Thrust vectoring device and aircraft engine comprising the sameDisclosed 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…DRIVE·Dec 17·1 min readFollowB64D33/04MTU AERO ENGINES AG [DE]
Mixing device and turbofan engine with such a mixing deviceThe 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 actuat…DRIVE·Oct 8·2 min readFollowF02K1/386MTU AERO ENGINES AG [DE]
Seal mount made from from titanium aluminide for a flow machineThe 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. Th…DRIVE·Aug 6·1 min readFollowF01D11/001MTU AERO ENGINES AG [DE]
Flow guidance device for cooling the low pressure turbine casing of a gas turbine engineThe 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. …DRIVE·Feb 12·1 min readFollowF01D11/24MTU AERO ENGINES AG [DE]
Thermal engine for free piston compressorThe 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 co…DRIVE·Oct 16·1 min readFollowF02C5/08MTU AERO ENGINES AG [DE]
Method for producing an abradableThe 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)…DRIVE·Oct 9·1 min readFollowF01D11/122MTU AERO ENGINES AG [DE]
Aircraft engineThe 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), turb…DRIVE·Sep 18·1 min readFollowF02C3/04MTU AERO ENGINES AG [DE]
Sealing arrangement, method and fluid flow engineThe 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…DRIVE·Jul 31·1 min readFollowF01D11/001MTU AERO ENGINES AG [DE]
