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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



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