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Mtu Aero Engines Gmbh patents

Recent patent applications related to Mtu Aero Engines Gmbh. Mtu Aero Engines Gmbh is listed as an Agent/Assignee. Note: Mtu Aero Engines Gmbh may have other listings under different names/spellings. We're not affiliated with Mtu Aero Engines Gmbh, we're just tracking patents.

ARCHIVE: New 2017 2016 2015 2014 2013 2012 2011 2010 2009 | Company Directory "M" | Mtu Aero Engines Gmbh-related inventors

Date Mtu Aero Engines Gmbh patents (updated weekly) - BOOKMARK this page
06/23/16Low noise turbine for geared gas turbine engine
04/28/16Destruction-free and contactless inspection method and inspection surfaces of components with ultrasound waves
03/17/16Process for producing holes
06/05/14Gas turbine and guide blade for a housing of a gas turbine
05/29/14Method and device for machining robot-guided components
05/29/14Turbomachine rotor disk
03/13/14Blade arrangement for a turbo engine
12/26/13Process for producing a run-in coating
12/05/13Aircraft engine with turbine heat exchanger bypass
10/31/13Damping means for damping a blade movement of a turbomachine
10/24/13Rotor blade arrangement for a turbo machine
10/17/13Nickel-based solder alloy
10/10/13Sealing system for a turbomachine
10/10/13Sealing system for a turbomachine
10/03/13Aluminide or chromide coatings of cavities
09/26/13Securing device for axially securing a blade root of a turbomachine blade
09/19/13Blade ring segment having an annular space delimiting surface having a wavy height profile and a manufacturing same
09/12/13Housing and turbomachine
08/15/13Blade group arrangement as well as turbomachine
08/08/13Blade cascade and turbomachine
08/01/13Electrode and installation for electrochemical machining and method therefor
07/25/13Method for nondestructive testing of workpiece surfaces
07/25/13Turbomachine seal arrangement
07/25/13Seal assembly, method and turbomachine
07/25/13Blade rim segment for a turbomachine and manufacture
07/25/13Rotor for a turbomachine
07/25/13Method for producing a locally limited diffusion coat and reactor for it
07/18/13System for injecting a fluid, compressor and turbomachine
07/18/13Housing-side structure of a turbomachine
07/11/13Cleaning of a turbo-machine stage
07/04/13Apparatus and processing a sealing element located within the housing of a gas turbine
07/04/13Method for repair of a component of a turbomachine and a component repaired according to this method
06/27/13Mounting device and mounting a component on a component carrier using an adhesive
06/20/13Turbomachine and turbomachine stage
06/20/13Turbomachine and turbomachine stage
06/13/13Rotating blade having a rib arrangement with a coating
06/06/13Method and device for removing a layer from a surface of a body
06/06/13Process and applying layers of material to a workpiece made of tial
05/23/13Coating plastic components by means of kinetic cold gas spraying
04/11/13Blade row for a turbomachine
03/14/13Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow losses
03/07/13Method and device for producing a component
03/07/13Method and electrode for electrochemically processing a workpiece
02/28/13Transition channel of a turbine unit
02/07/13Device and preserving fluid systems and an engine
02/07/13Method for processing a surface of a component
01/31/13Guide blade of a turbomachine
12/13/12Blade comprising pre-wired sections
11/29/12Housing system for an axial turbomachine
11/15/12Measurement for measuring layer thicknesses as well as production method and coating system
11/15/12Combined heating for soldering an armor cladding onto a tip by means of induction and laser
11/08/12Method for producing an integrally bladed rotor using arcuate friction welding, device for carrying out said method, and rotor produced by means of said method
11/08/12Inner ring for forming a guide blade ring, and guide blade ring and turbomachine
11/08/12Sealing device, integrally bladed rotor basic body, and turbomachine
11/08/12Blade, integrally bladed rotor base body and turbomachine
10/25/12Method for producing a component with at least one element arranged in the component
10/25/12Method for fusion welding a monocrystalline workpiece to a polycrystalline workpiece and rotor
Patent Packs
10/04/12Method for producing an abradable coating on a turbomachine
09/13/12Gas turbine blade for a turbomachine
09/06/12Coupling element for mechanically coupling blades and a rotor
09/06/12Method and device for producing an integrally bladed rotor and rotor produced by means of the method
09/06/12Method and device for coating components
08/30/12Method and device for producing a component of a turbomachine
08/30/12Method and device for producing a component
08/23/12Device for fastening and detaching a component, and method therefor
08/23/12Method and device for producing a component of a turbomachine
08/09/12Ring element and turbomachine having such a ring element
08/09/12Blade channel having an end wall contour and a turbomachine
08/09/12Method for producing a rotor or stator blade and such a blade
07/05/12Thin-walled structural component, and the production thereof
06/21/12Aircraft engine blading
06/21/12Method for the local heat treatment of gas turbine blades
Patent Packs
06/14/12Pressure-measuring probe
06/14/12Method for replacing a blade of a rotor having integrated blades and such a rotor
06/07/12Blade segment and fluid flow machine
06/07/12Anti-wear coating and component comprising an anti-wear coating
05/24/12Repair of turbine components and solder alloy therefor
05/24/12Method for coating a turbine blade
05/17/12Rotor and manufacturing a rotor for a turbo machine
05/17/12Joining element and the production of such a joining element as well as an integrally bladed rotor
05/17/12Blade tip coating that can be rubbed off
05/17/12Rotor for a turbo machine
05/17/12Rotor for a turbo machine
05/17/12Rotor for a turbo machine
05/03/12Method for reducing vibration amplitudes
05/03/12Device and electrochemically removing a surface of a component
05/03/12Shroud segment to be arranged on a blade
04/19/12Method for manufacturing an integrally bladed rotor
04/12/12Layer system for rotor/stator seal of a turbomachine and producing this type of layer system
04/05/12Method and device for producing a hole in an object
03/15/12Clearance control system, turbomachine and adjusting a running clearance between a rotor and a casing of a turbomachine
03/08/12Method and surface hardening a component, which is made of an intermetallic compound at least in the region of the surface to be hardened
03/08/12Rotor for a turbomachine
02/23/12Flow device comprising a cavity cooling system
02/16/12Compressor having a guide vane assembly with a radially variable outflow
02/09/12Method for producing a plating of a vane tip and correspondingly produced vanes and gas turbines
02/02/12Dual blisks in the high-pressure compressor
01/19/12Device for fixing workpieces on a workpiece carrier and machining workpieces
01/05/12Device and fixing a component in position on a component carrier
01/05/12Turbine shroud
Social Network Patent Pack
12/29/11Tandem blade design
12/15/11Component for a gas turbine and a the production of the component
12/08/11Anti-erosion coating system for gas turbine components
12/01/11Method for producing a blade plating on a blade for a turbomachine
12/01/11Sealing apparatus at the blade shaft of a rotor stage of an axial turbomachine
11/03/11Method for mounting an integral inner ring of a turbocompressor stator
11/03/11Method and device for inductively heating a component
10/20/11Damping element and damping rotor blade vibrations, a rotor blade, and a rotor
10/20/11Method for repairing a rotor system of a turbomachine, annular element for a rotor system of a turbomachine, and rotor system for a turbomachine
10/20/11Method for the production of an integrally bladed rotor, and rotor
Patent Packs
10/20/11Integrally bladed rotor disk for a turbine
10/13/11Replacement part for a gas turbine blade of a gas turbine, gas turbine blade and repairing a gas turbine blade
10/06/11Capacitor arrangement and producing a capacitor arrangement
10/06/11Energy storage device
09/29/11Method for determing the machining quality of components, particularly for metal cutting by nc machines
09/22/11Assembly mechanism comprising a tension anchor and corresponding a rotor system of an axial turbo engine
09/22/11Turbo engine
09/22/11Method for joining components
09/22/11Brush seal
09/15/11Method for replacing an inner disk element of an integrally bladed disk
09/15/11Mask for kinetic cold gas compacting
09/08/11Method for connecting at least one turbine blade to a turbine disk or a turbine ring
09/08/11Repair method
