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Mtu Aero Engines Ag patents

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

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

Date Mtu Aero Engines Ag patents (updated weekly) - BOOKMARK this page
05/25/17 new patent  Method of making a bladed rotor for a turbomachine
05/25/17 new patent  Vane segment with peripheral securing
05/25/17 new patent  Brush sealing arrangement for a turbomachine, installation securing arrangement and turbomachine
05/25/17 new patent  Method, compressor and turbomachine
05/25/17 new patent  Compressor, method and turbomachine
05/18/17Method and device for the quality assurance of at least one component during the production thereof by a generative production process
05/18/17Rapid manufacturing for the same comprising oppositely-directed protective gas streams parallel to the powder layer
05/18/17Device and influencing the temperatures in inner ring segments of a gas turbine
05/11/17Arrangement for joining elements of turbomachines
05/04/17Turbine rotor for a low pressure turbine of a gas turbine system
05/04/17Ductile compensation layer for brittle components
05/04/17Low noise compressor and turbine for geared turbofan engine
05/04/17Low noise compressor and turbine for geared turbofan engine
05/04/17Turbine blade and aircraft engine comprising same
04/27/17Rotating blade
04/20/17Module for a gas turbine
04/13/17Repair sealing segments
04/13/17Repair of worn component surfaces
04/13/17Containment for a continuous flow machine
04/06/17Sealing fin armoring and the production thereof
03/30/17Apparatus and producing and/or repairing in particular rotationally symmetrical components
03/16/17Gas turbine compressor stage
03/09/17Device and producing a blade airfoil
03/09/17Thermography for quality assurance in an additive manufacturing process
03/09/17Device for bounding a flow channel of a turbomachine
03/09/17Turbomachine blade
03/02/17Rhenium-free nickel base superalloy of low density
02/23/17Optimized nickel-based superalloy
02/16/17Bladed gas turbine rotor
02/09/17Method for machining a workpiece having an irregular edge
02/09/17Guide vane ring element for a turbomachine
02/02/17Method for repairing a gas turbine blade having at least one cavity
02/02/17Gas turbine
01/19/17Method for the electroplating of tial alloys
12/29/16Process and producing forged tial components
12/29/16Seal carrier, guide vane ring and turbomachine
12/22/16Device and additively producing at least one component region of a component
12/22/16Device and additively producing at least one component region of a component
12/15/16Low noise turbine for geared turbofan engine
12/15/16Rotor for a turbomachine and compressor
12/01/16Clamping device for joining flange pieces
11/24/16Method and device for determining a contour, at least in regions, of at least one additively manufactured component layer
11/17/16Manufacture of blade channels of turbomachine rotors
11/17/16Combination of blade tip cladding and erosion-resistant layer and the production thereof
11/17/16Masking producing a combination of blade tip hardfacing and erosion-protection coating
11/10/16Rotor arrangement for a turbomachine and compressor
11/10/16Turbomachine blade
11/10/16Gas turbine guide vane element
11/10/16Turbomachine having a seal device
11/10/16Rotor drum for a turbomachine and compressor
11/10/16Method for manufacturing brush seals with obliquely positioned bristles and a corresponding device
10/27/16Repair of monocrystalline flow channel segments by monocrystalline remelting
10/13/16Method for evaluating at least one component layer manufactured by means of an additive powder layer method
10/13/16Composite ceramic comprising a corrosion protection layer and production method
10/13/16Method for joining at least two rotor elements of a turbomachine
10/06/16Method and device for additively manufacturing at least one component region of a component
10/06/16Method for additive manufacturing of a gas turbine casing part
09/22/16Method for producing a component from a composite material comprising a metal matrix and incorporated intermetallic phases
09/22/16Blade of a turbomachine made of different materials and the production thereof
09/22/16Protective device for a turbomachine
09/22/16Method for producing a component
09/22/16Maintenance of a used gas turbine
09/22/16Method and device for the quality evaluation of a component produced by means of an additive manufacturing method
09/08/16Device and partially masking a component zone of a component
Patent Packs
09/08/16Method for determing a transition point and/or for determining wall shear stresses on surfaces around which surfaces a flow circulates, and measuring device
09/08/16Diagnosis of aircraft gas turbine engines
08/25/16Locking element and turbomachine
08/25/16Method for producing a component, and the corresponding component
08/18/16Blade, shroud and turbomachine
08/18/16Axially divided inner ring for a turbomachine and guide vane ring
08/18/16Axially split inner ring for a fluid flow machine, guide vane ring, and aircraft engine
08/11/16Gas turbine component
