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MTU Aero Engines AG Patents
What MTU Aero Engines AG has filed at the patent office — applications as well as grants, because a filing is on the record eighteen months before anyone has to say what it was for.
MTUAY on carbonthat →Filings on file
52
Granted
13
Still pending
39
Filed under
2 names
52 filings
Newest filing first. A pending application has no patent number yet, and most never get one.
| Invention | Patent |
|---|---|
| CONTROL DEVICE FOR A FUEL CELL SYSTEMH01M 8/04753, B60L 50/70, B60L2200/10, H01M 8/04395, H01M 8/04507, H01M 8/04835, H01M2250/20Filed as MTU Aero Engines AG2026-07-28Sebastian Nicolay | pending |
| TURBOMACHINE HAVING A FLOW DUCTFiled as MTU Aero Engines AG2026-06-02Harsimar SAHOTA | pending |
| VANE ACTUATING DEVICE FOR A GAS TURBINE, TURBOMACHINE HAVING THE VANE ACTUATING DEVICE, AND RELATED METHODF01D 17/12, F01D 17/162, F05D2250/11, F05D2250/13, F05D2250/22, F05D2250/23, F05D2260/36, F05D2260/37, F05D2260/38, F05D2260/50Filed as MTU Aero Engines AG2026-05-29Florian NEUBERGER | pending |
| TURBOMACHINE HAVING A FLOW DUCTF01D 5/141, F01D 9/041, F01D 9/023, F01D 9/065, F01D 25/162, F02C 3/06, F02C 7/04, F02C 7/36, F02C 9/18, F04D 19/028, F04D 29/324, F04D 29/444, F04D 29/541, F04D 29/544, F04D 29/547, F05D2240/301Filed as MTU Aero Engines AG2026-03-04Harsimar SAHOTA | pending |
| MODULE FOR A TURBOMACHINEF01D 11/001, F01D 11/02, F05D2240/55, F05D2250/232, F05D2250/292, F05D2260/31Filed as MTU Aero Engines AG2026-02-17Christoph Lauer | pending |
| METHOD AND REPAIR KIT FOR RESTORING A MOUNTING ASSEMBLY, REPAIR KIT, REPAIRED MOUNTING ASSEMBLY, AND AIRCRAFT ENGINEB23P 6/00, B23P 6/002, B23G 9/009, B23P 6/045, F16B 31/021, F16B 37/145Filed as MTU Aero Engines AG2026-01-14Joerg SCHNITZLER | pending |
| Turbine or compressor stage assemblyF01D 5/225, F01D 25/06, F01D 5/10, F01D 9/042, F01D 25/04, F05D2220/323, F05D2240/11, F05D2250/231, F05D2250/241, F05D2250/711, F05D2260/96Filed as MTU Aero Engines AG2025-12-17Andreas HARTUNG | pending |
| DRIVE SYSTEM FOR AN AIRCRAFTB64D 35/021, B64D 27/355, B64D 27/34, B64D 27/31, B64D 31/16, B64D 31/10, H02P 5/50, Y02T 90/40Filed as MTU Aero Engines AG2025-11-10Barnaby LAW | pending |
| LOW NOISE TURBINE FOR GAS TURBINE ENGINEF02C 3/107, F02C 7/36, G06F 30/17, F01D 5/06, F01D 5/14, F01D 15/12, F01D 25/24, F02C 3/04, F02K 3/04, F02K 3/06, F04D 25/045, F04D 29/053, F04D 29/321, F04D 29/325, F05D2220/323, F05D2230/50, F05D2260/40311, F05D2260/96, F05D2270/304, F05D2270/333, Y02T 50/60Filed as MTU AERO ENGINES AG2025-11-07Bruce L. Morin | pending |
