Safran Aircraft Engines

André Pierre Jean Xavier Leroux

Stéphane Rousselin

Jérémy Giordan

Valentine Lucette Bader

An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.

Growing community of inventors

Moissy Cramayel, France

André Pierre Jean Xavier Leroux