CompressorThe compressor has a stator vane assembly including an inner ring (1) and a seal carrier (2), where the seal carrier comprises two opposite seal carrier end faces (2-10, 2-11) and the inner ring compr…DRIVE·Sep 11·1 min readFollowF01D11/001MTU AERO ENGINES GMBH [DE]
Ventilation device and method for producing a ventilation device, rotor and fluid flow engineThe device (1) has air conduit tubes (14) for guiding air from an outer annular space radially toward a rotor shaft, and a support ring (12) for arranging the air conduit tubes in a radially closed in…DRIVE·Jul 24·1 min readFollowF01D5/087MTU AERO ENGINES GMBH [DE]
Flow engine seal assemblyThe arrangement has shells (1-3) connected with one another in a circumferential direction (U) and arranged adjacent to each other in an axial direction (A). The shells comprise V or U-shaped cross se…DRIVE·Jul 24·1 min readFollowF01D11/08MTU AERO ENGINES GMBH [DE]
Segmented componentThe component has component segments (12a, 12b) arranged relative to one another such that a gap is defined between the segments. The segments are sealed opposite to each other by a sealing device (16…DRIVE·Apr 3·1 min readFollowF01D11/005MTU AERO ENGINES GMBH [DE]
System for injecting a fluid, compressor and turbomachine comprising the sameThe system (6) has multiple nozzles (8), which are arranged in a side wall (2) that limits stream (4) and area oriented diagonally in flow direction (x). The nozzles have a rectangular flat cross-sect…DRIVE·Jan 16·1 min readFollowF02C7/22MTU AERO ENGINES GMBH [DE]
Blade with cooled rootThe blades (2, 4) have a blade root (8), a blade neck (10) and a platform (14) arranged between the neck and a blade pan (12). The platform has a front projection (16) and a rear projection (18), wher…DRIVE·Nov 7·1 min readFollowF01D5/081MTU AERO ENGINES GMBH [DE]
Fan for an aircraft engineThe fan (11) for especially an aviation gas turbine engine has a supplementary rotor (18) positioned upstream of the fan rotor (13) with blades (19) which extend radially outwards from a hub and finis…DRIVE·Mar 8·1 min readFollowF02K3/06MTU AERO ENGINES GMBH [DE]
Fluid structure for a turbocompressorThe flow structure for the compressor of especially a gas turbine has at least one toroidal chamber (18) installed concentrically to an axis (17) of the compressor in the region of the free blade ends…DRIVE·Jan 11·1 min readFollowF01D11/08MTU AERO ENGINES GMBH [DE]
Gas turbine with control box mounting deviceThe gas turbine, especially an aviation jet engine (10), has at least one ancillary unit (14) fastened to it and receiving signals from at least one sub-unit of the gas turbine. The ancillary unit has…DRIVE·Dec 15·1 min readFollowF01D17/02MTU AERO ENGINES GMBH [DE]
Method for controlling fuel supplyThe method involves feeding the fuel with a pump (2), dispensing it into the engine by a fuel dosing valve (5) and regulating the pressure to which the fuel dosing valve is subjected using a recircula…DRIVE·Oct 17·1 min readFollowF02C9/26MTU AERO ENGINES GMBH [DE]
