Beschrieben wird eine Verstellleitschaufel (50) für einen Verdichter (16), insbesondere Hochdruckverdichter (29), einer Gasturbine (10), insbesondere Fluggasturbine, mit einem radial äußeren Lagerabschnitt (56), einem radial inneren Lagerabschnitt (52),...

Disclosed is a thrust deflection device for deflecting a thrust jet with a flap arrangement having a plurality of deflection flaps, each of which is pivotable about its vertical axis, wherein the flap arrangement is arranged between parallel guide surfaces...

The invention relates to a mixing device and a turbofan engine with such a mixing device (30) for mixing a first gas stream (50) with a second gas stream (40) in a turbofan engine (20), with an actuating device (95) and a wall (60) which defines a radially...

The turbomachine has a housing structure surrounding an annular flow channel. Rotating vanes are rotatably accommodated in the structure. Guide vanes are stationarily accommodated in the structure. The vanes are arranged in the channel. The guide vanes for...

The gas turbine jet engine has a housing structure (22) radially surrounding the main flow channel (20), in which a housing gas flow flows in a same direction as a main flow in the main flow channel. The housing structure has an adjustable flow conducting ...

The engine (1) has a turbomachine (2) i.e. gas turbine, comprising a compressor (20), a combustion chamber (23) and a turbine (26). A free piston compressor (3) is coupled with the turbomachine and comprises a compressor piston (30) and a cylinder chamber ...

The method involves applying and manufacturing an abradable coating (20) on a component of a turbomachine by a kinetic cold gas compacting process. The component is a static or rotating component (16) of the turbomachine. An adhesive layer or a thermal ins...

The aircraft engine has one-or multi-stage compressor arrangement (V), downstream combustion chamber (BK), one or multi-stage turbine assembly (HT,NT), compressor heat exchanger arrangement (WV), turbine heat exchanger arrangement (WT) and by-pass unit (BY...

The sealing arrangement (1) has several seals (4) arranged in peripheral direction so as to form closed seal ring. Each seal has honeycomb element (8) with several honeycombs separated from each other by walls, and base (10) having front side connected to ...