Crosne, France

Monique Andrée Thore


Average Co-Inventor Count = 6.0

ph-index = 1

Forward Citations = 11(Granted Patents)


Company Filing History:


Years Active: 2002

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1 patent (USPTO):Explore Patents

Title: Monique Andrée Thore: Innovator in High-Pressure Compressor Technology

Introduction

Monique Andrée Thore is a notable inventor based in Crosne, France. He has made significant contributions to the field of gas turbine engines, particularly in the design of high-pressure compressor components. His innovative approach has led to the development of a unique stator that enhances the efficiency and performance of these engines.

Latest Patents

Thore holds a patent for a high-pressure compressor stator. This stator is designed for use in gas turbine engines and features two points of ventilation at different temperatures. The upstream section of the stator is constructed with a casing and a shroud, both of which are unbroken around the circumference and made from a material with a low degree of thermal expansion. In contrast, the downstream shroud is constructed using angular sectors made from a material with a higher degree of thermal expansion. This innovative design aims to improve the overall performance and reliability of high-pressure compressors.

Career Highlights

Monique Andrée Thore has had a distinguished career at Snecma Moteurs, where he has been instrumental in advancing compressor technology. His work has not only contributed to the efficiency of gas turbine engines but has also positioned him as a key figure in the field of aerospace engineering.

Collaborations

Thore has collaborated with notable colleagues, including Pascal Gérard Gervais and Pascal Michel Daniel Lejeune. These partnerships have fostered a collaborative environment that encourages innovation and the sharing of ideas within the aerospace sector.

Conclusion

Monique Andrée Thore's contributions to high-pressure compressor technology exemplify the spirit of innovation in the aerospace industry. His patented designs and collaborative efforts continue to influence the development of more efficient gas turbine engines.

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