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MTU AERO ENGINES GMBH

Overview
  • Total Patents
    2,600
  • GoodIP Patent Rank
    186,216
About

MTU AERO ENGINES GMBH has a total of 2,600 patent applications. Its first patent ever was published in 1991. It filed its patents most often in Germany, WIPO (World Intellectual Property Organization) and EPO (European Patent Office). Its main competitors in its focus markets engines, pumps and turbines, machine tools and machines are BUNKER RONALD SCOTT, VOL VO AEHRO CORP and MEIER REINHOLD.

Patent filings per year

Chart showing MTU AERO ENGINES GMBHs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Bayer Erwin 291
#2 Meier Reinhold 148
#3 Jakimov Andreas 121
#4 Uihlein Thomas 120
#5 Hertter Manuel 100
#6 Steinwandel Juergen 99
#7 Bamberg Joachim 92
#8 Platz Albin 90
#9 Eichmann Wolfgang 88
#10 Schneiderbanger Stefan 76

Latest patents

Publication Filing date Title
DE102015224375A1 Method of testing a blade unit
DE102015217166A1 Method for determining at least one surface property
DE102014218639A1 Apparatus and method for generatively constructing a workpiece assembly
DE102013225989A1 Heat exchanger for a gas turbine engine
DE102013214228A1 Optical measuring system for determining the position of an electrode during the electrochemical machining of components
EP2806110A1 Turbo engine stage and method for determining a seal gap of such a turbo engine stage
EP2789802A1 Blade row for a turbomachine and corresponding manufacturing method
EP2784333A1 Device for the positioning and clamping of two concentric elements that partially overlap each other
EP2834387A1 Slurry and method for producing an aluminum diffusion layer
EP2834392A1 Cr (vi)-free anti-corrosion layers or adhesive layers which contain a solution comprising phosphate ions and metal powder, the metal powder being at least partially coated with si or si alloys
US2014241893A1 System for specifying an installation position of rotor blades, securing element, rotor blade, turbomachine, and method
US2014147286A1 Turbomachine rotor disk
US2013136621A1 Blading
EP2719867A1 Housing structure with improved sealing and cooling
WO2013029584A1 Method for manufacturing, repairing and/or exchanging a rotor/stator combination system, and a rotor/stator combination system manufactured in accordance wih the method
EP2695704A1 Method for manufacturing a TIAL blade ring segment for a gas turbine and corresponding blade ring segment
EP2696042A1 Fluid flow engine with at least one guide blade assembly
DE102012201052A1 Multi-part electrode assembly and method of electrochemically machining vanes with shrouds
EP2620517A1 Heat-resistant TiAl alloy
DE102012200891A1 System for specifying a mounting position of blades, securing element, blade, turbomachine and method