Loading patent…
OwnerHelmuth Gabl, Edmund Lorenz +1inventors
InventorsHelmuth Gabl, Edmund Lorenz, Franz Niederl
Estimating the term…
The subject of the present invention is a combustion turbine (1) for intermittent combustion with at least one combustion chamber (3) having inlet valves (2) and an ignition device (18), the at least one combustion chamber (3) having no shut-off devices on the off-gas side and being thus open on the off-gas side at all times. Downstream of the at least one combustion chamber (3), a turbine (4), which can be impinged with process gas obtained in the combustion chamber (3), is positioned, with a flow-through chamber (5) being positioned between the at least one combustion chamber (3) and the turbine (4) axially behind the at least one combustion chamber (3). The flow-through chamber (5) is separated from the at least one combustion chamber (3) by a guiding plate (6) or a further turbine (7). The subject of the present invention is furthermore a process for operation of a combustion turbine (1) and a drive system for a machine having as its core a combustion turbine (1) according to the invention.
A combustion turbine for discontinuous combustion comprising:
A process for operation of a combustion turbine, where air is fed through inlet valves to at least one combustion chamber, mixed with a fuel and burnt in the combustion chamber, which is not closed on the outlet side, and a turbine is impinged with the process gas obtained in this manner, with the process gas flowing through a flow-through chamber positioned axially downstream of the at least one combustion chamber before impinging the turbine with it, wherein the process gas being fed from the at least one combustion chamber to the flow-through chamber via a guiding plate, which is designed as perforated plate or swirl grid.
A combustion turbine for discontinuous combustion comprising:
Dependencies are inferred from the claim text.