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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
12015022615508/13/15 Thrust deflecting device and aircraft engine
22015021867508/06/15 High-temperature tial alloy
32015021944408/06/15 Method and determining residual stresses of a component
42015020423807/23/15 Low noise turbine for geared turbofan engine
52015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
62015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
72015019202607/09/15 Gas turbine
82015019202807/09/15 Gas turbine
92015016551606/18/15 Method for producing a cylindrical component
102015016554506/18/15 Irradiation in generative fabrication
112015016747706/18/15 Gas turbinen rotor blade
122015016747806/18/15 Blade cascade
132015016747906/18/15 Blade cascade
142015015955106/11/15 Gas turbine
152015015274206/04/15 Sealing element, sealing unit, and turbomachine
162015014722005/28/15 Material of laves phase and ferritic fe-al phase
172015013978605/21/15 Run-in coating based on metal fibers
182015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
192015013980805/21/15 Rotor of a turbomachine
202015013981105/21/15 Blade-disk assembly, method and turbomachine
212015012958305/14/15 Method for producing low-pressure turbine blades from tial
222015013211505/14/15 Unknown
232015013212305/14/15 Gas turbine
242015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
252015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
262015012527805/07/15 Seal configuration for a turbo machine
272015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
282015010256504/16/15 Unknown
292015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
302015009879904/09/15 Component support and turbomachine
312015009880904/09/15 Turbomachine
322015009323504/02/15 Brush seal for a turbomachine
332015009324904/02/15 Blade for a gas turbine
342015009493104/02/15 Method for performing maintenance on an engine
352015008428503/26/15 Brush seal and producing a brush seal
362015008633103/26/15 Bauteilsystem einer turbomaschine
372015008641403/26/15 Creep-resistant tial alloy
382015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
392015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
402015007927803/19/15 Slip and process for producing an aluminum diffusion layer
412015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
422015006042203/05/15 Apparatus for laser materials processing
432015006122803/05/15 Sealing arrangement in an axial turbomachine
442015006398303/05/15 Turbomachine
452015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
462015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
472015006435403/05/15 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
482015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
492015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
502015004403802/12/15 Blade cascade and turbomachine
512015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
522015002694401/29/15 Method for repairing a receiving hook for guide vanes
532015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
542015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
552015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
562015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
572015001695701/15/15 Ceramic component for a turbomachine
582015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
592015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
602015001698401/15/15 Guide vane arragement and mounting a guide vane
612015001698501/15/15 Gas turbine stage
622015001698601/15/15 Gas turbine compressor stator vane assembly
632015001701101/15/15 Blade for a gas turbomachine
642015001705401/15/15 Control in generative production
652015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
662015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
672015000181101/01/15 Dichteinrichtung und stromungsmaschine
682015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
692015000397601/01/15 Turbomachine, circulation structure and method
702015000398801/01/15 Turbomachine rotor blade
712014036637412/18/14 Method for closing cooling air bores
722014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
732014036066412/11/14 Method for coating components
742014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
752014035664412/04/14 Tial blade with surface modification
762014034676811/27/14 Adapter and turbomachine
772014034844911/27/14 Split inner ring
782014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
792014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
802014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
812014034865511/27/14 Balancing body for a continuous blade arrangement
822014034866011/27/14 Blade cascade and continuous-flow machine
832014034866111/27/14 Blade row, blade and turbomachine
842014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
852014032196910/30/14 Slide ring seal
862014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
872014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
882014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
892014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
902014030184010/09/14 Guide vane arrangement
912014030185210/09/14 Blade cascade for turbo machine
922014030185310/09/14 Securing blade assortment
932014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
942014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
952014029457010/02/14 Turbomachine
962014025518309/11/14 Twist prevention for turbomachinery
972014024683509/04/14 Component
982014023955308/28/14 Multi-frequency induction heating of generatively produced components
992014023955408/28/14 Process and device for producing a three-dimensional object
1002014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1012014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1022014020260107/24/14 Forged tial components, and producing same
1032014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1042014015926606/12/14 Method and device for the generative production of a component
1052014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1062014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1072014016160706/12/14 Turbomachine
1082014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1092014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1102014009495004/03/14 Method for the production of an abradable spray coating
1112014007603803/20/14 Checking a blade contour of a turbomachine
1122014006534303/06/14 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
1132014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1142014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1152014004453702/13/14 Gas turbine
1162014004454602/13/14 Bladed rotor for a turbomachine
1172014004454902/13/14 Ductile compensation layer for brittle components
1182014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1192014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1202014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1212014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1222013034394712/26/13 Method and device for process monitoring
1232013028759010/31/13 Generatively produced turbine blade and device and producing same
1242013028043910/24/13 Method for the layered manufacturing of a structural component and device



ARCHIVE: New 2015 2014 2013 2012 2011 2010 2009



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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. Freshpatents.com 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 FreshPatents.com

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