MTU AERO ENGINES GMBH

Nickel-based solder alloy

#2 | 2013-10-10

US20130266427A1

SEALING SYSTEM FOR A TURBOMACHINE

#3 | 2013-07-25 ✅ Patent 9,500,088 granted on 2016-11-22

US20130189108A1

Blade rim segment for a turbomachine and method for manufacture

#4 | 2013-07-25 ✅ Patent 9,382,809 granted on 2016-07-05

US20130189086A1

Seal assembly, method and turbomachine

#5 | 2013-07-11 ✅ Patent 9,492,906 granted on 2016-11-15

US20130174869A1

Cleaning of a turbo-machine stage

#6 | 2013-02-28

US20130051996A1

TRANSITION CHANNEL OF A TURBINE UNIT

#7 | 2013-02-07 ✅ Patent 9,441,786 granted on 2016-09-13

US20130032215A1

Device and method for preserving fluid systems and an engine

#8 | 2012-11-29 ✅ Patent 9,057,274 granted on 2015-06-16

US20120301279A1

Housing system for an axial turbomachine

#9 | 2012-11-15

US20120288639A1

COMBINED HEATING FOR SOLDERING AN ARMOR CLADDING ONTO A TIP BY MEANS OF INDUCTION AND LASER

#10 | 2012-11-15 ✅ Patent 8,691,322 granted on 2014-04-08

US20120288616A1

Measurement method and device for measuring layer thicknesses as well as production method and coating system

#11 | 2012-11-08

US20120280021A1

METHOD FOR PRODUCING AN INTEGRALLY BLADED ROTOR USING ARCUATE FRICTION WELDING, DEVICE FOR CARRYING OUT SAID METHOD, AND ROTOR PRODUCED BY MEANS OF SAID METHOD

#12 | 2012-10-25

US20120269642A1

METHOD FOR FUSION WELDING A MONOCRYSTALLINE WORKPIECE TO A POLYCRYSTALLINE WORKPIECE AND ROTOR

#13 | 2012-09-13 ✅ Patent 8,622,704 granted on 2014-01-07

US20120230825A1

Gas turbine blade for a turbomachine

#14 | 2012-09-06

US20120224972A1

METHOD AND DEVICE FOR PRODUCING AN INTEGRALLY BLADED ROTOR AND ROTOR PRODUCED BY MEANS OF THE METHOD

#15 | 2012-09-06 ✅ Patent 9,045,989 granted on 2015-06-02

US20120224969A1

Coupling element for mechanically coupling blades and a rotor

#16 | 2012-08-30

US20120219726A1

METHOD AND DEVICE FOR PRODUCING A COMPONENT

#17 | 2012-08-30

US20120217226A1

METHOD AND DEVICE FOR PRODUCING A COMPONENT OF A TURBOMACHINE

#18 | 2012-08-09 ✅ Patent 9,132,508 granted on 2015-09-15

US20120201691A1

Method for producing a rotor or stator blade and such a blade

#19 | 2012-06-14 ✅ Patent 9,138,834 granted on 2015-09-22

US20120148413A1

Method for replacing a blade of a rotor having integrated blades and such a rotor

#20 | 2012-06-14

US20120144931A1

PRESSURE-MEASURING PROBE

#21 | 2012-05-24 ✅ Patent 9,011,081 granted on 2015-04-21

US20120128480A1

Blade

#22 | 2012-05-17 ✅ Patent 8,851,847 granted on 2014-10-07

US20120121437A1

Rotor for a turbo machine

#23 | 2012-05-17 ✅ Patent 9,022,727 granted on 2015-05-05

US20120121436A1

Rotor for a turbo machine

#24 | 2012-05-17 ✅ Patent 9,133,855 granted on 2015-09-15

US20120121435A1

Rotor for a turbo machine

#25 | 2012-05-17 ✅ Patent 9,260,784 granted on 2016-02-16

US20120121431A1

Blade tip coating that can be rubbed off

#26 | 2012-05-17 ✅ Patent 8,888,456 granted on 2014-11-18

US20120121384A1

Rotor and method for manufacturing a rotor for a turbo machine

#27 | 2012-05-03 ✅ Patent 8,801,906 granted on 2014-08-12

US20120103830A1

Device and method for electrochemically removing a surface of a component

#28 | 2012-05-03

US20120102701A1

METHOD FOR REDUCING VIBRATION AMPLITUDES

#29 | 2012-04-19 ✅ Patent 8,826,535 granted on 2014-09-09

US20120090175A1

Method for manufacturing an integrally bladed rotor

#30 | 2012-04-12 ✅ Patent 8,992,169 granted on 2015-03-31

US20120087781A1

Layer system for rotor/stator seal of a turbomachine and method for producing this type of layer system

#31 | 2012-03-15 ✅ Patent 8,678,742 granted on 2014-03-25

US20120063884A1

Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

#32 | 2012-03-08

US20120057988A1

ROTOR FOR A TURBOMACHINE

#33 | 2012-02-23 ✅ Patent 9,297,391 granted on 2016-03-29

US20120045313A1

Flow device comprising a cavity cooling system

#34 | 2012-02-09 ✅ Patent 9,021,696 granted on 2015-05-05

US20120034092A1

Method for producing a plating of a vane tip and correspondingly produced vanes and gas turbines

