new TOP 200 Companies filing patents this week

new Companies with the Most Patent Filings (2010+)


Popular
Companies


Web
Adobe patents
Amazon patents
Apple patents
Ebay patents
Facebook patents
Google patents
IBM patents
Linkedin patents
Microsoft patents
Oracle patents
Red Hat patents
Yahoo patents

Food/Health
Adidas
Nike patents
Pfizer patents
Monsanto patents
Medtronic patents
Kraft patents

Transportation
Boeing patents
Tesla Motors patents

Telecom
Qualcomm patents
Motorola patents
Nokia patents
RIMM patents

Industrial/Electronics
AMD
Applied Materials
Seagate patents
General Electric
Caterpillar patents
Samsung
Wal-mart patents

  

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


Brush seal having brush filaments of nonmetallic materials

Mtu Aero Engines Ag

Brush seal having brush filaments of nonmetallic materials

Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine

Mtu Aero Engines Ag

Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine

Gas turbine

Mtu Aero Engines Ag

Gas turbine



Search recent Press Releases: Mtu Aero Engines Ag-related press releases
Count Application # Date Mtu Aero Engines Ag patents (updated weekly) - BOOKMARK this page
12015020423807/23/15  new patent  Low noise turbine for geared turbofan engine
22015019825107/16/15 Brush seal having brush filaments of nonmetallic materials
32015019202507/09/15 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine
42015019202607/09/15 Gas turbine
52015019202807/09/15 Gas turbine
62015016551606/18/15 Method for producing a cylindrical component
72015016554506/18/15 Irradiation in generative fabrication
82015016747706/18/15 Gas turbinen rotor blade
92015016747806/18/15 Blade cascade
102015016747906/18/15 Blade cascade
112015015955106/11/15 Gas turbine
122015015274206/04/15 Sealing element, sealing unit, and turbomachine
132015014722005/28/15 Material of laves phase and ferritic fe-al phase
142015013978605/21/15 Run-in coating based on metal fibers
152015013978905/21/15 Array of flow-directing elements for a gas turbine compressor
162015013980805/21/15 Rotor of a turbomachine
172015013981105/21/15 Blade-disk assembly, method and turbomachine
182015012958305/14/15 Method for producing low-pressure turbine blades from tial
192015013211505/14/15 Unknown
202015013212305/14/15 Gas turbine
212015013212405/14/15 Inner ring of a fluid flow machine and stator vane array
222015013213605/14/15 Rotor having a basic rotor body and a plurality of rotating blades mounted thereon
232015012527805/07/15 Seal configuration for a turbo machine
242015011484404/30/15 Identifying and regulating the starting behavior during electrochemical machining of workpieces
252015010256504/16/15 Unknown
262015009879804/09/15 Brush seal system for sealing a gap between components of a thermal gas turbine that may be moved relative to one another
272015009879904/09/15 Component support and turbomachine
282015009880904/09/15 Turbomachine
292015009323504/02/15 Brush seal for a turbomachine
302015009324904/02/15 Blade for a gas turbine
312015009493104/02/15 Method for performing maintenance on an engine
322015008428503/26/15 Brush seal and producing a brush seal
332015008633103/26/15 Bauteilsystem einer turbomaschine
342015008641403/26/15 Creep-resistant tial alloy
352015007532703/19/15 Wear-resistant coating produced by electrodeposition and process therefor
362015007889303/19/15 Seal arrangement for a turbomachine and process for the production thereof
372015007927803/19/15 Slip and process for producing an aluminum diffusion layer
382015007176903/12/15 Method for disassembly and assembly of a rotor of a gas turbine
392015006042203/05/15 Apparatus for laser materials processing
402015006122803/05/15 Sealing arrangement in an axial turbomachine
412015006398303/05/15 Turbomachine
422015006398603/05/15 Apparatus for energy absorption, a turbo-machine and a energy absorption
432015006405003/05/15 Multiple coil arrangement for a device for generative production of components and corresponding production method
442015006435403/05/15 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
452015006443003/05/15 Heat insulation layer system with corrosion and erosion protection
462015005051102/19/15 Intermetallic wear-resistant layer for titanium materials
472015004403802/12/15 Blade cascade and turbomachine
482015003716102/05/15 Method for mounting a gas turbine blade in an associated receiving recess of a rotor base body
492015002694401/29/15 Method for repairing a receiving hook for guide vanes
502015002790401/29/15 Multipart electrode array and the electrochemical treatment of blades having shrouding bands
512015003043401/29/15 Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine
522015002119901/22/15 Optical measurement system for determining the position of an electrode during the electrochemical processing of a component
532015001417901/15/15 Cmas-inert thermal barrier layer and producing the same
542015001695701/15/15 Ceramic component for a turbomachine
552015001696901/15/15 Turbomachine, sealing segment, and guide vane segment
