Slinger combustor and gas turbine engine system having the same
AssigneeHanwha Techwin Co., Ltd.
InventorSoo Youl PARK
Life of this patent
Estimating the term…
Abstract
A slinger combustor includes; a first compressed air line connected to a compressor and configured to supply compressed air; a first fuel line connected to a fuel storage and configured to supply fuel; a rotation shaft configured to rotate and inject the fuel supplied from the first fuel line; a main combustion chamber configured to receive the fuel injected from the rotation shaft and receive the compressed air from the first compressed air line; and a sub-combustion chamber configured to selectively discharge a flame generated in an inner space of the sub-combustion chamber to the main combustion chamber.
Claims7
A slinger combustor comprising:
- a first compressed air line connected to a compressor and configured to supply compressed air;
- a first fuel line connected to a fuel storage and configured to supply fuel;
- a rotation shaft configured to rotate and inject the fuel supplied from the first fuel line;
- a main combustion chamber configured to receive the fuel injected from the rotation shaft and receive the compressed air from the first compressed air line;
- and
- a sub-combustion chamber configured to selectively discharge a flame generated in an inner space of the sub-combustion chamber to the main combustion chamber.
A gas turbine engine system comprising:
- the compressor;
- the fuel storage arranged spaced apart from the compressor;
- and
- a turbine connected to an outlet of the slinger combustor,
- wherein the slinger combustor comprises:
- a first compressed air line connected to a compressor and configured to supply compressed air;
- a first fuel line connected to a fuel storage and configured to supply fuel;
- a rotation shaft configured to rotate and inject the fuel supplied from the first fuel line;
- a main combustion chamber configured to receive the fuel injected from the rotation shaft and receive the compressed air from the first compressed air line;
- and
- a sub-combustion chamber configured to selectively discharge a flame generated in an inner space of the sub-combustion chamber to the main combustion chamber.
Dependencies are inferred from the claim text.