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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
12015028482410/08/15  new patent  Nickel-based alloy with optimized matrix properties
22015028507910/08/15  new patent  Gas turbine compressor
32015028508010/08/15  new patent  Unknown
42015027568310/01/15 Guide vane ring ,guide vane, inner ring and turbomachine
52015027668310/01/15 Method and device for ascertaining an edge layer characteristic of a component
62015026755409/24/15 Safety device for a bearing arrangement of a rotor of a turbomachine
72015026004609/17/15 Method for designing a turbine
82015025125009/10/15 Device and the generative production of a component
92015025219909/10/15 Anti-ice coating for compressor blades
102015025269109/10/15 Gas turbine duct casing
112015024641409/03/15 Apparatus and generative production of a component
122015024648109/03/15 Creation of residual compressive stresses during additve manufacturing
132015022615508/13/15 Thrust deflecting device and aircraft engine
142015021867508/06/15 High-temperature tial alloy
152015021944408/06/15 Method and determining residual stresses of a component
162015020423807/23/15 Low noise turbine for geared turbofan engine
172015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
182015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
192015019202607/09/15 Gas turbine
202015019202807/09/15 Gas turbine
212015016551606/18/15 Method for producing a cylindrical component
222015016554506/18/15 Irradiation in generative fabrication
232015016747706/18/15 Gas turbinen rotor blade
242015016747806/18/15 Blade cascade
252015016747906/18/15 Blade cascade
262015015955106/11/15 Gas turbine
272015015274206/04/15 Sealing element, sealing unit, and turbomachine
282015014722005/28/15 Material of laves phase and ferritic fe-al phase
292015013978605/21/15 Run-in coating based on metal fibers
302015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
312015013980805/21/15 Rotor of a turbomachine
322015013981105/21/15 Blade-disk assembly, method and turbomachine
332015012958305/14/15 Method for producing low-pressure turbine blades from tial
342015013211505/14/15 Unknown
352015013212305/14/15 Gas turbine
362015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
372015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
382015012527805/07/15 Seal configuration for a turbo machine
392015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
402015010256504/16/15 Unknown
412015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
422015009879904/09/15 Component support and turbomachine
432015009880904/09/15 Turbomachine
442015009323504/02/15 Brush seal for a turbomachine
452015009324904/02/15 Blade for a gas turbine
462015009493104/02/15 Method for performing maintenance on an engine
472015008428503/26/15 Brush seal and producing a brush seal
482015008633103/26/15 Bauteilsystem einer turbomaschine
492015008641403/26/15 Creep-resistant tial alloy
502015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
512015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
522015007927803/19/15 Slip and process for producing an aluminum diffusion layer
532015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
542015006042203/05/15 Apparatus for laser materials processing
552015006122803/05/15 Sealing arrangement in an axial turbomachine
562015006398303/05/15 Turbomachine
572015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
582015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
592015006435403/05/15 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
602015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
612015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
622015004403802/12/15 Blade cascade and turbomachine
632015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
642015002694401/29/15 Method for repairing a receiving hook for guide vanes
652015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
662015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
672015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
682015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
692015001695701/15/15 Ceramic component for a turbomachine
702015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
712015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
722015001698401/15/15 Guide vane arragement and mounting a guide vane
732015001698501/15/15 Gas turbine stage
742015001698601/15/15 Gas turbine compressor stator vane assembly
752015001701101/15/15 Blade for a gas turbomachine
762015001705401/15/15 Control in generative production
772015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
782015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
792015000181101/01/15 Dichteinrichtung und stromungsmaschine
802015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
812015000397601/01/15 Turbomachine, circulation structure and method
822015000398801/01/15 Turbomachine rotor blade
832014036637412/18/14 Method for closing cooling air bores
842014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
852014036066412/11/14 Method for coating components
862014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
872014035664412/04/14 Tial blade with surface modification
882014034676811/27/14 Adapter and turbomachine
892014034844911/27/14 Split inner ring
902014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
912014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
922014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
932014034865511/27/14 Balancing body for a continuous blade arrangement
942014034866011/27/14 Blade cascade and continuous-flow machine
952014034866111/27/14 Blade row, blade and turbomachine
962014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
972014032196910/30/14 Slide ring seal
982014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
992014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
1002014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
1012014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
1022014030184010/09/14 Guide vane arrangement
1032014030185210/09/14 Blade cascade for turbo machine
1042014030185310/09/14 Securing blade assortment
1052014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
1062014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
1072014029457010/02/14 Turbomachine
1082014025518309/11/14 Twist prevention for turbomachinery
1092014024683509/04/14 Component
1102014023955308/28/14 Multi-frequency induction heating of generatively produced components
1112014023955408/28/14 Process and device for producing a three-dimensional object
1122014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1132014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1142014020260107/24/14 Forged tial components, and producing same
1152014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1162014015926606/12/14 Method and device for the generative production of a component
1172014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1182014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1192014016160706/12/14 Turbomachine
1202014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1212014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1222014009495004/03/14 Method for the production of an abradable spray coating
1232014007603803/20/14 Checking a blade contour of a turbomachine
1242014006534303/06/14 Device 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
1252014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1262014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1272014004453702/13/14 Gas turbine
1282014004454602/13/14 Bladed rotor for a turbomachine
1292014004454902/13/14 Ductile compensation layer for brittle components
1302014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1312014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1322014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1332014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1342013034394712/26/13 Method and device for process monitoring
1352013028759010/31/13 Generatively produced turbine blade and device and producing same
1362013028043910/24/13 Method 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