SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT

SYSTEM AND METHOD FOR LINKAGE LENGTH ADJUSTMENT

A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relative...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
1. Verfasser: WIINIKKA, MARK A
Format: Patent
Sprache:eng ; fre
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
BEARINGS
BLASTING
COSMONAUTICS
ELEMENTS OR CRANKSHAFT MECHANISMS
ENGINEERING ELEMENTS AND UNITS
FLEXIBLE SHAFTS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
HELICOPTERS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
ROTARY BODIES OTHER THAN GEARING ELEMENTS
SHAFTS
THERMAL INSULATION IN GENERAL
TRANSPORTING
WEAPONS
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Beschreibung
Zusammenfassung:A rotor system has a rotor (302), an axis of rotation about which the rotor (302) may be rotated, a linkage system (310) having a first adjustable length portion (210) and a second adjustable length portion (212), wherein the second adjustable length portion (212) is configured to provide a relatively finer adjustment of an overall effective length of the linkage system (310) as compared to the first adjustable length portion (210) and wherein the rotor (302) is configured to rotate about the axis in response to changing the overall effective length of the linkage system (310).