08/04/16Powder build unit, corresponding device, and method employing a powder build unit
08/04/16Guide vane ring for a turbomachine
07/28/16Device and the manufacture or repair of a three-dimensional object
07/28/16Adjustable guide vane for a turbomachine
07/28/16Gas turbine axial compressor
07/28/16Device and attaching seal elements
07/14/16Extruded profile for manufacturing a blade of an outlet guide vane
Patent Packs
06/23/16Device for the additive manufacture of a component
06/23/16Cooling-air supply device for a gas turbine
06/16/16Turbomachine having an annulus enlargment and airfoil
06/02/16Low noise turbine for geared turbofan engine
05/26/16Brazing reinforcing the z-notch of tial blades
05/26/16Guide vane ring and turbomachine
05/26/16Blade or vane for a turbomachine and axial turbomachine
05/19/16Blade or vane arrangement for a turbomachine
05/12/16Oxidation-resistant layer for tial materials and the production thereof
05/12/16Low noise turbine for geared turbofan engine
05/12/16Gas turbine
05/05/16Device and the manufacture or repair of a three-dimensional object
05/05/16Repair for the additive repair of a component
05/05/16Slip and process for producing an oxidation- and corrosion-resistant diffusion layer
05/05/16Method for producing a high temperature-resistant target alloy, a device, an alloy and a corresponding component
04/28/16Guide vane ring for a turbomachine and turbomachine
04/21/16Pneumatic needling device
03/17/16Electrochemical machining of a workpiece
03/17/16Temperature regulation for a device for the additive manufacturing of components and corresponding production method
03/10/16Surfacing of additively manufactured components and corresponding manufactured components of a turbomachine
03/03/16Production process for tial components
03/03/16Creep- and oxidation-resistant molybdenum superalloy
03/03/16Gas turbine subassembly
03/03/16Shaft seal system and a compressor having a corresponding shaft seal system
02/25/16Method for the quality assessment of a component produced by means of an additive manufacturing method
02/18/16Apparatus and securing sealing elements
02/11/16Roller bearings, in particular needle bearings, for arranging on a pivot pin of a variable guide vane of a turbomachine
02/04/16Guide blade for a gas turbine
02/04/16Leaf seal for sealing off a shaft rotating around an axis
02/04/16Low noise turbine for geared turbofan engine
Social Network Patent Pack
02/04/16Housing for a gas turbine, aircraft engine, and a process for operating a gas turbine
02/04/16Component arrangement of a gas turbine
02/04/16Turbofan aircraft engine
01/28/16Blade cascade for a turbomachine
01/28/16Turbomachine blade
01/28/16Low noise turbine for geared turbofan engine
01/21/16Equipment and the generative manufacture and/or repair of components
01/21/16Turbofan aircraft engine
01/21/16Method and device for evaluating the quality of a component produced by means of an additive laser sintering and/or laser melting method
01/14/16Antifouling layer for compressor blades
Patent Packs
01/14/16Al-rich high-temperature tial alloy
01/14/16Turbomachine blade
01/14/16Wear protection arrangement for a turbomachine, process and compressor
01/07/16Brush seal
12/31/15Leiteinrichtung fur eine gasturbine sowie gasturbine mit einer solchen leiteinrichtung
12/31/15Brush seal system for sealing a clearance between components of a turbo engine that are movable in relation to one another
12/31/15Component arrangement for a gas turbine
12/17/15Mid-frame for a gas turbine and gas turbine having such a mid-frame
11/19/15Casing arrangement for a gas turbine
11/19/15Mid-frame for a gas turbine and gas turbine
11/12/15Seal, producing a seal and turbomachine
11/12/15Device and generative production of at least one component area of a component
11/05/15Lightweight structural nial alloy with a high high-temperature strength
10/29/15Bearing cage and bearing means having this type of bearing cage as well as designing, repairing and/or replacing such a bearing cage
10/22/15Aircraft engine
10/15/15Device for the generative production of a component
10/15/15Method and device for improving material quality in generative manufacturing methods
10/08/15Nickel-based alloy with optimized matrix properties
10/08/15Gas turbine compressor
10/01/15Guide vane ring ,guide vane, inner ring and turbomachine
10/01/15Method and device for ascertaining an edge layer characteristic of a component
09/24/15Safety device for a bearing arrangement of a rotor of a turbomachine
09/17/15Method for designing a turbine
09/10/15Device and the generative production of a component
09/10/15Anti-ice coating for compressor blades
09/10/15Gas turbine duct casing
Patent Packs
09/03/15Apparatus and generative production of a component
09/03/15Creation of residual compressive stresses during additve manufacturing
08/13/15Thrust deflecting device and aircraft engine
08/06/15High-temperature tial alloy
08/06/15Method and determining residual stresses of a component
07/23/15Low noise turbine for geared turbofan engine
07/16/15Brush seal having brush filaments of nonmetallic materials
07/09/15Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
