combustor structure

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