Thermisch Aktivierte Durchflussregelvorrichtung

Details

Veröffentlichungs-Nr.

EP4711598

Anmeldetag

4. Juli 2025

Veröffentlichung

18. März 2026

Rechtsraum

EP

IPC

F02C7/04, F02C7/042, F02C7/047

Abstract

Systems, apparatuses and methods can provide for technology includes a turbofan engine subassembly having an inlet surface with a first side and a second side, and one or more flow effectors coupled to the inlet surface, wherein the flow effector(s) transition from a retracted position to an extended position on the second side of the inlet surface in response to an ambient temperature on the first side of the inlet surface exceeding a first threshold. The flow effector(s) may also transition from the extended position to the retracted position in response to the ambient temperature on the first side of the inlet surface falling below a second threshold.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA