Thomas GOEHLER

Person

Dachau, DE

People

Patents Grantslast 30 patents

Information Patent Grant
Turbine blade and aircraft engine comprising same
- Patent number 10,577,948
- Issue date Mar 3, 2020
- MTU Aero Engines AG
- Wilfried Smarsly
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Nickel-based alloy with optimized matrix properties
- Patent number 10,487,376
- Issue date Nov 26, 2019
- MTU Aero Engines AG
- Thomas Goehler
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Grant
Rhenium-free or rhenium-reduced nickel-base superalloy
- Patent number 9,850,765
- Issue date Dec 26, 2017
- MTU Aero Engines AG
- Robert F. Singer
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Grant
Irradiation in generative fabrication
- Patent number 9,636,769
- Issue date May 2, 2017
- MTU Aero Engines AG
- Thomas Goehler
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR

Patents Applicationslast 30 patents

Information Patent Application
SIMULATION METHOD FOR DEVELOPING A PRODUCTION PROCESS
- Publication number 20210162541
- Publication date Jun 3, 2021
- MTU Aero Engines AG
- Thomas Goehler
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
SIMULATION METHOD FOR DEVELOPING A PRODUCTION PROCESS
- Publication number 20180071868
- Publication date Mar 15, 2018
- MTU Aero Engines AG
- Thomas Goehler
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
HEAT TREATMENT PROCESS FOR COMPONENTS COMPOSED OF NICKEL-BASED SUPE...
- Publication number 20170241005
- Publication date Aug 24, 2017
- MTU AERO ENGINES AG
- Thomas GOEHLER
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Application
TURBINE BLADE AND AIRCRAFT ENGINE COMPRISING SAME
- Publication number 20170122256
- Publication date May 4, 2017
- MTU AERO ENGINES AG
- Wilfried SMARSLY
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
RHENIUM-FREE NICKEL BASE SUPERALLOY OF LOW DENSITY
- Publication number 20170058383
- Publication date Mar 2, 2017
- MTU AERO ENGINES AG
- Thomas GOEHLER
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Application
OPTIMIZED NICKEL-BASED SUPERALLOY
- Publication number 20170051382
- Publication date Feb 23, 2017
- MTU AERO ENGINES AG
- Thomas GOEHLER
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Application
NICKEL-BASED ALLOY WITH OPTIMIZED MATRIX PROPERTIES
- Publication number 20150284824
- Publication date Oct 8, 2015
- MTU AERO ENGINES AG
- Thomas GOEHLER
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...
Information Patent Application
CREATION OF RESIDUAL COMPRESSIVE STRESSES DURING ADDITVE MANUFACTURING
- Publication number 20150246481
- Publication date Sep 3, 2015
- MTU Aero Engines AG
- Georg Schlick
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
Irradiation in generative fabrication
- Publication number 20150165545
- Publication date Jun 18, 2015
- MTU AERO ENGINES AG
- Thomas Goehler
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
RHENIUM-FREE OR RHENIUM-REDUCED NICKEL-BASE SUPERALLOY
- Publication number 20140356183
- Publication date Dec 4, 2014
- MTU Aero Engines AG
- Robert F. Singer
- C22 - METALLURGY FERROUS OR NON-FERROUS ALLOYS TREATMENT OF ALLOYS OR NON-FER...

Thomas GOEHLER

Person

Patents Grantslast 30 patents

Turbine blade and aircraft engine comprising same

Nickel-based alloy with optimized matrix properties

Rhenium-free or rhenium-reduced nickel-base superalloy

Irradiation in generative fabrication

Patents Applicationslast 30 patents

SIMULATION METHOD FOR DEVELOPING A PRODUCTION PROCESS

SIMULATION METHOD FOR DEVELOPING A PRODUCTION PROCESS

HEAT TREATMENT PROCESS FOR COMPONENTS COMPOSED OF NICKEL-BASED SUPE...

TURBINE BLADE AND AIRCRAFT ENGINE COMPRISING SAME

RHENIUM-FREE NICKEL BASE SUPERALLOY OF LOW DENSITY

OPTIMIZED NICKEL-BASED SUPERALLOY

NICKEL-BASED ALLOY WITH OPTIMIZED MATRIX PROPERTIES

CREATION OF RESIDUAL COMPRESSIVE STRESSES DURING ADDITVE MANUFACTURING

Irradiation in generative fabrication

RHENIUM-FREE OR RHENIUM-REDUCED NICKEL-BASE SUPERALLOY