CASCADE VANE LEADING EDGE

CASCADE VANE LEADING EDGE

Aspects of the disclosure are directed to a cascade vane for an aircraft, comprising: a leading edge that is configured to interface to a fluid flow, where the leading edge is associated with a first thickness that is proximate to the fluid flow, and where the leading edge is associated with a secon...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Pritekel Joshua, Whitaker Anthony, Wen Matthew
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:Aspects of the disclosure are directed to a cascade vane for an aircraft, comprising: a leading edge that is configured to interface to a fluid flow, where the leading edge is associated with a first thickness that is proximate to the fluid flow, and where the leading edge is associated with a second thickness that is further from the fluid flow than the first thickness, and where the first thickness is smaller than the second thickness such that the leading edge includes a distance associated with a blended profile between the first thickness and the second thickness.