GB857493A - Combustion equipment for gas turbine engines - Google Patents
Combustion equipment for gas turbine enginesInfo
- 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
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
- F23R3/10—Air inlet arrangements for primary air
-
- 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
- F23R3/60—Support 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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4704869A (en) * | 1983-06-08 | 1987-11-10 | Hitachi, Ltd. | Gas turbine combustor |
-
1957
- 1957-12-12 GB GB3871357A patent/GB857493A/en not_active Expired
Cited By (1)
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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