Airfoil assembly with leading edge element

An airfoil assembly including a composite body having a mounting edge and a trailing edge which is secured to a leading edge element defining a 3-D leading edge geometry with both chord and camber variation.

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Bibliographic Details
Main Authors Kray, Nicholas Joseph, Shim, Dong-Jin, Wood, Trevor Howard, Shah, Pranav Dhoj
Format Patent
LanguageEnglish
Published 21.01.2020
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:An airfoil assembly including a composite body having a mounting edge and a trailing edge which is secured to a leading edge element defining a 3-D leading edge geometry with both chord and camber variation.
Bibliography:Application Number: US201615040582