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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
12015033023711/19/15 Casing arrangement for a gas turbine
22015033040611/19/15 Mid-frame for a gas turbine and gas turbine
32015032280811/12/15 Seal, producing a seal and turbomachine
42015032331811/12/15 Device and generative production of at least one component area of a component
52015032451711/12/15 Unknown
62015031591911/05/15 Lightweight structural nial alloy with a high high-temperature strength
72015030850210/29/15 Bearing cage and bearing means having this type of bearing cage as well as designing, repairing and/or replacing such a bearing cage
82015030025910/22/15 Aircraft engine
92015029067110/15/15 Device for the generative production of a component
102015029071210/15/15 Method and device for improving material quality in generative manufacturing methods
112015028482410/08/15 Nickel-based alloy with optimized matrix properties
122015028507910/08/15 Gas turbine compressor
132015028508010/08/15 Unknown
142015027568310/01/15 Guide vane ring ,guide vane, inner ring and turbomachine
152015027668310/01/15 Method and device for ascertaining an edge layer characteristic of a component
162015026755409/24/15 Safety device for a bearing arrangement of a rotor of a turbomachine
172015026004609/17/15 Method for designing a turbine
182015025125009/10/15 Device and the generative production of a component
192015025219909/10/15 Anti-ice coating for compressor blades
202015025269109/10/15 Gas turbine duct casing
212015024641409/03/15 Apparatus and generative production of a component
222015024648109/03/15 Creation of residual compressive stresses during additve manufacturing
232015022615508/13/15 Thrust deflecting device and aircraft engine
242015021867508/06/15 High-temperature tial alloy
252015021944408/06/15 Method and determining residual stresses of a component
262015020423807/23/15 Low noise turbine for geared turbofan engine
272015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
282015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
292015019202607/09/15 Gas turbine
302015019202807/09/15 Gas turbine
312015016551606/18/15 Method for producing a cylindrical component
322015016554506/18/15 Irradiation in generative fabrication
332015016747706/18/15 Gas turbinen rotor blade
342015016747806/18/15 Blade cascade
352015016747906/18/15 Blade cascade
362015015955106/11/15 Gas turbine
372015015274206/04/15 Sealing element, sealing unit, and turbomachine
382015014722005/28/15 Material of laves phase and ferritic fe-al phase
392015013978605/21/15 Run-in coating based on metal fibers
402015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
412015013980805/21/15 Rotor of a turbomachine
422015013981105/21/15 Blade-disk assembly, method and turbomachine
432015012958305/14/15 Method for producing low-pressure turbine blades from tial
442015013211505/14/15 Unknown
452015013212305/14/15 Gas turbine
462015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
472015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
482015012527805/07/15 Seal configuration for a turbo machine
492015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
502015010256504/16/15 Unknown
512015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
522015009879904/09/15 Component support and turbomachine
532015009880904/09/15 Turbomachine
542015009323504/02/15 Brush seal for a turbomachine
552015009324904/02/15 Blade for a gas turbine
562015009493104/02/15 Method for performing maintenance on an engine
572015008428503/26/15 Brush seal and producing a brush seal
582015008633103/26/15 Bauteilsystem einer turbomaschine
592015008641403/26/15 Creep-resistant tial alloy
602015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
612015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
622015007927803/19/15 Slip and process for producing an aluminum diffusion layer
632015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
642015006042203/05/15 Apparatus for laser materials processing
652015006122803/05/15 Sealing arrangement in an axial turbomachine
662015006398303/05/15 Turbomachine
672015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
682015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
692015006435403/05/15 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
702015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
712015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
722015004403802/12/15 Blade cascade and turbomachine
732015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
742015002694401/29/15 Method for repairing a receiving hook for guide vanes
752015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
762015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
772015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
782015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
792015001695701/15/15 Ceramic component for a turbomachine
802015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
812015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
822015001698401/15/15 Guide vane arragement and mounting a guide vane
832015001698501/15/15 Gas turbine stage
842015001698601/15/15 Gas turbine compressor stator vane assembly
852015001701101/15/15 Blade for a gas turbomachine
862015001705401/15/15 Control in generative production
872015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
882015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
892015000181101/01/15 Dichteinrichtung und stromungsmaschine
902015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
912015000397601/01/15 Turbomachine, circulation structure and method
922015000398801/01/15 Turbomachine rotor blade
932014036637412/18/14 Method for closing cooling air bores
942014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
952014036066412/11/14 Method for coating components
962014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
972014035664412/04/14 Tial blade with surface modification
982014034676811/27/14 Adapter and turbomachine
992014034844911/27/14 Split inner ring
1002014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
1012014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
1022014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
1032014034865511/27/14 Balancing body for a continuous blade arrangement
1042014034866011/27/14 Blade cascade and continuous-flow machine
1052014034866111/27/14 Blade row, blade and turbomachine
1062014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
1072014032196910/30/14 Slide ring seal
1082014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
1092014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
1102014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
1112014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
1122014030184010/09/14 Guide vane arrangement
1132014030185210/09/14 Blade cascade for turbo machine
1142014030185310/09/14 Securing blade assortment
1152014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
1162014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
1172014029457010/02/14 Turbomachine
1182014025518309/11/14 Twist prevention for turbomachinery
1192014024683509/04/14 Component
1202014023955308/28/14 Multi-frequency induction heating of generatively produced components
1212014023955408/28/14 Process and device for producing a three-dimensional object
1222014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1232014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1242014020260107/24/14 Forged tial components, and producing same
1252014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1262014015926606/12/14 Method and device for the generative production of a component
1272014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1282014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1292014016160706/12/14 Turbomachine
1302014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1312014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1322014009495004/03/14 Method for the production of an abradable spray coating
1332014007603803/20/14 Checking a blade contour of a turbomachine
1342014006534303/06/14 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
1352014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1362014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1372014004453702/13/14 Gas turbine
1382014004454602/13/14 Bladed rotor for a turbomachine
1392014004454902/13/14 Ductile compensation layer for brittle components
1402014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1412014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1422014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1432014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1442013034394712/26/13 Method and device for process monitoring
1452013028759010/31/13 Generatively produced turbine blade and device and producing same
1462013028043910/24/13 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