562015001697401/15/15 Method of producing an insulation element and insulation element for a housing of an aero engine
572015001698401/15/15 Guide vane arragement and mounting a guide vane
582015001698501/15/15 Gas turbine stage
592015001698601/15/15 Gas turbine compressor stator vane assembly
602015001701101/15/15 Blade for a gas turbomachine
612015001705401/15/15 Control in generative production
622015001773601/15/15 Method for the non-destructive testing of workpiece surfaces
632015001039601/08/15 Blade row poisitioning device, blade-device combination, method and turbomachine
642015000181101/01/15 Dichteinrichtung und stromungsmaschine
652015000397001/01/15 Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement
662015000397601/01/15 Turbomachine, circulation structure and method
672015000398801/01/15 Turbomachine rotor blade
682014036637412/18/14 Method for closing cooling air bores
692014036982212/18/14 Method for producing forged components from a tial alloy and component produced thereby
702014036066412/11/14 Method for coating components
712014035618312/04/14 Rhenium-free or rhenium-reduced nickel-base superalloy
722014035664412/04/14 Tial blade with surface modification
732014034676811/27/14 Adapter and turbomachine
742014034844911/27/14 Split inner ring
752014034863111/27/14 Turbomachine stage and determining a seal gap and/or an axial position of such a turbomachine stage
762014034863211/27/14 Turbomachine stage and detecting a sealing gap of such a turbomachine stage
772014034863311/27/14 Turbine stage with a blow-out arrangement and blowing out a sealing gas flow
782014034865511/27/14 Balancing body for a continuous blade arrangement
792014034866011/27/14 Blade cascade and continuous-flow machine
802014034866111/27/14 Blade row, blade and turbomachine
812014033492411/13/14 Method and device for the generative production of a component using a laser beam and corresponding turbo-engine component
822014032196910/30/14 Slide ring seal
832014032199810/30/14 Housing section of a turbine engine compressor stage or turbine engine turbine stage
842014032255510/30/14 Process for producing a high-temperature protective coating and correspondingly produced component
852014030811710/16/14 Armoring sealing fins of tial vanes by induction brazing hard-material particles
862014029877210/09/14 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
872014030184010/09/14 Guide vane arrangement
882014030185210/09/14 Blade cascade for turbo machine
892014030185310/09/14 Securing blade assortment
902014030185410/09/14 Securement securing an attachment portion of at least one rotor blade or rotor blade segment in a mounting site of a rotor base
912014030186010/09/14 Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
922014029457010/02/14 Turbomachine
932014025518309/11/14 Twist prevention for turbomachinery
942014024683509/04/14 Component
952014023955308/28/14 Multi-frequency induction heating of generatively produced components
962014023955408/28/14 Process and device for producing a three-dimensional object
972014022708008/14/14 Seal support of titanium aluminide for a turbomachine
982014022710208/14/14 Rotor blade for a compressor of a turbomachine, compressor, and turbomachine
992014020260107/24/14 Forged tial components, and producing same
1002014017820106/26/14 Turbine blade having a shroud and a cutting tooth
1012014015926606/12/14 Method and device for the generative production of a component
1022014016159006/12/14 Cover device, integrally bladed main rotor body, method and turbomachine
1032014016160106/12/14 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
1042014016160706/12/14 Turbomachine
1052014016162406/12/14 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane
1062014011994105/01/14 Creep-resistant, rhenium-free nickel base superalloy
1072014009495004/03/14 Method for the production of an abradable spray coating
1082014007603803/20/14 Checking a blade contour of a turbomachine
1092014006534303/06/14 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
1102014004452602/13/14 Stationary blade ring, assembly method and turbomachine
1112014004453202/13/14 Process for producing a tial guide vane ring for a gas turbine and a corresponding guide vane ring
1122014004453702/13/14 Gas turbine
1132014004454602/13/14 Bladed rotor for a turbomachine
1142014004454902/13/14 Ductile compensation layer for brittle components
1152014004455002/13/14 Restraint mechanism for rotor blades of a turbo engine, an assembly method and a turbo engine
1162014004455102/13/14 Blade cascade with side wall contours and continuous-flow machine
1172014004493802/13/14 Process for producing a component-matched protective layer and component having such a protective layer
1182014004498602/13/14 Duplex-phase cral coating for improved corrosion/oxidation protection
1192013034394712/26/13 Method and device for process monitoring
1202013028759010/31/13 Generatively produced turbine blade and device and producing same
1212013028043910/24/13 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. Freshpatents.com 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 FreshPatents.com

###

     SHARE