| FUEL SYSTEM FOR SUPPLYING AN AIRCRAFT WITH HYDROGEN, METHOD AND AIRCRAFTB64D 37/30, F17C 7/02, B64D 37/005, B64D 37/06, B64D 37/20, B64D 37/32, B64D 45/00, B64D2041/005, B64D2045/0085, F17C 1/12, F17C2201/0109, F17C2201/054, F17C2201/056, F17C2203/015, F17C2203/032, F17C2203/0329, F17C2203/0391, F17C2203/0631, F17C2205/0111, F17C2205/013, F17C2205/0134, F17C2205/0149, F17C2205/0326, F17C2205/0332, F17C2221/012, F17C2223/0161, F17C2223/033, F17C2227/0388, F17C2250/0443, F17C2260/012, F17C2260/018, F17C2265/066, F17C2270/0189Filed as MTU Aero Engines AG2025-10-15Anja MAROSKY | pending |
| Ejector jet pumpF04F 5/24, H01M 8/04164, F04F 5/44, F04F 5/54, H01M 8/04097, H01M 8/04119, H01M2250/20, Y02E 60/50Filed as MTU Aero Engines AG2025-10-06Gionata LUISONI | pending |
| STATOR VANE SEGMENTF01D 5/225, F01D 9/041, F04D 29/542, F05D2220/323, F05D2240/12, F05D2240/80, F05D2250/75Filed as MTU Aero Engines AG2025-09-03Dennis VON BRAUNECK | pending |
| Sealing device, turbomachine, and useF01D 11/003, F16J 15/3288, F01D 5/025, F01D 11/005, F05D2220/323, F05D2240/56Filed as MTU Aero Engines AG2025-08-21Matthias SIEBEL | pending |
| TURBINE MODULE FOR A TURBOMACHINEF01D 5/145, F01D 9/041, F01D 9/042, F05D2240/12, F05D2240/121, F05D2240/80, F05D2240/81, F05D2260/606Filed as MTU Aero Engines AG2025-07-21Michal Piatek | 12624639 |
| PANEL SEGMENT FOR A COOLING PANELF01D 25/12, F01D 25/14, F01D 11/24, F05D2230/232, F05D2230/237, F05D2230/51, F05D2230/54, F05D2240/40, F05D2260/201, F23R 3/002Filed as MTU Aero Engines AG2025-07-18Krzysztof MARZEC | pending |
| DEVICE AND METHOD FOR ELECTROCHEMICAL MACHININGB23H 3/00, B23H 7/28, B23H 9/10Filed as MTU Aero Engines AG2025-06-12Kilian Bayer | pending |
| BLADE ARRANGEMENT OF A THERMAL TURBOMACHINE THROUGH WHICH AXIAL FLOW MAY PASS, AND THERMAL TURBOMACHINE THROUGH WHICH AXIAL FLOW MAY PASSF01D 9/042, F01D 25/246, B33Y 10/00, B33Y 80/00, B22F 10/28, B22F 5/04, F01D 5/10, F01D 9/041, F01D 25/04, F01D 25/06, F05D2230/22, F05D2230/234, F05D2230/30, F05D2230/31, F05D2230/54, F05D2240/12, F05D2250/15, F05D2250/183, F05D2250/184, F05D2250/241, F05D2250/25, F05D2250/75, F05D2260/96Filed as MTU Aero Engines AG2025-06-06Dennis VON BRAUNECK | pending |
| GUIDE VANE ELEMENT FOR A COMPRESSOR OF A TURBOMACHINE, GUIDE VANE CLUSTER AND TURBOMACHINEF01D 5/143, F05D2220/323, F05D2240/24Filed as MTU Aero Engines AG2025-06-04Dennis Von Brauneck | pending |
| PLAIN BEARING ARRANGEMENT FOR AN AIRCRAFT ENGINE AND AIRCRAFT ENGINE HAVING A PLAIN BEARING ARRANGEMENTF01D 25/166, F16C 33/043, C23C 14/0605, F01D 17/16, F01D 17/162, F05D2220/323, F05D2260/56, F05D2260/79, F05D2300/224, F05D2300/509, F05D2300/611, F16C 17/18, F16C2206/04, F16C2223/60, F16C2240/64, F16C2326/43, F16C2360/24Filed as MTU Aero Engines AG2025-05-14Joachim FALLER | pending |
