US 11,591,081 B2Granted

Vertical-lift augmentation system

AssigneeTextron Innovations Inc.

InventorChristopher M. Johnson

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Abstract

In an embodiment, a vertical-lift augmentation system for an aircraft includes a fan bank mounted to the aircraft in proximity to a wing of the aircraft, where the fan bank may include at least one fan. The vertical-lift augmentation system also includes a panel movably attached to the aircraft in relation to the fan bank, where the panel is adjustable between at least a first position in which the panel encloses the fan bank in the aircraft and a second position in which the panel at least partially exposes the fan bank.

Claims6

Dependent claims

An aircraft operable in an airplane mode and a helicopter mode;

the aircraft comprising:
a fuselage;
a forward pair of ducted rotors rotatably coupled directly to the fuselage on opposite sides of the fuselage;
a wing extending from the fuselage aft of the forward pair of ducted rotors;
an aft pair of ducted rotors rotatably mounted at opposite outboard ends of the wing, wherein the forward pair and the aft pair of ducted rotors provide forward thrust when the aircraft is in an airplane mode and vertical thrust when the aircraft is in a helicopter mode;
a first fan bank mounted to the wing on a first side of the fuselage, wherein the first fan bank is configured to provide vertical thrust when engaged;
a second fan bank mounted to the wing on a second side of the fuselage opposite the first side, wherein the second fan bank is configured to provide vertical thrust when engaged;
a first panel movably attached to the wing in relation to the first fan bank, wherein the first panel is adjustable between at least a closed position in which the first panel encloses the first fan bank in the wing in the airplane mode and an open position in which the first panel at least partially exposes the first fan bank in the helicopter mode;
a second panel movably attached to the wing in relation to the second fan bank, wherein the second panel is adjustable between at least a closed position in which the second panel encloses the second fan bank in the wing in the airplane mode and an open position in which the second panel at least partially exposes the second fan bank in the helicopter mode;
a third fan bank mounted to the first side of the fuselage adjacent to a first wing root of the wing;
a third panel movably attached to the fuselage in relation to the third fan bank, wherein the third panel is adjustable between at least a closed position in which the third panel encloses the third fan bank in the fuselage and an open position in which the third panel at least partially exposes the third fan bank;
a fourth fan bank mounted to the second side of the fuselage adjacent to a second wing root of the wing;
and
a fourth panel movably attached to the fuselage in relation to the fourth fan bank, wherein the fourth panel is adjustable between at least a closed position in which the fourth panel encloses the fourth fan bank in the fuselage and an open position in which the fourth panel at least partially exposes the fourth fan bank.

11 more elements

Dependencies are inferred from the claim text.

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Abstract

An aircraft operable in an airplane mode and a helicopter mode;

the aircraft comprising:
a fuselage;
a forward pair of ducted rotors rotatably coupled directly to the fuselage on opposite sides of the fuselage;
a wing extending from the fuselage aft of the forward pair of ducted rotors;
an aft pair of ducted rotors rotatably mounted at opposite outboard ends of the wing, wherein the forward pair and the aft pair of ducted rotors provide forward thrust when the aircraft is in an airplane mode and vertical thrust when the aircraft is in a helicopter mode;
a first fan bank mounted to the wing on a first side of the fuselage, wherein the first fan bank is configured to provide vertical thrust when engaged;
a second fan bank mounted to the wing on a second side of the fuselage opposite the first side, wherein the second fan bank is configured to provide vertical thrust when engaged;
a first panel movably attached to the wing in relation to the first fan bank, wherein the first panel is adjustable between at least a closed position in which the first panel encloses the first fan bank in the wing in the airplane mode and an open position in which the first panel at least partially exposes the first fan bank in the helicopter mode;
a second panel movably attached to the wing in relation to the second fan bank, wherein the second panel is adjustable between at least a closed position in which the second panel encloses the second fan bank in the wing in the airplane mode and an open position in which the second panel at least partially exposes the second fan bank in the helicopter mode;
a third fan bank mounted to the first side of the fuselage adjacent to a first wing root of the wing;
a third panel movably attached to the fuselage in relation to the third fan bank, wherein the third panel is adjustable between at least a closed position in which the third panel encloses the third fan bank in the fuselage and an open position in which the third panel at least partially exposes the third fan bank;
a fourth fan bank mounted to the second side of the fuselage adjacent to a second wing root of the wing;
and
a fourth panel movably attached to the fuselage in relation to the fourth fan bank, wherein the fourth panel is adjustable between at least a closed position in which the fourth panel encloses the fourth fan bank in the fuselage and an open position in which the fourth panel at least partially exposes the fourth fan bank.

11 more elements