Mery/Oise, France

Gilles Charles Klein

This inventor holds 3 USPTO granted patents, plus 13 CIPO patents. Top assignee: Societe Nationale D'etude Et De Construction De Moteurs D'aviation. Active years: 1996-1999.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Gilles Charles Klein. Retrieved from https://idiyas.com/inventor/gilles-charles-klein

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile


% Patents Active = 100.0

 

Average Co-Inventor Count = 2.5

ph-index = 2

Forward Citations = 27(Granted Patents)


Location History:

  • Mery S/Oise, FR (1996)
  • Mery/Oise, FR (1999)

Company Filing History:


Years Active: 1996-1999

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3 patents (USPTO):Explore Patents

Title: **Innovator Gilles Charles Klein: Mastering Turbomachine Blade Manufacturing**

Introduction

Gilles Charles Klein, based in Mery/Oise, France, is a prominent inventor known for his groundbreaking contributions to the field of turbomachinery. With a total of three patents to his name, Klein has made significant strides in the manufacturing processes of hollow turbomachine blades. His innovative approaches have enhanced the efficiency and performance of these critical components.

Latest Patents

Klein's latest patents focus on sophisticated manufacturing processes for hollow turbomachine blades. One of his notable inventions is a process for the manufacture of a hollow turbomachine blade involving the assembly of die-forged and machined sheets that are diffusion welded face to face. This process includes applying an antidiffusion coating to specific areas of the sheets before they undergo a unique unsticking step. This step involves localized heating and the controlled injection of pressurized gas, designed to facilitate the formation of a gas distribution duct while ensuring a successful unsticking of the coated areas.

Another significant patent describes a method of manufacturing a hollow blade for a turbomachine where primary sheet-like components with anti-diffusion coatings are assembled and diffusion welded. Before this welding, a preheating treatment is performed to purge binders from the coatings, followed by evacuating the interior while progressively heating the assembly. This method culminates in the application of isostatic pressure, effectively compacting the anti-diffusion material and pre-welding uncoated areas, which optimizes the overall blade structure.

Career Highlights

Gilles Charles Klein is associated with the Société Nationale d'Étude et de Construction de Moteurs d'Aviation. His work there emphasizes innovation in turbomachinery, showcasing not only his technical expertise but also his commitment to advancing aerospace engineering. His patents exemplify a precise understanding of materials and methods that propel the industry forward.

Collaborations

Klein's work is further enriched by collaborations with fellow professionals, including Gilles Michel Calle and Philippe Louis Alassoeur. These partnerships highlight a collective effort aimed at pushing the boundaries of current technologies in the aerospace sector, fostering a rich environment for innovation and discovery.

Conclusion

Gilles Charles Klein remains a pivotal figure in the field of turbomachinery manufacturing. His patented processes and methods are set to redefine standards in blade production, ensuring enhanced performance in aviation engines. As he continues to innovate and collaborate within his industry, Klein undoubtedly contributes to the future of aerospace engineering, paving the way for new advancements and technologies.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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