| SEALING ARRANGEMENT FOR A TURBOMACHINE, SEAL CARRIER ELEMENT FOR THE SEALING ARRANGEMENT, GUIDE BLADE ELEMENT, AND TURBOMACHINEF01D 11/003, F01D 9/04, F01D 11/001, F01D 25/246, F05D2220/323, F05D2230/64, F05D2240/59, F05D2260/36, F05D2300/611Filed as MTU Aero Engines AG2025-05-07Oskar OSTERMEIR | 12584417 |
| POWER SUPPLY SYSTEM FOR A PROPULSION SYSTEM OF AN AIRCRAFTH01M 8/04029, H01M 8/04268, B64D 35/021, B64D 27/026, B64D2041/005, H01M 8/0267, H01M 8/04074, H01M 8/04701, H01M 8/248, H01M2008/1095, H01M2250/20, Y02T 90/40Filed as MTU Aero Engines AG2025-04-30Stephan LELLEK | pending |
| AIRCRAFT HAVING A FUEL-CELL PROPULSION SYSTEMB64C 29/04, H01M 8/04067, B60L 50/71, B64D 27/34, B64D 27/355, B64C 1/00, B64D 33/08, B64D 33/10, B64D 37/04, B64D 37/30, H01M 8/04014, H01M 8/04029, H01M 8/04201, H01M2250/20, Y02T 90/40Filed as MTU Aero Engines AG2025-04-11Thomas Scherer | pending |
| TURBOMACHINE FOR A FLIGHT PROPULSION DRIVEF01D 25/30, F05D2240/12, F05D2250/232, F05D2250/27, F05D2250/712, F05D2250/72, F05D2260/213Filed as MTU Aero Engines AG2025-04-03Simon Schuldt | pending |
| CLAMPING COMPOSITE ASSEMBLYF01D 5/066, F01D 5/025, F01D 25/243, F05D2260/30, F05D2260/31, F05D2260/33, F05D2260/36Filed as MTU Aero Engines AG2025-02-20Hermann Nachtigall | 12553347 |
| AIRCRAFT FUEL CELL PROPULSION UNITH01M 8/04029, H01M 8/04164, B60L 50/70, B64D 27/355, B60L2200/10, B64D 33/10, H01M 8/04156, H01M 8/04768, H01M2250/20, Y02E 60/50, Y02T 90/40Filed as MTU Aero Engines AG2025-02-19Stephan Lellek | pending |
| MEASUREMENT OF A RADIAL GAP IN A GAS TURBINE ASSEMBLYF01D 21/003, F05D2270/8041, G01B 11/14, F01D 25/285, G01B 11/2518Filed as MTU Aero Engines AG2025-02-17Dr. Juergen Gruendmayer | pending |
| Guide Vane SegmentF01D 5/225, F01D 9/042, F01D 9/041, F01D 11/08, F01D 25/246, F04D 29/542, F05D2240/11, F05D2240/80, F05D2260/36, F05D2260/941Filed as MTU Aero Engines AG2025-02-12Dennis VON BRAUNECK | pending |
| TURBOMACHINE HAVING A FLOW DUCTF04D 29/547, F04D 29/542Filed as MTU Aero Engines AG2025-02-07Harsimar SAHOTA | 12435735 |
| GAS TURBINE STRUCTURAL COMPONENTF01D 25/162, F01D 25/24, F01D 25/243, F01D 25/28, F05D2220/32, F05D2220/323, F05D2230/232, F05D2230/60, F05D2250/13Filed as MTU Aero Engines AG2025-01-29Magnus MECHLER | pending |
| METHOD FOR MONITORING A TURBOMACHINEG01M 15/14, G01H 13/00Filed as MTU Aero Engines AG2025-01-29Georg Schoenberger | pending |
| TURBOFAN ENGINE HAVING A LOW-PRESSURE TURBINEF01D 5/12, F02K 3/06, F01D 5/141, F01D 9/041, F01D 15/12, F05D2220/31, F05D2220/3215, F05D2220/36, F05D2240/122, F05D2240/304, Y02T 50/60Filed as MTU Aero Engines AG2025-01-20Markus BRETTSCHNEIDER | 12735987 |
