This inventor holds 1 USPTO granted patent and 1 EPO patent. Top assignee: Turbomeca. Active years: 2014.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
Company Filing History:
Years Active: 2014
Title: Philippe Perot and His Turbine-Engine Compressor Invention.
Introduction
Philippe Perot is an inventor associated with Lons, France. His patent work includes a design for a centrifugal compressor cover used in a turbine engine. The available information lists 1 patent for him.
Latest Patents
Perot’s patent, “Compressor Cover for Turbine Engine Having Axial Abutment,” describes a centrifugal compressor with a bladed impeller rotating inside a casing. A cover extends over the impeller blades to form the outer surface of the gas-flow passage. It is fastened to the casing at its upstream end, while its downstream end remains free. An abutment limits axial movement of that downstream end relative to the casing during compressor operation.
Career Highlights
Perot is associated with Turbomeca and Safran Helicopter Engines. His patented compressor-cover design addresses the positioning of the cover during operation, an important aspect of turbine-engine compressor construction.
Collaborations
The listed coworkers associated with Perot include Yann Mouze and Philippe Denis Joubert.
Conclusion
Philippe Perot’s patent documents a turbine-engine compressor-cover design that uses an axial abutment to control movement during operation, reflecting his work in the aerospace engineering field.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
