Duisburg, Germany

Frank Günther

USPTO Granted Patents = 2 


Average Co-Inventor Count = 7.5

ph-index = 2

Forward Citations = 11(Granted Patents)


Company Filing History:


Years Active: 2010-2011

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2 patents (USPTO):Explore Patents

Title: Frank Günther: Innovator in Gas Turbine Technology

Introduction

Frank Günther is a notable inventor based in Duisburg, Germany. He has made significant contributions to the field of gas turbine technology, holding two patents that showcase his innovative approach to engineering challenges.

Latest Patents

Günther's latest patents include a gas turbine with a protective sheath for a probe and a method for protecting an instrument lead laid in a protective sheath. The first invention relates to a gas turbine featuring a flow path for hot gas, enclosed by a channel wall. This design incorporates a measuring probe that determines a parameter of the hot gas, with a temperature-resistant measuring tip in contact with the gas. The measuring line is arranged outside the flow path within a protective sleeve, which includes a flow of coolant to safeguard the measuring lines from high operating temperatures. The second patent describes a method for cooling a gas turbine after operation, where a liquid is introduced into the air stream upstream of the compressor during the cooling phase. This method aims to reduce downtime by intermittently driving the rotor at a reduced nominal speed.

Career Highlights

Throughout his career, Frank Günther has worked with prominent companies, including Siemens Aktiengesellschaft and Siemens AG. His experience in these organizations has allowed him to develop and refine his innovative ideas in gas turbine technology.

Collaborations

Günther has collaborated with notable colleagues such as Giuseppe Gaio and Matthias Beutin, contributing to advancements in their respective fields.

Conclusion

Frank Günther's work in gas turbine technology exemplifies his commitment to innovation and engineering excellence. His patents reflect a deep understanding of the complexities involved in gas turbine operation and cooling methods.

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