| FUEL CELL STACKB64D 27/355, H01M 8/248, H01M 8/2465, H01M 8/2475, H01M2250/20, Y02E 60/50Filed as MTU Aero Engines AG2025-01-06Ann-Kathrin Henss | pending |
| HEAT EXCHANGER FOR A HIGH INFLOW VELOCITYF28F 1/02, F28F 9/0265, F28F 13/08, F28F2250/06, F28D2021/0021, F28D2021/0026, F28F2250/02Filed as MTU Aero Engines AG2024-12-06Hermann Klingels | pending |
| VANE ACTUATING ARM FOR A GAS TURBINE, TURBOMACHINE HAVING THE VANE ACTUATING ARM, AND METHOD FOR MOUNTING A VANE ACTUATING ARM FOR A TURBOMACHINEF01D 17/12, F01D 17/162, F05D2250/11, F05D2250/13, F05D2250/22, F05D2250/23, F05D2260/36, F05D2260/37, F05D2260/38, F05D2260/50Filed as MTU Aero Engines AG2024-11-25Florian NEUBERGER | pending |
| Guide vane, guide vane cluster, and housing for a gas turbine as well as gas turbine having a platform with an arched wall section to receive a damperF01D 9/041, F01D 25/246, F01D 25/04, F01D 25/06, F01D 25/24, F05D2220/323, F05D2230/54, F05D2240/125, F05D2240/80, F05D2250/191, F05D2250/711, F05D2250/75, Y02T 50/60Filed as MTU Aero Engines AG2024-10-14Markus Schlemmer | 12692794 |
| INNER RING SEGMENT, AXIALLY DIVIDED INNER RING AND VARIABLE VANE CASCADE FOR AN AIRCRAFT ENGINEF01D 17/14, F01D 17/162, F01D 5/143, F01D 9/041, F01D 11/001, F01D 17/16, F05D2220/323, F05D2230/51, F05D2230/64, F05D2240/80, F05D2260/961Filed as MTU Aero Engines AG2024-09-13Werner Humhauser | 12497907 |
| LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINEF02C 3/107, F02C 7/36, G06F 30/17, F01D 5/06, F01D 5/14, F01D 15/12, F01D 25/24, F02C 3/04, F02K 3/04, F02K 3/06, F04D 25/045, F04D 29/053, F04D 29/321, F04D 29/325, F05D2220/323, F05D2230/50, F05D2260/40311, F05D2260/96, F05D2270/304, F05D2270/333, Y02T 50/60Filed as MTU AERO ENGINES AG2024-09-12Bruce L. Morin | 12492664 |
| METHOD FOR IMAGING A SURFACE OF A TURBOMACHINE AND DETECTING DAMAGEG06T 3/4038, G06T 7/0004, G06T2207/20084, G06T2207/30164Filed as MTU Aero Engines AG2024-09-12Maximilian Buchstab | pending |
| BLADING ASSEMBLY FOR A TURBOMACHINE AND TURBOMACHINEF01D 5/141, F01D 5/143, B23P 15/02, F01D 5/145, F01D 9/041, F05D2230/10, F05D2230/30, F05D2240/121, F05D2240/122, F05D2240/303, F05D2240/304, F05D2240/80, Y02T 50/60Filed as MTU Aero Engines AG2024-09-12Roland WUNDERER | 12460548 |
| STATOR VANE ASSEMBLY OF A TURBOMACHINE AND METHOD FOR ASSEMBLING A STATOR VANE ASSEMBLYF01D 17/12, F01D 17/162, F05D2220/32, F05D2230/60, F05D2230/64, F05D2240/12, F05D2240/54, F05D2260/36, F05D2260/37, F05D2260/38Filed as MTU Aero Engines AG2024-08-07Alexander RAUSCHMEIER | 12618334 |
| AIR CONDUCTION SYSTEMF02C 7/18Filed as MTU Aero Engines AG2024-08-01Nils Busch | 12435670 |
