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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
12015006042203/05/15 new patent  Apparatus for laser materials processing
22015006122803/05/15 new patent  Sealing arrangement in an axial turbomachine
32015006398303/05/15 new patent  Turbomachine
42015006398603/05/15 new patent  Apparatus for energy absorption, a turbo-machine and a energy absorption
52015006405003/05/15 new patent  Multiple coil arrangement for a device for generative production of components and corresponding production method
62015006435403/05/15 new patent  Cr(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
72015006443003/05/15 new patent  Heat insulation layer system with corrosion and erosion protection
82015005051102/19/15Intermetallic wear-resistant layer for titanium materials
92015004403802/12/15Blade cascade and turbomachine
102015003716102/05/15Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
112015002694401/29/15Method for repairing a receiving hook for guide vanes
122015002790401/29/15Multipart electrode array and the electrochemical treatment of blades having shrouding bands
132015003043401/29/15Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
142015002119901/22/15Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
152015001417901/15/15Cmas-inert thermal barrier layer and producing the same
162015001695701/15/15Ceramic component for a turbomachine
172015001696901/15/15Turbomachine, sealing segment, and guide vane segment
182015001697401/15/15Method of producing an insulation element and insulation element for a housing of an aero engine
192015001698401/15/15Guide vane arragement and mounting a guide vane
202015001698501/15/15Gas turbine stage
212015001698601/15/15Gas turbine compressor stator vane assembly
222015001701101/15/15Blade for a gas turbomachine
232015001705401/15/15Control in generative production
242015001773601/15/15Method for the non-destructive testing of workpiece surfaces
252015001039601/08/15Blade row poisitioning device, blade-device combination, method and turbomachine
262015000181101/01/15Dichteinrichtung und stromungsmaschine
272015000397001/01/15Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
282015000397601/01/15Turbomachine, circulation structure and method
292015000398801/01/15Turbomachine rotor blade
302014036637412/18/14Method for closing cooling air bores
312014036982212/18/14Method for producing forged components from a tial alloy and component produced thereby
322014036066412/11/14Method for coating components
332014035618312/04/14Rhenium-free or rhenium-reduced nickel-base superalloy
342014035664412/04/14Tial blade with surface modification
352014034676811/27/14Adapter and turbomachine
362014034844911/27/14Split inner ring
372014034863111/27/14Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
382014034863211/27/14Turbomachine stage and detecting a sealing gap of such a turbomachine stage
392014034863311/27/14Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
402014034865511/27/14Balancing body for a continuous blade arrangement
412014034866011/27/14Blade cascade and continuous-flow machine
422014034866111/27/14Blade row, blade and turbomachine
432014033492411/13/14Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
442014032196910/30/14Slide ring seal
452014032199810/30/14Housing section of a turbine engine compressor stage or turbine engine turbine stage
462014032255510/30/14Process for producing a high-temperature protective coating and correspondingly produced component
472014030811710/16/14Armoring sealing fins of tial vanes by induction brazing hard-material particles
482014029877210/09/14Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
492014030184010/09/14Guide vane arrangement
502014030185210/09/14Blade cascade for turbo machine
512014030185310/09/14Securing blade assortment
522014030185410/09/14Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
532014030186010/09/14Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
552014025518309/11/14Twist prevention for turbomachinery
572014023955308/28/14Multi-frequency induction heating of generatively produced components
582014023955408/28/14Process and device for producing a three-dimensional object
592014022708008/14/14Seal support of titanium aluminide for a turbomachine
602014022710208/14/14Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
612014020260107/24/14Forged tial components, and producing same
622014017820106/26/14Turbine blade having a shroud and a cutting tooth
632014015926606/12/14Method and device for the generative production of a component
642014016159006/12/14Cover device, integrally bladed main rotor body, method and turbomachine
652014016160106/12/14Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
672014016162406/12/14Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
682014011994105/01/14Creep-resistant, rhenium-free nickel base superalloy
692014009495004/03/14Method for the production of an abradable spray coating
702014007603803/20/14Checking a blade contour of a turbomachine
712014006534303/06/14Device 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
722014004452602/13/14Stationary blade ring, assembly method and turbomachine
732014004453202/13/14Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
742014004453702/13/14Gas turbine
752014004454602/13/14Bladed rotor for a turbomachine
762014004454902/13/14Ductile compensation layer for brittle components
772014004455002/13/14Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
782014004455102/13/14Blade cascade with side wall contours and continuous-flow machine
792014004493802/13/14Process for producing a component-matched protective layer and component having such a protective layer
802014004498602/13/14Duplex-phase cral coating for improved corrosion/oxidation protection
812013034394712/26/13Method and device for process monitoring
822013028759010/31/13Generatively produced turbine blade and device and producing same
832013028043910/24/13Method for the layered manufacturing of a structural component and device

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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