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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



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