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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
12016014602005/26/16  new patent  Brazing reinforcing the z-notch of tial blades
22016014602705/26/16  new patent  Guide vane ring and turbomachine
32016014604105/26/16  new patent  Blade or vane for a turbomachine and axial turbomachine
42016013840105/19/16 Blade or vane arrangement for a turbomachine
52016013070405/12/16 Oxidation-resistant layer for tial materials and the production thereof
62016013094905/12/16 Low noise turbine for geared turbofan engine
72016013102805/12/16 Gas turbine
82016012139805/05/16 Device and the manufacture or repair of a three-dimensional object
92016012143805/05/16 Repair for the additive repair of a component
102016012255505/05/16 Slip and process for producing an oxidation- and corrosion-resistant diffusion layer
112016012285005/05/16 Method for producing a high temperature-resistant target alloy, a device, an alloy and a corresponding component
122016011596604/28/16 Guide vane ring for a turbomachine and turbomachine
132016010848704/21/16 Pneumatic needling device
142016007495203/17/16 Electrochemical machining of a workpiece
152016007496503/17/16 Temperature regulation for a device for the additive manufacturing of components and corresponding production method
162016006782803/10/16 Surfacing of additively manufactured components and corresponding manufactured components of a turbomachine
172016005931203/03/16 Production process for tial components
182016006073403/03/16 Creep- and oxidation-resistant molybdenum superalloy
192016006111103/03/16 Gas turbine subassembly
202016006111603/03/16 Shaft seal system and a compressor having a corresponding shaft seal system
212016005423102/25/16 Method for the quality assessment of a component produced by means of an additive manufacturing method
222016004726202/18/16 Apparatus and securing sealing elements
232016004071302/11/16 Roller bearings, in particular needle bearings, for arranging on a pivot pin of a variable guide vane of a turbomachine
242016003274802/04/16 Guide blade for a gas turbine
252016003274902/04/16 Leaf seal for sealing off a shaft rotating around an axis
262016003275602/04/16 Low noise turbine for geared turbofan engine
272016003276002/04/16 Housing for a gas turbine, aircraft engine, and a process for operating a gas turbine
282016003277702/04/16 Component arrangement of a gas turbine
292016003282602/04/16 Turbofan aircraft engine
302016002492801/28/16 Blade cascade for a turbomachine
312016002494501/28/16 Turbomachine blade
322016002500401/28/16 Low noise turbine for geared turbofan engine
332016001633601/21/16 Equipment and the generative manufacture and/or repair of components
342016001779701/21/16 Turbofan aircraft engine
352016001832001/21/16 Method and device for evaluating the quality of a component produced by means of an additive laser sintering and/or laser melting method
362016000992701/14/16 Antifouling layer for compressor blades
372016001018401/14/16 Al-rich high-temperature tial alloy
382016001046201/14/16 Turbomachine blade
392016001048801/14/16 Wear protection arrangement for a turbomachine, process and compressor
402016000336001/07/16 Brush seal
412015037704212/31/15 Leiteinrichtung fur eine gasturbine sowie gasturbine mit einer solchen leiteinrichtung
422015037704912/31/15 Brush seal system for sealing a clearance between components of a turbo engine that are movable in relation to one another
432015037705312/31/15 Turbomachine
442015037706112/31/15 Unknown
452015037706812/31/15 Component arrangement for a gas turbine
462015036189312/17/15 Mid-frame for a gas turbine and gas turbine having such a mid-frame
472015033023711/19/15 Casing arrangement for a gas turbine
482015033040611/19/15 Mid-frame for a gas turbine and gas turbine
492015032280811/12/15 Seal, producing a seal and turbomachine
502015032331811/12/15 Device and generative production of at least one component area of a component
512015032451711/12/15 Unknown
522015031591911/05/15 Lightweight structural nial alloy with a high high-temperature strength
532015030850210/29/15 Bearing cage and bearing means having this type of bearing cage as well as designing, repairing and/or replacing such a bearing cage
542015030025910/22/15 Aircraft engine
552015029067110/15/15 Device for the generative production of a component
562015029071210/15/15 Method and device for improving material quality in generative manufacturing methods
572015028482410/08/15 Nickel-based alloy with optimized matrix properties
582015028507910/08/15 Gas turbine compressor
592015028508010/08/15 Unknown
602015027568310/01/15 Guide vane ring ,guide vane, inner ring and turbomachine
612015027668310/01/15 Method and device for ascertaining an edge layer characteristic of a component
622015026755409/24/15 Safety device for a bearing arrangement of a rotor of a turbomachine
632015026004609/17/15 Method for designing a turbine
642015025125009/10/15 Device and the generative production of a component
652015025219909/10/15 Anti-ice coating for compressor blades
662015025269109/10/15 Gas turbine duct casing
672015024641409/03/15 Apparatus and generative production of a component
682015024648109/03/15 Creation of residual compressive stresses during additve manufacturing
692015022615508/13/15 Thrust deflecting device and aircraft engine
702015021867508/06/15 High-temperature tial alloy
712015021944408/06/15 Method and determining residual stresses of a component
722015020423807/23/15 Low noise turbine for geared turbofan engine
732015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
742015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
752015019202607/09/15 Gas turbine
762015019202807/09/15 Gas turbine
772015016551606/18/15 Method for producing a cylindrical component
782015016554506/18/15 Irradiation in generative fabrication
792015016747706/18/15 Gas turbinen rotor blade
802015016747806/18/15 Blade cascade
812015016747906/18/15 Blade cascade
822015015955106/11/15 Gas turbine
832015015274206/04/15 Sealing element, sealing unit, and turbomachine
842015014722005/28/15 Material of laves phase and ferritic fe-al phase
852015013978605/21/15 Run-in coating based on metal fibers
862015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
