1
Keller Jakob Dr, Sattelmayer Thomas Dr, Styner Daniel: Process for combustion of liquid fuel in a burner.. Bbc Brown Boveri & Cie, June 28, 1989: EP0321809-A1 (176 worldwide citation)

In the premix combustion of liquid fuel in a burner without premixing section, there is formed in the interior (14) of the burner a conical liquid fuel column (5) which widens in the direction of flow and which is surrounded by a rotating combustion air flow (15) which flows tangentially into the bu ...


2
Ruck Thomas, Sattelmayer Thomas Dr, Steinbach Christian Dr: Burner. Abb Management, April 3, 1996: EP0704657-A2 (46 worldwide citation)

The burner comprises a swirl generator for the combustion air-stream and fuel injection devices. Inside a first section (200) of the mixing passage (220) downstream of the swirl-generator (100) are transfer passages (201) delivering the current (40) to the downstream portion (20) of the mixing passa ...


3
Sattelmayer Thomas Dr, Valk Martin Dr: Burner for a heat generator. Abb Research, September 24, 1997: EP0797051-A2 (18 worldwide citation)

The burner incorporates a swirl-inducer for the combustion air, into which fuel is sprayed by nozzles. There is a mixing passage upstream of the combustion chamber which is connected to the inducer. There are a large number of mixing units (300) situated concentrically to the passage at the stepped ...


4
Sattelmayer Thomas Dr: Combustion chamber. Abb Research, January 31, 1996: EP0694740-A2 (15 worldwide citation)

The combustion chamber has two stages (1,2) in series in the gas flow direction. On the head side of the first stage, there is a mixer (100) which forms a fuel-air mixture. Downstream of this mixer there is a catalyser (3), in which the mixture is fully burnt. The mixture is such that an adiabatic f ...


5
Keller Jakob Dr, Sattelmayer Thomas Dr: Gas turbine combustion chamber.. Asea Brown Boveri, September 19, 1990: EP0387532-A1 (12 worldwide citation)

In an annular combustion chamber (A), there is arranged on the inflow side in circumferential direction a row of pre-mix burners (B, C). The large pre-mix burners (B), which are the main burners of the annular combustion chamber (A), and the small pre-mix burners (C), which are the pilot burners of ...


6
Althaus Rolf Dr, Chyou Yau Pin Dr, Frutschi Hans Ulrich Dr, Genet Christian, Kamber Peter, Lindvall Anders, Rufli Peter, Sattelmayer Thomas Dr, Senior Peter Dr: Method for providing partial load operation in a gas turbine plant.. Abb Management, April 5, 1995: EP0646705-A1 (12 worldwide citation)

The invention proposes a method for providing partial load operation in a turbine plant. This gas turbine plant essentially comprises a compressor unit (1), an HP combustion chamber (4) arranged downstream of the compressor unit (1), an HP turbine (5) arranged downstream of this HP combustion chambe ...


7
Doebbeling Klaus Dr, Eroglu Adnan, Sattelmayer Thomas Dr: Premix burner.. Abb Management, October 12, 1994: EP0619457-A1 (11 worldwide citation)

A premix burner in accordance with the double-cone principle consists essentially of two hollow conical partial bodies (111, 112) fitted into each other in the flow direction, the respective centre axes (113, 114) of which are offset relative to one another. The adjacent walls of the two partial bod ...


8
Sattelmayer Thomas Dr: Burner for operating a combustion chamber with a liquid and/or gaseous fuel. Abb Research, July 1, 1998: EP0851172-A2 (10 worldwide citation)

The combustion air (7) flows through tangential air inlet ducts (5,6) into a pre-mixing section formed by the burner. A critical spin-flow formed at the burner's outlet and induces a backflow zone to stabilise the flame-front. The burner along the flow direction has at least one zone(27) in which ex ...


9
Sattelmayer Thomas Dr, Senior Peter: Burner for an internal combustion engine, a combustion chamber of a gas turbine plant or a furnace.. Asea Brown Boveri, December 16, 1992: EP0518072-A1 (6 worldwide citation)

For operating an internal combustion engine, a combustion chamber of a gas-turbo assembly or a furnace installation, a burner is used which is characterised by an internal premixing zone. The burner itself consists of at least two hollow part-cone members (1, 2) which are positioned one on another i ...


10
Haumann Juergen Dr, Knoepfel Hans Peter, Sattelmayer Thomas Dr: Method of operating a vortex stabilised burner and burner applying the method. Abb Research, September 23, 1998: EP0866268-A1 (6 worldwide citation)

To operate a twist-stabilised burner using a gas or liquid fuel, and especially as a premix burner, lighting-up air (38) is injected during the lighting-up process, at the downstream end of the twist generator (37) from the edge to the centre. The injected air has at least one radial speed component ...