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A combustor is a component or area of a gas turbine, ramjet, or scramjet engine where combustion takes place. It is also known as a burner, burner can, combustion chamber or flame holder. In a gas turbine engine, the combustor or combustion chamber is fed high-pressure air by the compression system. The combustor then heats this air at constant pressure…
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combustion fuel air turbine combustors gas liner engines flow zone emissions engine also cooling used high annular pressure type ramjet
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Combustor | is a | component or area of a gas turbine | 0.90 | text |
| Combustor | is a | fully annular combustor | 0.90 | text |
| Combustor | is a | double annular combustor | 0.90 | text |
| Combustor | is a | primary contributor to a gas turbine's emissions | 0.90 | text |
| fuel flow | instance of | the response to changing conditions | 0.80 | text |
| air speed | instance of | the response to changing conditions | 0.80 | text |
| Combustor | related to Air flow paths | This | 0.60 | section |
| Combustor | related to Air flow paths | It | 0.60 | section |
| Combustor | related to Air flow paths | Intermediate | 0.60 | section |
| Combustor | related to Air flow paths | CO | 0.60 | section |
| Combustor | related to Air flow paths | H2 | 0.60 | section |
| Combustor | related to Annular | The | 0.60 | section |
These clusters group vocabulary that occurs around closely connected concepts in the source material.
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