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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
12016003274802/04/16  new patent  Guide blade for a gas turbine
22016003274902/04/16  new patent  Leaf seal for sealing off a shaft rotating around an axis
32016003275602/04/16  new patent  Low noise turbine for geared turbofan engine
42016003276002/04/16  new patent  Housing for a gas turbine, aircraft engine, and a process for operating a gas turbine
52016003277702/04/16  new patent  Component arrangement of a gas turbine
62016003282602/04/16  new patent  Turbofan aircraft engine
72016002492801/28/16 Blade cascade for a turbomachine
82016002494501/28/16 Turbomachine blade
92016002500401/28/16 Low noise turbine for geared turbofan engine
102016001633601/21/16 Equipment and the generative manufacture and/or repair of components
112016001779701/21/16 Turbofan aircraft engine
122016001832001/21/16 Method and device for evaluating the quality of a component produced by means of an additive laser sintering and/or laser melting method
132016000992701/14/16 Antifouling layer for compressor blades
142016001018401/14/16 Al-rich high-temperature tial alloy
152016001046201/14/16 Turbomachine blade
162016001048801/14/16 Wear protection arrangement for a turbomachine, process and compressor
172016000336001/07/16 Brush seal
182015037704212/31/15 Leiteinrichtung fur eine gasturbine sowie gasturbine mit einer solchen leiteinrichtung
192015037704912/31/15 Brush seal system for sealing a clearance between components of a turbo engine that are movable in relation to one another
202015037705312/31/15 Turbomachine
212015037706112/31/15 Unknown
222015037706812/31/15 Component arrangement for a gas turbine
232015036189312/17/15 Mid-frame for a gas turbine and gas turbine having such a mid-frame
242015033023711/19/15 Casing arrangement for a gas turbine
252015033040611/19/15 Mid-frame for a gas turbine and gas turbine
262015032280811/12/15 Seal, producing a seal and turbomachine
272015032331811/12/15 Device and generative production of at least one component area of a component
282015032451711/12/15 Unknown
292015031591911/05/15 Lightweight structural nial alloy with a high high-temperature strength
302015030850210/29/15 Bearing cage and bearing means having this type of bearing cage as well as designing, repairing and/or replacing such a bearing cage
312015030025910/22/15 Aircraft engine
322015029067110/15/15 Device for the generative production of a component
332015029071210/15/15 Method and device for improving material quality in generative manufacturing methods
342015028482410/08/15 Nickel-based alloy with optimized matrix properties
352015028507910/08/15 Gas turbine compressor
362015028508010/08/15 Unknown
372015027568310/01/15 Guide vane ring ,guide vane, inner ring and turbomachine
382015027668310/01/15 Method and device for ascertaining an edge layer characteristic of a component
392015026755409/24/15 Safety device for a bearing arrangement of a rotor of a turbomachine
402015026004609/17/15 Method for designing a turbine
412015025125009/10/15 Device and the generative production of a component
422015025219909/10/15 Anti-ice coating for compressor blades
432015025269109/10/15 Gas turbine duct casing
442015024641409/03/15 Apparatus and generative production of a component
452015024648109/03/15 Creation of residual compressive stresses during additve manufacturing
462015022615508/13/15 Thrust deflecting device and aircraft engine
472015021867508/06/15 High-temperature tial alloy
482015021944408/06/15 Method and determining residual stresses of a component
492015020423807/23/15 Low noise turbine for geared turbofan engine
502015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
512015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
522015019202607/09/15 Gas turbine
532015019202807/09/15 Gas turbine
542015016551606/18/15 Method for producing a cylindrical component
552015016554506/18/15 Irradiation in generative fabrication
562015016747706/18/15 Gas turbinen rotor blade
572015016747806/18/15 Blade cascade
582015016747906/18/15 Blade cascade
592015015955106/11/15 Gas turbine
602015015274206/04/15 Sealing element, sealing unit, and turbomachine
612015014722005/28/15 Material of laves phase and ferritic fe-al phase
622015013978605/21/15 Run-in coating based on metal fibers
632015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
642015013980805/21/15 Rotor of a turbomachine
652015013981105/21/15 Blade-disk assembly, method and turbomachine
662015012958305/14/15 Method for producing low-pressure turbine blades from tial
672015013211505/14/15 Unknown
682015013212305/14/15 Gas turbine
692015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
702015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
712015012527805/07/15 Seal configuration for a turbo machine
722015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
732015010256504/16/15 Unknown
742015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
752015009879904/09/15 Component support and turbomachine
762015009880904/09/15 Turbomachine
772015009323504/02/15 Brush seal for a turbomachine
782015009324904/02/15 Blade for a gas turbine
792015009493104/02/15 Method for performing maintenance on an engine
802015008428503/26/15 Brush seal and producing a brush seal
812015008633103/26/15 Bauteilsystem einer turbomaschine
