Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
305 words
Burner system for a gas turbine combustion chamber comprising (a) a pre-mixing burner with an integrated diffusion burner (b) the pre-mixing burner having a pre-mixing chamber into which chamber a main fuel nozzle and a feeding device for combustion air open, and which chamber is bounded at its downstream end by a flame retention baffle (c) the diffusion burner having a pilot fuel nozzle arranged in the central region of the flame retention baffle, (d) fuel control means including a load signal device which generates a signal in accordance with the load of the gas turbine, a fuel control device connected to and operating in response to the load signal device, a main fuel control valve through which fuel flows to the main fuel nozzle, a pilot fuel control valve through which fuel flows to the pilot fuel nozzle, said fuel control device connected to the main fuel control valve and to the pilot fuel control valve and operating in response to the load signal device controls the flow of fuel through the pilot fuel control valve exclusively from start of the gas turbine to a low load or idling speed or a small partial load of the gas turbine and thereafter to an upper range load of the gas turbine through both the main fuel control valve and the pilot fuel control valve, (e) said opening in the pre-mixing chamber for the feeding device for combustion air being the sole entrance for the entire combustion air required for the operation of the diffusion burner, and (f) said fuel control device connected to the main fuel control valve and to the pilot fuel control valve and operating in response to the load signal device above the upper range load of the gas turbine controls the flow of fuel through the main fuel control valve exclusively.
Claim 2
Dependent Claim
305 words
Burner system for a gas turbine combustion chamber comprising (a) a pre-mixing burner with an integrated diffusion burner (b) the pre-mixing burner having a pre-mixing chamber into which chamber a main fuel nozzle and a feeding device for combustion air open, and which chamber is bounded at its downstream end by a flame retention baffle (c) the diffusion burner having a pilot fuel nozzle arranged in the central region of the flame retention baffle, (d) fuel control means including a load signal device which generates a signal in accordance with the load of the gas turbine, a fuel control device connected to and operating in response to the load signal device, a main fuel control valve through which fuel flows to the main fuel nozzle, a pilot fuel control valve through which fuel flows to the pilot fuel nozzle, said fuel control device connected to the main fuel control valve and to the pilot fuel control valve and operating in response to the load signal device controls the flow of fuel through the pilot fuel control valve exclusively from start of the gas turbine to a low load or idling speed or a small partial load of the gas turbine and thereafter to an upper range load of the gas turbine through both the main fuel control valve and the pilot fuel control valve, (e) said opening in the pre-mixing chamber for the feeding device for combustion air being the sole entrance for the entire combustion air required for the operation of the diffusion burner, and (f) said fuel control device connected to the main fuel control valve and to the pilot fuel control valve and operating in response to the load signal device above the upper range load of the gas turbine controls the flow of fuel through the main fuel control valve exclusively.
Claim 3
Dependent Claim
21 words
Burner system according to claim 1, wherein the fuel control device is associated with additional pre-mixing burners with integrated diffusion burners.
Claim 4
Dependent Claim
28 words
Burner system according to claim 1, wherein the pre-mixing burner comprises a first main fuel nozzle for gaseous fuel and a second main fuel nozzle for liquid fuel.
Claim 5
Dependent Claim
28 words
Burner system according to claim 1, wherein the diffusion burner comprises a first pilot fuel nozzle for gaseous fuel and a second pilot fuel nozzle for liquid fuel.
Claim 6
Dependent Claim
39 words
Burner system according to claim 4, wherein the fuel feed lines leading to the first pilot fuel nozzle and to the second pilot fuel nozzle go through the pre-mixing chamber as concentric tubes centrally and in the axial direction.
Claim 7
Dependent Claim
28 words
Burner system according to claim 3, wherein the fuel feed lines leading to the two main fuel nozzles and to the two pilot fuel nozzles are concentric tubes.
Claim 8
Dependent Claim
42 words
Burner system according to claim 1, wherein the swirling device has vanes in the form of hollow blades, and the swirling device acts as the main fuel nozzle by means of several fuel injection holes made in each of the hollow blades.
Claim 9
Dependent Claim
40 words
Burner system according to claim 6, wherein the fuel feed lines, the two main fuel nozzles and the two pilot fuel nozzles are combined as a unit which can be pulled out of the pre-mixing chamber in the axial direction.
Claim 10
Dependent Claim
61 words
Burner system according to claim 1, wherein said fuel control device connected to the main fuel control valve and to the pilot fuel control valve and operating in response to the load signal device reduces the partial amount of the fuel fed to the pilot fuel nozzle with increasing load after the idling speed or a small partial load is reached.
Claim 11
Dependent Claim
70 words
Burner system according to claim 1, wherein the pre-mixing chamber has a venturi-like contour with a section converging at the upstream end and a section diverging at the downstream end, wherein the feeding device for combustion air which leads to the pre-mixing chamber is a swirling device and wherein the fuel feed line leading to the pilot fuel nozzle goes through the pre-mixing chamber centrally and in the axial direction.