Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
162 words
A gas turbine construction having an air compressor, a heat exchanger connected downstream of the air compressor, a combustion chamber, and a turbine which can be driven by hot combustion gases and from which the combustion gases are fed to the heat exchanger for heating compressed supply air coming from the air compressor, wherein the heat exchanger and the combustion chamber are integrated in a common unit, and wherein fuel can be added to the supply air before entry in the unit, which fuel can be ignited catalytically in the form of an air/fuel mixture inside the unit, in which a catalyst is provided; the unit comprising of heat exchanger and combustion chamber provides at least one duct which feeds the air/fuel mixture to the turbine and is thermally coupled to at least one exhaust-gas return duct carrying off the combustion gases; and wherein the duct feeding the air/fuel mixture is provided, at least partly, with a catalyst material on the inside.
Claim 2
Dependent Claim
162 words
A gas turbine construction having an air compressor, a heat exchanger connected downstream of the air compressor, a combustion chamber, and a turbine which can be driven by hot combustion gases and from which the combustion gases are fed to the heat exchanger for heating compressed supply air coming from the air compressor, wherein the heat exchanger and the combustion chamber are integrated in a common unit, and wherein fuel can be added to the supply air before entry in the unit, which fuel can be ignited catalytically in the form of an air/fuel mixture inside the unit, in which a catalyst is provided; the unit comprising of heat exchanger and combustion chamber provides at least one duct which feeds the air/fuel mixture to the turbine and is thermally coupled to at least one exhaust-gas return duct carrying off the combustion gases; and wherein the duct feeding the air/fuel mixture is provided, at least partly, with a catalyst material on the inside.
Claim 3
Dependent Claim
16 words
The gas-turbine construction as claimed in claim 1 , wherein the catalyst material (K) is platinum.
Claim 4
Dependent Claim
26 words
The gas-turbine construction as claimed in one of claim 1 , wherein the fuel can be admixed with the supply air upstream of the air compressor.
Claim 5
Dependent Claim
38 words
The gas-turbine construction as claimed in one of claim 1 , wherein the fuel can be admixed with the compressed supply air by means of an injection nozzle downstream of the air compressor and upstream of the unit.
Claim 6
Dependent Claim
40 words
The gas-turbine construction as claimed in one of claim 1 , wherein the duct feeding the air/fuel mixture to the turbine and the exhaust-gas return duct carrying off the combustion gases are arranged in layers like a plate-type heat exchanger.
Claim 7
Dependent Claim
25 words
The gas-turbine construction as claimed in claim 5 , wherein a multiplicity of repetitive layers consisting of feeding duct and exhaust-gas return duct are provided.
Claim 8
Dependent Claim
50 words
The gas-turbine construction as claimed in one of claim 1 , wherein the feeding duct consists of a heat-exchanger wall enclosing the duct and having a catalyst coating surrounding the heat-exchanger wall on the inside, and the exhaust-gas return duct is enclosed by heat-exchanger walls of two adjacent feeding ducts.
Claim 9
Dependent Claim
53 words
The gas-turbine construction as claimed in one of claim 1 , wherein the unit is of elongated design, having an inlet side for the air/fuel mixture and an outlet side facing turbines, the catalyst being provided in the feeding duct at least in the region of the outlet side, which faces the turbines.
Claim 10
Dependent Claim
54 words
A method of operating the gas-turbine construction as claimed in one of claim 1 , wherein the waste heat of the combustion gases is utilized in order to reach the ignition temperature of the air/fuel mixture directed into the unit, and this waste heat heats the catalyst to the ignition temperature via thermal coupling.
Claim 11
Dependent Claim
75 words
The method as claimed in claim 9 , wherein, after the ignition temperature, which, for instance, is about 500° C., has been reached, a heat transfer takes place from the ignited air/fuel mixture inside the feeding duct to the combustion gases flowing around the duct, as a result of which the catalyst is cooled in the duct region in which the air/fuel mixture is ignited, and the preheating output of the combustion gases is increased.
Claim 12
Dependent Claim
29 words
The method as claimed in claim 9 , wherein the spatial ignition region inside the feeding duct is established by selection of the mixing ratio of the air/fuel mixture.