Patent ID: 7997896

Claim:
A premix burner with staged liquid fuel supply, comprising: at least two partial cone shells which on the radial side form the boundary of and define a swirl chamber which axialwards conically widens, which partial cone shells are arranged in a partially overlapping manner, the center axes of the partial cone shells of which extend with offset effect in relation to each another, and the mutually overlapping partial cone shell sections of which enclose in each case an air inlet slot which extends tangentially to the swirl chamber; a burner lance which projects axialwards into the swirl chamber, which lance provides means for feed of liquid fuel into the swirl chamber, and also with further means for feed of liquid fuel which are formed and arranged in the region of the air inlet slots in such a way that the liquid fuel delivery, which is conditioned by the further means, takes place in the form of a fuel spray which propagates perpendicularly to the tangential longitudinal extent of the air inlet slot, and also a fuel spray which propagates perpendicularly to an air flow which is directed through the air inlet slot; and a mixing pipe is axialwards directly connected downstream to the swirl chamber and upstream to a combustion chamber wherein no combustion occurs within the mixing pipe, and wherein the further means for liquid fuel feed extend axialwards at least into sections of the mixing pipe in such a way that a liquid fuel feed which is directed radially inwards into the mixing pipe is executable.