#35 | 2012-02-02 ✅ Patent 9,114,476 granted on 2015-08-25

US20120027603A1

Dual blisks in the high-pressure compressor

#36 | 2011-12-29 ✅ Patent 8,573,941 granted on 2013-11-05

US20110318172A1

Tandem blade design

#37 | 2011-12-01 ✅ Patent 8,356,741 granted on 2013-01-22

US20110290861A1

Method for producing a blade plating on a blade for a turbomachine

#38 | 2011-11-03 ✅ Patent 8,943,689 granted on 2015-02-03

US20110265328A1

Method for mounting an integral inner ring of a turbocompressor stator

#39 | 2011-09-29 ✅ Patent 8,346,383 granted on 2013-01-01

US20110238200A1

Method for determining the machining quality of components, particularly for metal cutting by NC machines

#40 | 2011-09-22 ✅ Patent 8,992,172 granted on 2015-03-31

US20110225979A1

Turbo engine

#41 | 2011-09-22 ✅ Patent 8,764,390 granted on 2014-07-01

US20110225822A1

Assembly mechanism comprising a tension anchor and corresponding method for a rotor system of an axial turbo engine

#42 | 2011-09-08

US20110217176A1

METHOD FOR CONNECTING AT LEAST ONE TURBINE BLADE TO A TURBINE DISK OR A TURBINE RING

#43 | 2011-09-01

US20110213569A1

METHOD AND DEVICE FOR DETECTING CRACKS IN COMPRESSOR BLADES

#44 | 2011-08-18 ✅ Patent 9,175,690 granted on 2015-11-03

US20110200470A1

Compressor

#45 | 2011-08-18 ✅ Patent 8,360,302 granted on 2013-01-29

US20110198390A1

Method for producing or repairing integrally bladed gas turbine rotors

#46 | 2011-06-16

US20110143039A1

PROCESS AND DEVICE FOR COLD SPRAYING

#47 | 2011-06-16

US20110142386A1

BEARING RING AND METHOD FOR COOLING A BEARING RING

#48 | 2011-06-16 ✅ Patent 8,601,881 granted on 2013-12-10

US20110138925A1

Material sample for testing biaxial stress conditions

#49 | 2011-06-09 ✅ Patent 8,036,769 granted on 2011-10-11

US20110137450A1

Method and device for compensating for positional and shape deviations

#50 | 2011-06-02 ✅ Patent 9,114,480 granted on 2015-08-25

US20110129353A1

Methods for joining a monocrystalline part to a polycrystalline part by means of an adapter piece made of polycrystalline material

#51 | 2011-02-24 ✅ Patent 9,951,411 granted on 2018-04-24

US20110045264A1

Erosion protection coating

#52 | 2011-01-20 ✅ Patent 8,697,184 granted on 2014-04-15

US20110014055A1

Gas dynamic cold spraying of oxide-containing protective layers

#53 | 2011-01-06 ✅ Patent 9,333,576 granted on 2016-05-10

US20110002789A1

Method for producing and repairing a part, and part of a gas turbine

#54 | 2010-12-23

US20100322780A1

SOLDER COATING, METHOD FOR COATING A COMPONENT, COMPONENT, AND ADHESIVE TAPE HAVING A SOLDER COATING

#55 | 2010-06-10

US20100143108A1

Device for the Protection of Components Having A Flammable Titanium Alloy From Titanium Fire, and Method for the Production Thereof

#56 | 2009-12-31 ✅ Patent 8,092,148 granted on 2012-01-10

US20090324384A1

Gas turbine having a peripheral ring segment including a recirculation channel

#57 | 2009-04-30 ✅ Patent 8,124,912 granted on 2012-02-28

US20090107968A1

Method for heating components

#58 | 2009-04-16 ✅ Patent 7,644,599 granted on 2010-01-12

US20090095042A1

Method for surface blasting cavities, particularly cavities in gas turbines

#59 | 2007-09-13 ✅ Patent 7,638,733 granted on 2009-12-29

US20070210044A1

Method for checking a bore hole

#60 | 2007-08-23 ✅ Patent 7,600,965 granted on 2009-10-13

US20070196204A1

Flow structure for a turbocompressor

#61 | 2007-08-09 ✅ Patent 7,416,393 granted on 2008-08-26

US20070181539A1

Apparatus and method for joining a rotor blade to a rotor mount of a gas turbine rotor

#62 | 2007-08-02

US20070177979A1

Vane comprising a transition zone

#63 | 2007-04-26

US20070090152A1

Method for cladding the blade tips of rotor blades of a gas turbine power plant and device for carrying out the method

#64 | 2007-01-25

US20070017607A1

Method for heating components

#65 | 2006-11-02 ✅ Patent 7,422,416 granted on 2008-09-09

US20060245917A1