| MODULE FOR A TURBOMACHINEF01D 11/001, F01D 11/02, F05D2240/55, F05D2250/232, F05D2250/292, F05D2260/31Filed as MTU Aero Engines AG2024-06-07Christoph Lauer | 12607130 |
| ROTOR SHAFT FOR AN ELECTRIC MOTOR, ASSEMBLY FOR A ROTOR SHAFT, AND METHOD FOR MANUFACTURING AN ASSEMBLY FOR A ROTOR SHAFTH02K 1/32, H02K 9/19, B33Y 80/00, B64D 33/08, H02K 1/30, H02K 7/003Filed as MTU Aero Engines AG2024-05-03Martin Schloffer | pending |
| FUEL CELL FOR A FUEL CELL STACKH01M 8/2418, H01M 8/0267, B64D 27/355, B64D 33/08, H01M 8/0258, H01M 8/0271, H01M 8/1004, H01M 8/241, H01M 8/249, H01M2220/20, H01M2250/20, Y02E 60/50Filed as MTU Aero Engines AG2024-05-02Ann-Kathrin Henss | pending |
| ROTOR DISK FOR A BLADE RINGF01D 5/3023, F01D 5/021, F05D2300/17Filed as MTU Aero Engines AG2024-04-29Matthias SIEBEL | pending |
| METHOD FOR RECOGNIZING AN ANOMALY IN MEASURED OPERATING VALUES OF A TURBOMACHINE, AND ANALYSIS DEVICE AND MACHINE MONITORING DEVICEF01D 19/00, F01D 21/003, F05D2260/80, F05D2270/80, G05B 23/0254Filed as MTU Aero Engines AG2024-04-24Duilio Becchio | pending |
| ELASTICALLY CENTERED SYNCHRONIZATION DEVICEF01D 17/162, F01D 25/16, F04D 29/462, F04D 29/563, F05D2240/54, F05D2250/14, F05D2260/50, F05D2260/70, F05D2260/79Filed as MTU Aero Engines AG2024-04-24Alexander BOECK | pending |
| DRIVE SYSTEM, AND AIRCRAFT INCLUDING A DRIVE SYSTEMF02C 3/34, F02C 6/18, F02C 3/305, F02C 7/141, F02C 7/16, F02C 7/32, F05D2220/72, F05D2220/76, F05D2260/213Filed as MTU Aero Engines AG2024-04-18Istvan BOLGAR | pending |
| METHOD FOR ELECTROCHEMICALLY MACHINING A WORKPIECEB23H 3/10, B01D 61/18, B01D 63/082, B01D 63/087, B01D 63/16, B01D2315/02, B23H 9/10Filed as MTU Aero Engines AG2024-04-10Nicole Feiling | pending |
| DAMPER RING FOR REDUCING UNWANTED VIBRATIONS OF A BLISK, AS WELL AS BLISK AND TURBOMACHINEF01D 5/10, F05D2250/221, F05D2250/241, F05D2260/96Filed as MTU Aero Engines AG2024-03-27Andreas HARTUNG | pending |
| METHOD FOR OPERATING A COMBUSTION SYSTEM OF A TURBOMACHINE FOR A FLIGHT PROPULSION SYSTEM, AND TURBOMACHINEF02C 3/30, F05D2220/323, F05D2260/213, F05D2270/08, F23R 3/286, F23R 3/30, F23R 3/32Filed as MTU Aero Engines AG2024-03-26Dr. Oliver Schmitz | pending |
| ROTOR ARRANGEMENT FOR A LOW-PRESSURE TURBINE OF A TURBOMACHINEF01D 5/025, F01D 5/026, F01D 5/048, F01D 5/066, F01D 5/082, F01D 25/162, F05D2220/323, F05D2240/54, F05D2260/941, Y02T 50/60Filed as MTU Aero Engines AG2024-03-25Ilse Fleischer | 12669057 |
Filings are matched to the company by applicant name, so a subsidiary filing under its own name is only here if that name resolves to this company. The applicant is printed as filed, which makes a wrong match visible. A patent is not a product: most applications are never granted, and most grants are never built.