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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 2016 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
12016011596604/28/16  new patent  Guide vane ring for a turbomachine and turbomachine
22016010848704/21/16 Pneumatic needling device
32016007495203/17/16 Electrochemical machining of a workpiece
42016007496503/17/16 Temperature regulation for a device for the additive manufacturing of components and corresponding production method
52016006782803/10/16 Surfacing of additively manufactured components and corresponding manufactured components of a turbomachine
62016005931203/03/16 Production process for tial components
72016006073403/03/16 Creep- and oxidation-resistant molybdenum superalloy
82016006111103/03/16 Gas turbine subassembly
92016006111603/03/16 Shaft seal system and a compressor having a corresponding shaft seal system
102016005423102/25/16 Method for the quality assessment of a component produced by means of an additive manufacturing method
112016004726202/18/16 Apparatus and securing sealing elements
122016004071302/11/16 Roller bearings, in particular needle bearings, for arranging on a pivot pin of a variable guide vane of a turbomachine
132016003274802/04/16 Guide blade for a gas turbine
142016003274902/04/16 Leaf seal for sealing off a shaft rotating around an axis
152016003275602/04/16 Low noise turbine for geared turbofan engine
162016003276002/04/16 Housing for a gas turbine, aircraft engine, and a process for operating a gas turbine
172016003277702/04/16 Component arrangement of a gas turbine
182016003282602/04/16 Turbofan aircraft engine
192016002492801/28/16 Blade cascade for a turbomachine
202016002494501/28/16 Turbomachine blade
212016002500401/28/16 Low noise turbine for geared turbofan engine
222016001633601/21/16 Equipment and the generative manufacture and/or repair of components
232016001779701/21/16 Turbofan aircraft engine
242016001832001/21/16 Method and device for evaluating the quality of a component produced by means of an additive laser sintering and/or laser melting method
252016000992701/14/16 Antifouling layer for compressor blades
262016001018401/14/16 Al-rich high-temperature tial alloy
272016001046201/14/16 Turbomachine blade
282016001048801/14/16 Wear protection arrangement for a turbomachine, process and compressor
292016000336001/07/16 Brush seal
302015037704212/31/15 Leiteinrichtung fur eine gasturbine sowie gasturbine mit einer solchen leiteinrichtung
312015037704912/31/15 Brush seal system for sealing a clearance between components of a turbo engine that are movable in relation to one another
322015037705312/31/15 Turbomachine
332015037706112/31/15 Unknown
342015037706812/31/15 Component arrangement for a gas turbine
352015036189312/17/15 Mid-frame for a gas turbine and gas turbine having such a mid-frame
362015033023711/19/15 Casing arrangement for a gas turbine
372015033040611/19/15 Mid-frame for a gas turbine and gas turbine
382015032280811/12/15 Seal, producing a seal and turbomachine
392015032331811/12/15 Device and generative production of at least one component area of a component
402015032451711/12/15 Unknown
412015031591911/05/15 Lightweight structural nial alloy with a high high-temperature strength
422015030850210/29/15 Bearing cage and bearing means having this type of bearing cage as well as designing, repairing and/or replacing such a bearing cage
432015030025910/22/15 Aircraft engine
442015029067110/15/15 Device for the generative production of a component
452015029071210/15/15 Method and device for improving material quality in generative manufacturing methods
462015028482410/08/15 Nickel-based alloy with optimized matrix properties
472015028507910/08/15 Gas turbine compressor
482015028508010/08/15 Unknown
492015027568310/01/15 Guide vane ring ,guide vane, inner ring and turbomachine
502015027668310/01/15 Method and device for ascertaining an edge layer characteristic of a component
512015026755409/24/15 Safety device for a bearing arrangement of a rotor of a turbomachine
522015026004609/17/15 Method for designing a turbine
532015025125009/10/15 Device and the generative production of a component
542015025219909/10/15 Anti-ice coating for compressor blades
552015025269109/10/15 Gas turbine duct casing
562015024641409/03/15 Apparatus and generative production of a component
572015024648109/03/15 Creation of residual compressive stresses during additve manufacturing
582015022615508/13/15 Thrust deflecting device and aircraft engine
592015021867508/06/15 High-temperature tial alloy
602015021944408/06/15 Method and determining residual stresses of a component
612015020423807/23/15 Low noise turbine for geared turbofan engine
622015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
632015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
642015019202607/09/15 Gas turbine
652015019202807/09/15 Gas turbine
662015016551606/18/15 Method for producing a cylindrical component
672015016554506/18/15 Irradiation in generative fabrication
682015016747706/18/15 Gas turbinen rotor blade
692015016747806/18/15 Blade cascade
702015016747906/18/15 Blade cascade
712015015955106/11/15 Gas turbine
722015015274206/04/15 Sealing element, sealing unit, and turbomachine
732015014722005/28/15 Material of laves phase and ferritic fe-al phase
742015013978605/21/15 Run-in coating based on metal fibers
752015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
762015013980805/21/15 Rotor of a turbomachine
772015013981105/21/15 Blade-disk assembly, method and turbomachine
782015012958305/14/15 Method for producing low-pressure turbine blades from tial
792015013211505/14/15 Unknown
802015013212305/14/15 Gas turbine
812015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
822015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
832015012527805/07/15 Seal configuration for a turbo machine
