Barsac, France

Max Massot



 

Average Co-Inventor Count = 3.0

ph-index = 1

Forward Citations = 18(Granted Patents)


Company Filing History:


Years Active: 2016-2018

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2 patents (USPTO):Explore Patents

Title: Max Massot: Innovator in Turbojet Technology

Introduction

Max Massot is a notable inventor based in Barsac, France. He has made significant contributions to the field of turbojet technology, holding two patents that showcase his innovative spirit and technical expertise.

Latest Patents

One of Max Massot's latest patents is a flame-holder device designed for a reheat channel of a turbojet. This device features an arm shaped like a trough that defines a cavity, along with a heat shield fastened within the arm's cavity. Additionally, the flame-holder device includes a fastener plate with a first leg integrally formed with the plate and a second leg that is removable. The arm is securely attached to both legs using fastener members. Another significant patent is a method for fabricating a composite material turbine engine vane with incorporated platforms. This method employs multilayer weaving to create a fiber blank that aligns with the longitudinal direction of the vane. The process involves forming a preform for the vane by shaping various woven portions to create the airfoil and platform sections.

Career Highlights

Throughout his career, Max Massot has worked with prominent companies in the aerospace sector, including Herakles and Snecma. His experience in these organizations has allowed him to refine his skills and contribute to cutting-edge projects in turbojet technology.

Collaborations

Max has collaborated with talented individuals such as Elric Fremont and Romain Nunez. These partnerships have fostered a creative environment that has led to innovative solutions in their respective fields.

Conclusion

Max Massot's contributions to turbojet technology through his patents and collaborations highlight his role as a key innovator in the aerospace industry. His work continues to influence advancements in turbine engine design and fabrication.

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