Mtu Motoren-und Turbinen-union Munchen Gmbh

Mtu Motoren-und Turbinen-union Muenchen, Gmbh

Mtu Motoren-und Turbinen-union

Mtu Munuch, Gmbh

Franz Joos

Nikolaos Zarzalis

Burkhard Simon

Martin Rohlffs

A burner for gas turbine engines is provided in which a ring-shaped swirling device is coaxially assigned to a fuel nozzle. The swirling device forms tangential ducts for an adjustable feeding of combustion air between profiles arranged along the circumference. In this case, the profiles are to be formed by corresponding sections of components which are arranged to be axially movable relative to one another. One respective section of a profile is to be a hollow body in which the corresponding other section engages in a movable manner. With the burner, a combustion is made possible that is low in pollutants while the swirling efficiency and the rotational swirl development are optimal.

Burner for gas turbine engines with axially adjustable swirler

A burner for gas turbine engines is provided in which a ring-shaped swirling device is coaxially assigned to a fuel nozzle. The swirling device forms tangential ducts for an adjustable feeding of combustion air between profiled surfaces arranged along the circumference. Two components, which are axially adjustable relative to one another, are to form, on mutually opposite faces, the ducts between profiles and recesses which are arranged offset relative to one another along the circumference, in such a manner that, when at least one component is adjusted, the profiles can be moved into the recesses for a reduction of the duct cross-sections or can be moved out of the recesses for an enlargement of the duct cross-sections.

Burner for gas turbine engines

A fuel injection device having three concentric streams of air for the atomization of fuel sprayed onto a sleeve by an injector facing into the sleeve. The inner and outer streams of air are imparted with swirl in opposite direction, while the central stream of air is free of swirl. The two inner streams of air atomize the fuel as a result of shear forces, while the outer stream of air forms a stable recirculation region in a combustion chamber into which the fuel injector device extends.

Fuel injection apparatus and associated method

A reverse flow combustion chamber includes an annular chamber enclosed between flame tube wall sections to which cooling air is so supplied from an outer annular channel acted upon with secondary air opposite the main flow direction in the flame tube in such a manner that the cooling air that it is blown out in the opposite flow direction film-like against an adjoining flame tube wall. For the purpose of a cooling film with extremely great travel length which is homogeneous over the entire circumference, the annular chamber is to be constructed flat elliptically in the combustion chamber longitudinal direction in such a manner that together with air catching or collecting bores which terminate radially and essentially tangentially in the downstream end of the annular chamber--in relation to the secondary flow--, a part of the supplied cooling air produces an independent recirculation vortex following the elliptical annular chamber contour which is provided for the equalization of the main cooling air flow supplied by way of the air collecting bores and deflected into the flame tube through about 90.degree. in the direction of the main flow.

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Munich, Germany

Franz Joos