GB857493A - Combustion equipment for gas turbine engines - Google Patents

Combustion equipment for gas turbine engines

Info

Publication number
GB857493A
GB857493A GB3871357A GB3871357A GB857493A GB 857493 A GB857493 A GB 857493A GB 3871357 A GB3871357 A GB 3871357A GB 3871357 A GB3871357 A GB 3871357A GB 857493 A GB857493 A GB 857493A
Authority
GB
United Kingdom
Prior art keywords
air
flame tube
combustion
mouth
end wall
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
GB3871357A
Inventor
David Charles Broadbent
Sidney Henry Albert Magin
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB3871357A priority Critical patent/GB857493A/en
Publication of GB857493A publication Critical patent/GB857493A/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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

Abstract

857,493. Generating combustion products under pressure. NAPIER & SON Ltd., D. Nov. 25, 1958 [Dec. 12, 1957], No. 38713/57. Class 51 (1). A combustion chamber. and combustion air inlet duct assembly for a gas turbine engine (Figs. 1 and 3) has in the air inlet duct 10, an air distributer device comprising a shroud 12 which surrounds the upstream end wall of a flame tube 22 thus enclosing the primary air inlets of the combustion chamber and has a mouth 14 which faces upstream and opens across the full height of the inlet duct in a zone upstream of the flame tube so as to split the air stream at this zone into a primary air stream flowing through the mouth and secondary air streams on each side of and outside the mouth. The primary air flows into the combustion zone via perforations in the flame tube end wall 22, and in a conical cap 23 attached to the end wall. The secondary air enters the flame tube via apertures in the side walls 19 thereof. The shroud is held in position by longitudinal partition walls 17 diametrically opposite pairs being spaced apart laterally to define between them a " dead " space 18 in which no air flow occurs but through which may pass an igniter plug or fuel pipe.
GB3871357A 1957-12-12 1957-12-12 Combustion equipment for gas turbine engines Expired GB857493A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3871357A GB857493A (en) 1957-12-12 1957-12-12 Combustion equipment for gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3871357A GB857493A (en) 1957-12-12 1957-12-12 Combustion equipment for gas turbine engines

Publications (1)

Publication Number Publication Date
GB857493A true GB857493A (en) 1960-12-29

Family

ID=10405232

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3871357A Expired GB857493A (en) 1957-12-12 1957-12-12 Combustion equipment for gas turbine engines

Country Status (1)

Country Link
GB (1) GB857493A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4704869A (en) * 1983-06-08 1987-11-10 Hitachi, Ltd. Gas turbine combustor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4704869A (en) * 1983-06-08 1987-11-10 Hitachi, Ltd. Gas turbine combustor

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