RETRACTABLE LANDING GEAR SYSTEM FOR A VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT

RETRACTABLE LANDING GEAR SYSTEM FOR A VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT

A retractable landing gear system for a vertical takeoff and landing (VTOL) aircraft includes a rotational strut rotatably coupled to a fuselage of the VTOL aircraft. The rotational strut includes a first end, a second end, and an intermediate portion extending therebetween. A drag strut includes a...

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Hauptverfasser: SATIRA, Jason A, GAYAGOY, Charles, ALBER, Mark R
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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creator SATIRA, Jason A
GAYAGOY, Charles
ALBER, Mark R
description A retractable landing gear system for a vertical takeoff and landing (VTOL) aircraft includes a rotational strut rotatably coupled to a fuselage of the VTOL aircraft. The rotational strut includes a first end, a second end, and an intermediate portion extending therebetween. A drag strut includes a first end portion pivotally connected to the rotational strut and a second end portion. A locking link includes a first end section pivotally connected relative to the fuselage, a second end section pivotally connected to the drag strut and an intermediate section having a hinge element. A retraction system is operatively connected to the rotational strut and the locking link. The retraction system is operable to pivot the drag strut about a first axis and rotate the rotational strut about a second axis that is distinct from the first axis.
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language eng ; fre ; ger
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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title RETRACTABLE LANDING GEAR SYSTEM FOR A VERTICAL TAKEOFF AND LANDING (VTOL) AIRCRAFT
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