NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Aircraft Engine Icing Event Avoidance and Mitigation Through Real-Time Simulation and ControlsA process for mitigating or proactively avoiding an aircraft engine icing event may include detecting ice crystals in the atmosphere using one or more sensors on board an aircraft in real time. The process may also include modulating one or more engine operating conditions to proactively change an ice accretion location, to avoid the occurrence of an icing event. The process may further include implementing one or more modulated engine operating conditions in engine controls software, hardware, or both.
Document ID
20190000788
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Veres, Joseph P.
Jorgenson, Philip C.
Date Acquired
February 14, 2019
Publication Date
January 22, 2019
Subject Category
Avionics And Aircraft Instrumentation
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-10,184,405
Patent Application
US-Patent-Appl-SN-15/474,562
No Preview Available