09/01/11Method and device for detecting cracks in compressor blades
08/18/11Method for producing or repairing integrally bladed gas turbine rotors
08/04/11Device for use in a the production of a protective layer and the production of a protective layer
08/04/11Method for machining a metal component
08/04/11Gas turbine and varying the aerodynamic shape of a gas turbine blade
08/04/11Material for a gas turbine component, producing a gas turbine component and gas turbine component
07/28/11Blade for a turbo device with a vortex-generator
07/21/11Method for the production of a rotor and rotor
07/21/11Apparatus and masking a component zone
07/07/11Axial flow machine having an asymmetrical compressor inlet guide baffle
07/07/11Device and service-life monitoring
06/16/11Material sample for testing biaxial stress conditions
06/16/11Bearing ring and cooling a bearing ring
06/16/11Rotating blade system for a row of rotating blades of a turbomachine
06/16/11Process and device for cold spraying
06/09/11Method and device for compensating for positional and shape deviations
Patent Packs
06/09/11Method and arrangement for detecting a surface of an object
06/02/11Method for joining and joined connection of two components made of a metal material
06/02/11Process for producing a join to single-crystal or directionally solidified material
06/02/11Methods for joining a monocrystalline part to a polycrystalline part by means of an adapter piece made of polycrystalline material
05/05/11Gas turbine compressor
05/05/11Shroud for rotating blades of a turbo machine, and turbo machine
04/14/11Housing for a compressor of a gas turbine, compressor, and producing a housing segment of a compressor housing
03/24/11Covering device and coating components
03/10/11Device and redirecting a leakage current
03/10/11Turbine blade of a gas turbine and coating a turbine blade of a gas turbine
03/10/11High-temperature anti-corrosive layer and the production thereof
03/03/11High-pressure turbine rotor, and the production thereof
02/24/11Erosion protection coating
02/10/11Strut for an intermediate turbine housing, intermediate turbine housing, and producing an intermediate turbine housing
01/27/11Brush seal and mounting a brush seal
01/27/11Device and the partial coating of components
01/27/11Method for manufacturing a run-in coating
01/20/11Gas dynamic cold spraying of oxide-containing protective layers
01/13/11Method for the thermochemical cleaning and/or stripping of turbine components
01/13/11Probe for a capacitive sensor device and gap-measuring system
Social Network Patent Pack
01/13/11Method and device for automatic laser focusing
01/13/11Centrifugal pump having increased operational safety
01/06/11Method for repairing a sealing segment of a gas turbine
01/06/11Method for producing and repairing a part, and part of a gas turbine
12/30/10Brush seal and mounting a brush seal
12/30/10Circulation structure for a turbo compressor
12/23/10Method for producing integrally bladed rotors
12/23/10Seal arrangement
12/23/10Solder coating, coating a component, component, and adhesive tape having a solder coating
12/23/10Compressor of a gas turbine
12/02/10Method for producing a cast part, casting mould and cast part produced therewith
11/18/10Device and remelting metallic surfaces
11/11/10Honeycomb structure
10/28/10Method for removing material from a component, and electrode
10/28/10Method for producing an integrally bladed rotor, and rotor
10/21/10Decoating device for axially symmetric components, particularly from aircraft engines
10/07/10Electric drive, particularly for a fuel metering unit for an airplane engine
09/23/10Wear protection coating
09/16/10Turbo compressor in an axial type of construction
09/09/10Turbomachine blade with a blade tip armor cladding
Social Network Patent Pack
08/12/10Multilayer shielding ring for a flight driving mechanism
08/12/10Method for producing a lightweight turbine blade
08/05/10Closed-loop control for a gas turbine with actively stabilized compressor
08/05/10Damping device, welding system for rotary friction welding and rotary friction welding method
07/29/10Method and device for surface peening of a component in the region of a passage opening
07/22/10Induction coil, for the inductive heating of metal components
07/08/10Sealing device for a cooling agent supply on a rotating spindle and machine tool comprising such a sealing device