822015008641403/26/15 Creep-resistant tial alloy
832015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
842015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
852015007927803/19/15 Slip and process for producing an aluminum diffusion layer
862015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
872015006042203/05/15 Apparatus for laser materials processing
882015006122803/05/15 Sealing arrangement in an axial turbomachine
892015006398303/05/15 Turbomachine
902015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
912015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
922015006435403/05/15 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
932015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
942015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
952015004403802/12/15 Blade cascade and turbomachine
962015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
972015002694401/29/15 Method for repairing a receiving hook for guide vanes
982015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
992015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
1002015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
1012015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
1022015001695701/15/15 Ceramic component for a turbomachine
1032015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
1042015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
1052015001698401/15/15 Guide vane arragement and mounting a guide vane
1062015001698501/15/15 Gas turbine stage
1072015001698601/15/15 Gas turbine compressor stator vane assembly
1082015001701101/15/15 Blade for a gas turbomachine
1092015001705401/15/15 Control in generative production
1102015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
1112015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
1122015000181101/01/15 Dichteinrichtung und stromungsmaschine
1132015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
1142015000397601/01/15 Turbomachine, circulation structure and method
1152015000398801/01/15 Turbomachine rotor blade
1162014036637412/18/14 Method for closing cooling air bores
1172014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
1182014036066412/11/14 Method for coating components
1192014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
1202014035664412/04/14 Tial blade with surface modification
1212014034676811/27/14 Adapter and turbomachine
1222014034844911/27/14 Split inner ring
1232014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
1242014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
1252014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
1262014034865511/27/14 Balancing body for a continuous blade arrangement
1272014034866011/27/14 Blade cascade and continuous-flow machine
1282014034866111/27/14 Blade row, blade and turbomachine
1292014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
1302014032196910/30/14 Slide ring seal
1312014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
1322014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
1332014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
1342014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
1352014030184010/09/14 Guide vane arrangement
1362014030185210/09/14 Blade cascade for turbo machine
1372014030185310/09/14 Securing blade assortment
1382014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
1392014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
1402014029457010/02/14 Turbomachine
1412014025518309/11/14 Twist prevention for turbomachinery
1422014024683509/04/14 Component
1432014023955308/28/14 Multi-frequency induction heating of generatively produced components
1442014023955408/28/14 Process and device for producing a three-dimensional object
1452014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1462014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1472014020260107/24/14 Forged tial components, and producing same
1482014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1492014015926606/12/14 Method and device for the generative production of a component
1502014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1512014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1522014016160706/12/14 Turbomachine
1532014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1542014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1552014009495004/03/14 Method for the production of an abradable spray coating
1562014007603803/20/14 Checking a blade contour of a turbomachine
1572014006534303/06/14 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
1582014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1592014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1602014004453702/13/14 Gas turbine
1612014004454602/13/14 Bladed rotor for a turbomachine
1622014004454902/13/14 Ductile compensation layer for brittle components
1632014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1642014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1652014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1662014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1672013034394712/26/13 Method and device for process monitoring
1682013028759010/31/13 Generatively produced turbine blade and device and producing same
1692013028043910/24/13 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