MULTI-ELEMENT ROTOR BLADE

A main rotor assembly (12) for a rotary wing aircraft includes a blade assembly (20) secured to a rotor hub. The blade assembly includes a rotor blade (26) and a slat (28) positioned to define a slat gap between the rotor blade and the slat. One or more struts (32) extend from the rotor blade to the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	HEIN, Benjamin Reed
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COSMONAUTICS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HELICOPTERS PERFORMING OPERATIONS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING
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Beschreibung
Zusammenfassung:	A main rotor assembly (12) for a rotary wing aircraft includes a blade assembly (20) secured to a rotor hub. The blade assembly includes a rotor blade (26) and a slat (28) positioned to define a slat gap between the rotor blade and the slat. One or more struts (32) extend from the rotor blade to the slat to position the slat and control motion of the slat. The rotor blade and the slat are secured to a common rotor cuff such that the rotor cuff acts as a centrifugal force support.