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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 2015 2014 2013 2012 2011 2010 2009 | Company Directory "M" | Mtu Aero Engines Ag-related inventors

Search recent Press Releases: Mtu Aero Engines Ag-related press releases
Count Application # Date Mtu Aero Engines Ag patents (updated weekly) - BOOKMARK this page
12015013978605/21/15 new patent  Run-in coating based on metal fibers
22015013978905/21/15 new patent  Array of flow-directing elements for a gas turbine compressor
32015013980805/21/15 new patent  Rotor of a turbomachine
42015013981105/21/15 new patent  Blade-disk assembly, method and turbomachine
52015012958305/14/15Method for producing low-pressure turbine blades from tial
72015013212305/14/15Gas turbine
82015013212405/14/15Inner ring of a fluid flow machine and stator vane array
92015013213605/14/15Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
102015012527805/07/15Seal configuration for a turbo machine
112015011484404/30/15Identifying and regulating the starting behavior during electrochemical machining of workpieces
132015009879804/09/15Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
142015009879904/09/15Component support and turbomachine
162015009323504/02/15Brush seal for a turbomachine
172015009324904/02/15Blade for a gas turbine
182015009493104/02/15Method for performing maintenance on an engine
192015008428503/26/15Brush seal and producing a brush seal
202015008633103/26/15Bauteilsystem einer turbomaschine
212015008641403/26/15Creep-resistant tial alloy
222015007532703/19/15Wear-resistant coating produced by electrodeposition and process therefor
232015007889303/19/15Seal arrangement for a turbomachine and process for the production thereof
242015007927803/19/15Slip and process for producing an aluminum diffusion layer
252015007176903/12/15Method for disassembly and assembly of a rotor of a gas turbine
262015006042203/05/15Apparatus for laser materials processing
272015006122803/05/15Sealing arrangement in an axial turbomachine
292015006398603/05/15Apparatus for energy absorption, a turbo-machine and a energy absorption
302015006405003/05/15Multiple coil arrangement for a device for generative production of components and corresponding production method
312015006435403/05/15Cr(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
322015006443003/05/15Heat insulation layer system with corrosion and erosion protection
332015005051102/19/15Intermetallic wear-resistant layer for titanium materials
342015004403802/12/15Blade cascade and turbomachine
352015003716102/05/15Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
362015002694401/29/15Method for repairing a receiving hook for guide vanes
372015002790401/29/15Multipart electrode array and the electrochemical treatment of blades having shrouding bands
382015003043401/29/15Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
392015002119901/22/15Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
402015001417901/15/15Cmas-inert thermal barrier layer and producing the same
412015001695701/15/15Ceramic component for a turbomachine
422015001696901/15/15Turbomachine, sealing segment, and guide vane segment
432015001697401/15/15Method of producing an insulation element and insulation element for a housing of an aero engine
442015001698401/15/15Guide vane arragement and mounting a guide vane
452015001698501/15/15Gas turbine stage
462015001698601/15/15Gas turbine compressor stator vane assembly
472015001701101/15/15Blade for a gas turbomachine
482015001705401/15/15Control in generative production
492015001773601/15/15Method for the non-destructive testing of workpiece surfaces
502015001039601/08/15Blade row poisitioning device, blade-device combination, method and turbomachine
512015000181101/01/15Dichteinrichtung und stromungsmaschine
522015000397001/01/15Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
532015000397601/01/15Turbomachine, circulation structure and method
542015000398801/01/15Turbomachine rotor blade
552014036637412/18/14Method for closing cooling air bores
562014036982212/18/14Method for producing forged components from a tial alloy and component produced thereby
572014036066412/11/14Method for coating components
582014035618312/04/14Rhenium-free or rhenium-reduced nickel-base superalloy
592014035664412/04/14Tial blade with surface modification
602014034676811/27/14Adapter and turbomachine
612014034844911/27/14Split inner ring
622014034863111/27/14Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
632014034863211/27/14Turbomachine stage and detecting a sealing gap of such a turbomachine stage
642014034863311/27/14Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
652014034865511/27/14Balancing body for a continuous blade arrangement
662014034866011/27/14Blade cascade and continuous-flow machine
672014034866111/27/14Blade row, blade and turbomachine
682014033492411/13/14Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
692014032196910/30/14Slide ring seal
702014032199810/30/14Housing section of a turbine engine compressor stage or turbine engine turbine stage
712014032255510/30/14Process for producing a high-temperature protective coating and correspondingly produced component
722014030811710/16/14Armoring sealing fins of tial vanes by induction brazing hard-material particles
732014029877210/09/14Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
742014030184010/09/14Guide vane arrangement
752014030185210/09/14Blade cascade for turbo machine
762014030185310/09/14Securing blade assortment
772014030185410/09/14Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
782014030186010/09/14Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
802014025518309/11/14Twist prevention for turbomachinery
822014023955308/28/14Multi-frequency induction heating of generatively produced components
832014023955408/28/14Process and device for producing a three-dimensional object
842014022708008/14/14Seal support of titanium aluminide for a turbomachine
852014022710208/14/14Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
862014020260107/24/14Forged tial components, and producing same
872014017820106/26/14Turbine blade having a shroud and a cutting tooth
882014015926606/12/14Method and device for the generative production of a component
892014016159006/12/14Cover device, integrally bladed main rotor body, method and turbomachine
902014016160106/12/14Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
922014016162406/12/14Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
932014011994105/01/14Creep-resistant, rhenium-free nickel base superalloy
942014009495004/03/14Method for the production of an abradable spray coating
952014007603803/20/14Checking a blade contour of a turbomachine
962014006534303/06/14Device for producing, repairing and/or replacing a component by means of a powder that can be solidified by energy radiation, method and component produced according to said method
972014004452602/13/14Stationary blade ring, assembly method and turbomachine
982014004453202/13/14Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
992014004453702/13/14Gas turbine
1002014004454602/13/14Bladed rotor for a turbomachine
1012014004454902/13/14Ductile compensation layer for brittle components
1022014004455002/13/14Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1032014004455102/13/14Blade cascade with side wall contours and continuous-flow machine
1042014004493802/13/14Process for producing a component-matched protective layer and component having such a protective layer
1052014004498602/13/14Duplex-phase cral coating for improved corrosion/oxidation protection
1062013034394712/26/13Method and device for process monitoring
1072013028759010/31/13Generatively produced turbine blade and device and producing same
1082013028043910/24/13Method for the layered manufacturing of a structural component and device

ARCHIVE: New 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