842015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
852015010256504/16/15 Unknown
862015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
872015009879904/09/15 Component support and turbomachine
882015009880904/09/15 Turbomachine
892015009323504/02/15 Brush seal for a turbomachine
902015009324904/02/15 Blade for a gas turbine
912015009493104/02/15 Method for performing maintenance on an engine
922015008428503/26/15 Brush seal and producing a brush seal
932015008633103/26/15 Bauteilsystem einer turbomaschine
942015008641403/26/15 Creep-resistant tial alloy
952015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
962015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
972015007927803/19/15 Slip and process for producing an aluminum diffusion layer
982015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
992015006042203/05/15 Apparatus for laser materials processing
1002015006122803/05/15 Sealing arrangement in an axial turbomachine
1012015006398303/05/15 Turbomachine
1022015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
1032015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
1042015006435403/05/15 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
1052015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
1062015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
1072015004403802/12/15 Blade cascade and turbomachine
1082015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
1092015002694401/29/15 Method for repairing a receiving hook for guide vanes
1102015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
1112015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
1122015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
1132015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
1142015001695701/15/15 Ceramic component for a turbomachine
1152015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
1162015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
1172015001698401/15/15 Guide vane arragement and mounting a guide vane
1182015001698501/15/15 Gas turbine stage
1192015001698601/15/15 Gas turbine compressor stator vane assembly
1202015001701101/15/15 Blade for a gas turbomachine
1212015001705401/15/15 Control in generative production
1222015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
1232015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
1242015000181101/01/15 Dichteinrichtung und stromungsmaschine
1252015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
1262015000397601/01/15 Turbomachine, circulation structure and method
1272015000398801/01/15 Turbomachine rotor blade
1282014036637412/18/14 Method for closing cooling air bores
1292014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
1302014036066412/11/14 Method for coating components
1312014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
1322014035664412/04/14 Tial blade with surface modification
1332014034676811/27/14 Adapter and turbomachine
1342014034844911/27/14 Split inner ring
1352014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
1362014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
1372014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
1382014034865511/27/14 Balancing body for a continuous blade arrangement
1392014034866011/27/14 Blade cascade and continuous-flow machine
1402014034866111/27/14 Blade row, blade and turbomachine
1412014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
1422014032196910/30/14 Slide ring seal
1432014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
1442014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
1452014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
1462014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
1472014030184010/09/14 Guide vane arrangement
1482014030185210/09/14 Blade cascade for turbo machine
1492014030185310/09/14 Securing blade assortment
1502014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
1512014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
1522014029457010/02/14 Turbomachine
1532014025518309/11/14 Twist prevention for turbomachinery
1542014024683509/04/14 Component
1552014023955308/28/14 Multi-frequency induction heating of generatively produced components
1562014023955408/28/14 Process and device for producing a three-dimensional object
1572014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1582014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1592014020260107/24/14 Forged tial components, and producing same
1602014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1612014015926606/12/14 Method and device for the generative production of a component
1622014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1632014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1642014016160706/12/14 Turbomachine
1652014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1662014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1672014009495004/03/14 Method for the production of an abradable spray coating
1682014007603803/20/14 Checking a blade contour of a turbomachine
1692014006534303/06/14 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
1702014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1712014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1722014004453702/13/14 Gas turbine
1732014004454602/13/14 Bladed rotor for a turbomachine
1742014004454902/13/14 Ductile compensation layer for brittle components
1752014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1762014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1772014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1782014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1792013034394712/26/13 Method and device for process monitoring
1802013028759010/31/13 Generatively produced turbine blade and device and producing same
1812013028043910/24/13 Method for the layered manufacturing of a structural component and device

ARCHIVE: New 2016 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