07/08/10Adhesive masking tapes and coating and/or repairing components
07/01/10Alternating current switch device and the monitoring or diagnosis of the operability of an alternating current switch device
07/01/10Method for determining the polyester fraction of a multi-component powder during a thermal spraying process, coating or touching up an object by means of a thermal spraying process and thermal spraying device
07/01/10Maintenance planning method
06/24/10Component and joining metal elements
06/10/10Jet engine with active-magnetic bearing
06/10/10Device for the protection of components having a flammable titanium alloy from titanium fire, and the production thereof
06/03/10Method and blasting agent for surface peening
06/03/10Semi-finished product for producing a repaired blade for a gas turbine and repair repairing a blade for a gas turbine
05/27/10Method and device for the surface peening of a partial element of a component of a gas turbine
05/13/10Inlet cone for jet engine
05/13/10Method for the production of an abradable coating
05/06/10Method for stripping a component
05/06/10Method for the soldering repair of a component in a vacuum and an adjusted partial oxygen pressure
04/29/10Method for producing a structural element
04/29/10Gas turbine
04/22/10Method and device for coating components of a gas turbine
04/15/10Apparatus and non-contacting blade oscillation measurement
04/01/10Device and measuring layer thicknesses
03/25/10Method of manufacturing and refinishing integrally bladed rotors
03/25/10Vane ring, and the production thereof
03/18/10Method for repairing and/or replacing individual elements of a gas turbine component
03/11/10Method for the production of an abradable spray coating
Social Network Patent Pack
03/04/10Turbo engine
02/18/10Device and the surface peening of a component of a gas turbine
02/11/10Gas turbine comprising a guide ring and a mixer
02/04/10High-pressure turbine blade and procedure for repair of high-pressure turbine blades
01/21/10Apparatus and drawing off and recirculating a cooling stream
01/21/10Apparatus and the heat treatment of integral rotors of gas turbines
01/21/10Method for producing gear wheels
01/07/10Turbo engine
12/31/09Gas turbine having a peripheral ring segment including a recirculation channel
12/24/09Apparatus and controlling a blade tip clearance for a compressor
12/10/09Gas turbine and operating a gas turbine
12/10/09Cover element for a sonotrode and peening chamber arrangement for the surface peening of components
12/10/09Guide blade segment of a gas turbine and its production
12/10/09Method and device for joining by way of inductive hf pressure welding a rotor blade with a rotor support of a gas turbine with automatic supply of the rotor blade
12/03/09Thermal barrier layer
11/26/09Process for connecting metallic structural elements and components produced thereby
11/12/09Method and hardening a surface of a component
11/05/09Repair method
11/05/09Engine regulation qualifying the components of the engine regulation system
10/29/09Component, in particular, a gas turbine component
10/22/09Ring structure with a metal design having a run-in lining
10/01/09Method and measuring system for characterizing a deviation of an actual dimension of a component from a nominal dimension of the component
09/24/09Chuck-integrated force-measuring system
09/24/09Device and visualizing positions on a surface
09/17/09Method for repairing turbine vanes
09/03/09Method for the pre-treatment of titanium components for the subsequent coating thereof
08/27/09Procedure for the production and application of a protective layer
08/27/09Optimized machining of a contour using a pulsed tool
08/27/09Method for optimized milling close to the final contour

ARCHIVE: New 2017 2016 2015 2014 2013 2012 2011 2010 2009


This listing is an abstract for educational and research purposes is only meant as a recent sample of applications filed, not a comprehensive history. is not affiliated or associated with Mtu Aero Engines Gmbh in any way and there may be associated servicemarks. This data is also published to the public by the USPTO and available for free on their website. Note that there may be alternative spellings for Mtu Aero Engines Gmbh with additional patents listed. Browse our Agent directory for other possible listings. Page by