872015013980805/21/15 Rotor of a turbomachine
882015013981105/21/15 Blade-disk assembly, method and turbomachine
892015012958305/14/15 Method for producing low-pressure turbine blades from tial
902015013211505/14/15 Unknown
912015013212305/14/15 Gas turbine
922015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
932015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
942015012527805/07/15 Seal configuration for a turbo machine
952015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
962015010256504/16/15 Unknown
972015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
982015009879904/09/15 Component support and turbomachine
992015009880904/09/15 Turbomachine
1002015009323504/02/15 Brush seal for a turbomachine
1012015009324904/02/15 Blade for a gas turbine
1022015009493104/02/15 Method for performing maintenance on an engine
1032015008428503/26/15 Brush seal and producing a brush seal
1042015008633103/26/15 Bauteilsystem einer turbomaschine
1052015008641403/26/15 Creep-resistant tial alloy
1062015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
1072015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
1082015007927803/19/15 Slip and process for producing an aluminum diffusion layer
1092015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
1102015006042203/05/15 Apparatus for laser materials processing
1112015006122803/05/15 Sealing arrangement in an axial turbomachine
1122015006398303/05/15 Turbomachine
1132015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
1142015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
1152015006435403/05/15 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
1162015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
1172015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
1182015004403802/12/15 Blade cascade and turbomachine
1192015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
1202015002694401/29/15 Method for repairing a receiving hook for guide vanes
1212015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
1222015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
1232015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
1242015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
1252015001695701/15/15 Ceramic component for a turbomachine
1262015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
1272015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
1282015001698401/15/15 Guide vane arragement and mounting a guide vane
1292015001698501/15/15 Gas turbine stage
1302015001698601/15/15 Gas turbine compressor stator vane assembly
1312015001701101/15/15 Blade for a gas turbomachine
1322015001705401/15/15 Control in generative production
1332015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
1342015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
1352015000181101/01/15 Dichteinrichtung und stromungsmaschine
1362015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
1372015000397601/01/15 Turbomachine, circulation structure and method
1382015000398801/01/15 Turbomachine rotor blade
1392014036637412/18/14 Method for closing cooling air bores
1402014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
1412014036066412/11/14 Method for coating components
1422014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
1432014035664412/04/14 Tial blade with surface modification
1442014034676811/27/14 Adapter and turbomachine
1452014034844911/27/14 Split inner ring
1462014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
1472014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
1482014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
1492014034865511/27/14 Balancing body for a continuous blade arrangement
1502014034866011/27/14 Blade cascade and continuous-flow machine
1512014034866111/27/14 Blade row, blade and turbomachine
1522014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
1532014032196910/30/14 Slide ring seal
1542014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
1552014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
1562014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
1572014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
1582014030184010/09/14 Guide vane arrangement
1592014030185210/09/14 Blade cascade for turbo machine
1602014030185310/09/14 Securing blade assortment
1612014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
1622014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
1632014029457010/02/14 Turbomachine
1642014025518309/11/14 Twist prevention for turbomachinery
1652014024683509/04/14 Component
1662014023955308/28/14 Multi-frequency induction heating of generatively produced components
1672014023955408/28/14 Process and device for producing a three-dimensional object
1682014022708008/14/14 Seal support of titanium aluminide for a turbomachine
1692014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
1702014020260107/24/14 Forged tial components, and producing same
1712014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1722014015926606/12/14 Method and device for the generative production of a component
1732014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1742014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1752014016160706/12/14 Turbomachine
1762014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1772014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1782014009495004/03/14 Method for the production of an abradable spray coating
1792014007603803/20/14 Checking a blade contour of a turbomachine
1802014006534303/06/14 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
1812014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1822014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1832014004453702/13/14 Gas turbine
1842014004454602/13/14 Bladed rotor for a turbomachine
1852014004454902/13/14 Ductile compensation layer for brittle components
1862014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1872014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1882014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1892014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1902013034394712/26/13 Method and device for process monitoring
1912013028759010/31/13 Generatively produced turbine blade and device and producing same
1922013028043910/24/13 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