Turbinenmotorzustandserkennung und Verfahren für Offenen Fan

Details

Veröffentlichungs-Nr.

EP4814264

Anmeldetag

16. März 2026

Veröffentlichung

30. September 2026

Rechtsraum

EP

Abstract

An unducted turbine engine system (200) may include an emitter (212) positioned to direct an energy beam (214) towards a surface (205) of an airfoil (204) of an engine (100) to produce a reflected beam (216). The unducted turbine engine system (200) may include a detector (218) positioned to capture data from the reflected beam (216). The unducted turbine engine system (200) may include a processor (222) configured to determine a condition of the engine (100) based on data captured by the detector (218).

Anmelder

Firma

General Electric Company

Land

🇺🇸 USA