US 6,042,052 AGranted

Retractable step fairing for amphibian airplane

OwnerDonald E. Smithinventor

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Abstract

The invention comprises an improved seaplane having a retractable step. The term retractable step, however, is a misnomer. The step portion of the seaplane float includes a panel which may be extended once the plane is airborne to reduce aerodynamic drag created by such hydrodynamic steps. The panel may be hinged at a rear portion of the aircraft and extended and retracted using a hydraulic strut or the like. Side panels may also be provided which would hinge via a piano type hinge or the like to the sides of the extendable panel. The side panels may be provided with an end pin or pins which would travel in a track within the step cavity such that the side panels would be pushed into position as the step cover panel is extended. The apparatus of the present invention may be employed in both conventional and tunnel type hulls.

Claims12

Dependent claims

An aircraft comprising:

at least one floating hull have a major axis along a longitudinal axis of the aircraft;
a hydrodynamic step, formed at an aft portion of the at least one floating hull, said hydrodynamic step generating vortices so as to allow the at least one hull to cleanly separate from water flow when said aircraft becomes airborne;
and
a retractable fairing, coupled to the at least one floating hull, said retractable fairing retractable into the hydrodynamic step when the aircraft is waterborne and extendable to cover the hydrodynamic step when the aircraft is airborne so as to reduce aerodynamic drag,
wherein said retractable fairing further comprises:
a lower fairing portion having a cross-sectional shape conforming to a cross-sectional shape of the shape of the at least one hull at an edge of the hydrodynamic step, and
wherein said retractable step further comprises:
a first hinge portion, having a first portion attached at a rearward portion of the lower fairing portion and a second portion attached at a rear portion of the hydrodynamic step, so as to allow said lower fairing portion to hinge upwardly into the hydrodynamic step.

5 more elements

An retractable step fairing for an aircraft having at least one floating hull have a major axis along a longitudinal axis of the aircraft and a hydrodynamic step, formed at an aft portion of the at least one floating hull, the hydrodynamic step generating vortices so as to allow the at least one hull to cleanly separate from water flow when said aircraft becomes airborne, said retracting fairing comprising:

a lower fairing portion, coupled to the at least one floating hull, said lower fairing portion retractable into the hydrodynamic step when the aircraft is waterborne and extendable to cover the hydrodynamic step when the aircraft is airborne so as to reduce aerodynamic drag;
and
a first hinge portion, having a first portion attached at a rearward portion of the lower fairing portion and a second portion attached at a rear portion of the hydrodynamic step, so as to allow said lower fairing portion to hinge upwardly into the hydrodynamic step,
wherein said lower fairing portion has a cross-sectional shape conforming to a cross-sectional shape of the shape of the at least one hull at an edge of the hydrodynamic step.

1 more element

Dependencies are inferred from the claim text.