07/09/15Gas turbine
07/09/15Gas turbine
06/18/15Method for producing a cylindrical component
06/18/15Irradiation in generative fabrication
06/18/15Gas turbinen rotor blade
06/18/15Blade cascade
06/18/15Blade cascade
06/11/15Gas turbine
06/04/15Sealing element, sealing unit, and turbomachine
05/28/15Material of laves phase and ferritic fe-al phase
05/21/15Run-in coating based on metal fibers
05/21/15Array of flow-directing elements for a gas turbine compressor
Social Network Patent Pack
05/21/15Rotor of a turbomachine
05/21/15Blade-disk assembly, method and turbomachine
05/14/15Method for producing low-pressure turbine blades from tial
05/14/15Gas turbine
05/14/15Inner ring of a fluid flow machine and stator vane array
05/14/15Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
05/07/15Seal configuration for a turbo machine
04/30/15Identifying and regulating the starting behavior during electrochemical machining of workpieces
04/09/15Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
04/09/15Component support and turbomachine
04/02/15Brush seal for a turbomachine
04/02/15Blade for a gas turbine
04/02/15Method for performing maintenance on an engine
03/26/15Brush seal and producing a brush seal
03/26/15Bauteilsystem einer turbomaschine
03/26/15Creep-resistant tial alloy
03/19/15Wear-resistant coating produced by electrodeposition and process therefor
Social Network Patent Pack
03/19/15Seal arrangement for a turbomachine and process for the production thereof
03/19/15Slip and process for producing an aluminum diffusion layer
03/12/15Method for disassembly and assembly of a rotor of a gas turbine
03/05/15Apparatus for laser materials processing
03/05/15Sealing arrangement in an axial turbomachine
03/05/15Apparatus for energy absorption, a turbo-machine and a energy absorption
03/05/15Multiple coil arrangement for a device for generative production of components and corresponding production method
03/05/15Cr(vi)-free corrosion protection layers or adhesion promoter layers produced using a solution comprising phosphate ions and metal powder, wherein the metal powder is coated at least partly with si or si alloys
03/05/15Heat insulation layer system with corrosion and erosion protection
02/19/15Intermetallic wear-resistant layer for titanium materials
02/12/15Blade cascade and turbomachine
02/05/15Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
01/29/15Method for repairing a receiving hook for guide vanes
01/29/15Multipart electrode array and the electrochemical treatment of blades having shrouding bands
01/29/15Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
01/22/15Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
01/15/15Cmas-inert thermal barrier layer and producing the same
01/15/15Ceramic component for a turbomachine
01/15/15Turbomachine, sealing segment, and guide vane segment
01/15/15Method of producing an insulation element and insulation element for a housing of an aero engine
01/15/15Guide vane arragement and mounting a guide vane
01/15/15Gas turbine stage
01/15/15Gas turbine compressor stator vane assembly
01/15/15Blade for a gas turbomachine
01/15/15Control in generative production
01/15/15Method for the non-destructive testing of workpiece surfaces
01/08/15Blade row poisitioning device, blade-device combination, method and turbomachine
01/01/15Dichteinrichtung und stromungsmaschine
01/01/15Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
Social Network Patent Pack
01/01/15Turbomachine, circulation structure and method
01/01/15Turbomachine rotor blade
12/18/14Method for closing cooling air bores
12/18/14Method for producing forged components from a tial alloy and component produced thereby
12/11/14Method for coating components
12/04/14Rhenium-free or rhenium-reduced nickel-base superalloy
12/04/14Tial blade with surface modification
11/27/14Adapter and turbomachine
11/27/14Split inner ring
11/27/14Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
11/27/14Turbomachine stage and detecting a sealing gap of such a turbomachine stage
11/27/14Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
11/27/14Balancing body for a continuous blade arrangement
11/27/14Blade cascade and continuous-flow machine
11/27/14Blade row, blade and turbomachine
11/13/14Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
10/30/14Slide ring seal
10/30/14Housing section of a turbine engine compressor stage or turbine engine turbine stage
10/30/14Process for producing a high-temperature protective coating and correspondingly produced component
10/16/14Armoring sealing fins of tial vanes by induction brazing hard-material particles
10/09/14Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
10/09/14Guide vane arrangement
10/09/14Blade cascade for turbo machine
10/09/14Securing blade assortment
10/09/14Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
10/09/14Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
09/11/14Twist prevention for turbomachinery

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 Ag 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 Ag with additional patents listed. Browse our Agent directory for other possible listings. Page by