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Inventor profile of:

Thomas Uihlein

City:

Dachau

Country:

Germany

Published Applications:

31

Last publication date:

2019-10-03

Top Assignees for applications by Thomas Uihlein

The entities that hold a legal rights for patent applications filed by inventor Uihlein Thomas:

MTU Aero Engines GmbH 16 Munich, Germany
MTU AERO ENGINES GMBH 6 Munchen, Germany
MTU AERO ENGINES AG 5 Munich, Germany
MTU Aero Engines GmbH 4 Muenchen, Germany
MTU Areo Engines GmbH 1 Munich, Germany
MTU Aero Engines GmbH 1 , Germany
AB Solut Chemie GmbH 1 Rheinbreitbach, Germany

Recent patent applications by Uihlein Thomas

Thomas Uihlein from Dachau, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2019-10-03

US20190301291A9

Mechanical engineering

Masking method for producing a combination of blade tip hardfacing and erosion-protection coating

#2 | 2017-11-23

US20170335697A1

Mechanical engineering

Method of producing blades or blade arrangements of a turbomachine with erosion protection layers and correspondingly produced component

#3 | 2016-11-17

US20160333706A1

Mechanical engineering

MASKING METHOD FOR PRODUCING A COMBINATION OF BLADE TIP HARDFACING AND EROSION-PROTECTION COATING

#4 | 2016-11-17

US20160333705A1

Mechanical engineering

COMBINATION OF BLADE TIP CLADDING AND EROSION-RESISTANT LAYER AND METHOD FOR THE PRODUCTION THEREOF

#5 | 2016-09-08

US20160258046A1

Chemistry; metallurgy

Device and method for partially masking a component zone of a component

#6 | 2013-10-24

US20130280480A1

Performing operations; transporting

Anti-wear coating

#7 | 2013-07-11

US20130174869A1

Performing operations; transporting

Cleaning of a turbo-machine stage

#8 | 2012-06-07

US20120141822A1

Chemistry; metallurgy

Anti-wear coating and component comprising an anti-wear coating

#9 | 2011-12-08

US20110299996A1

Mechanical engineering

ANTI-EROSION COATING SYSTEM FOR GAS TURBINE COMPONENTS

#10 | 2011-12-01

US20110290861A1

Performing operations; transporting

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

#11 | 2011-10-20

US20110255981A1

Performing operations; transporting

Method for the production of an integrally bladed rotor, and rotor

#12 | 2011-09-08

US20110217176A1

Performing operations; transporting

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

#13 | 2011-06-02

US20110129353A1

Performing operations; transporting

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

#14 | 2011-02-24

US20110045264A1

Chemistry; metallurgy

Erosion protection coating

#15 | 2011-01-27

US20110020548A1

Mechanical engineering

DEVICE AND METHOD FOR THE PARTIAL COATING OF COMPONENTS

#16 | 2010-11-11

US20100284817A1

Mechanical engineering

METHOD FOR PRODUCING A BLISK OR A BLING, COMPONENT PRODUCED THEREWITH AND TURBINE BLADE

#17 | 2010-10-21

US20100263694A1

Chemistry; metallurgy

DECOATING DEVICE FOR AXIALLY SYMMETRIC COMPONENTS, PARTICULARLY FROM AIRCRAFT ENGINES

#18 | 2010-09-23

US20100239429A1

Chemistry; metallurgy

WEAR PROTECTION COATING

#19 | 2010-09-09

US20100226782A1

Mechanical engineering

Turbomachine blade with a blade tip armor cladding

#20 | 2010-06-10

US20100143110A1

Chemistry; metallurgy

VANE FOR A COMPRESSOR OR A TURBINE OF AN AIRCRAFT ENGINE, AIRCRAFT ENGINE COMPRISING SUCH A VANE AND A METHOD FOR COATING A VANE OF AN AIRCRAFT ENGINE

#21 | 2010-06-10

US20100143108A1

Chemistry; metallurgy

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

#22 | 2010-05-13

US20100119376A1

Mechanical engineering

INLET CONE FOR JET ENGINE

#23 | 2010-05-06

US20100108538A1

Chemistry; metallurgy

METHOD FOR STRIPPING A COMPONENT

#24 | 2010-03-18

US20100064515A1

Performing operations; transporting

METHOD FOR REPAIRING AND/OR REPLACING INDIVIDUAL ELEMENTS OF A GAS TURBINE COMPONENT

#25 | 2009-12-10

US20090302004A1

Mechanical engineering

Method for removing the coating from a gas turbine component

#26 | 2009-12-03

US20090297876A1

Chemistry; metallurgy

Thermal barrier layer

#27 | 2009-10-29

US20090269207A1

Mechanical engineering

COMPONENT, IN PARTICULAR, A GAS TURBINE COMPONENT

#28 | 2009-09-17

US20090233111A1

Mechanical engineering

Thermal Barrier Coating System

#29 | 2008-12-25

US20080317998A1

Chemistry; metallurgy

Wear-resistant coating

#30 | 2008-05-29

US20080124469A1

Chemistry; metallurgy

Method for producing a component covered with a wear-resistant coating

#31 | 2007-08-16

US20070190351A1

Mechanical engineering

Wear-resistant coating and a component having a wear-resistant coating

InventorID:

330049 ⎘