Rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight
US-10752357-B2 · Aug 25, 2020 · US
US11053008B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11053008-B2 |
| Application number | US-201816161415-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 16, 2018 |
| Priority date | Oct 16, 2018 |
| Publication date | Jul 6, 2021 |
| Grant date | Jul 6, 2021 |
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Official abstract text for this publication.
A parasite aircraft for airborne deployment and retrieve includes a wing; a fuselage rotatably mounted to the wing; a dock disposed on top of the fuselage and configured to receive a maneuverable capture device of a carrier aircraft; a pair of tail members extending from the fuselage; and a plurality of landing gear mounted to the wing. A method of preparing a parasite aircraft for flight includes unfolding an end portion of a wing; unfolding an end portion of a tail member of the parasite aircraft; and rotating a fuselage of the parasite aircraft so that the fuselage is perpendicular to the wing. A method of preparing a parasite aircraft for storage includes rotating a fuselage of the parasite aircraft to be parallel with a wing of the parasite aircraft; folding an end portion of the wing; and folding an end portion of a tail member of the parasite aircraft.
Opening claim text (preview).
What is claimed is: 1. A parasite aircraft comprising: a wing; a fuselage rotatably mounted to the wing; a dock disposed on top of the fuselage and configured to receive a maneuverable aircraft that is a capture device of a carrier aircraft; a pair of tail members extending from the fuselage; a plurality of landing gear mounted to the wing; and wherein the parasite aircraft excludes vertical take-off and landing (VTOL) capabilities and is configured to be at least one of deployed and retrieved vertically, in flight, using the maneuverable aircraft. 2. The parasite aircraft of claim 1 , wherein the dock further comprises a housing configured to receive a portion of the maneuverable aircraft to secure the maneuverable aircraft in the dock. 3. The parasite aircraft of claim 1 , wherein the dock further comprises a pin configured to mate with a hook of the maneuverable aircraft when the maneuverable aircraft is docked in the dock. 4. The parasite aircraft of claim 1 , wherein the dock is positioned on top of the parasite aircraft above a center of gravity of the parasite aircraft. 5. The parasite aircraft of claim 1 , wherein the wing comprises end portions that fold. 6. The parasite aircraft of claim 1 , wherein each tail member of the pair of tail members comprises an end portion that folds. 7. The parasite aircraft of claim 1 , wherein the wing comprises a pylon for securing a payload. 8. The parasite aircraft of claim 1 , further comprising a propulsion system disposed within an aft portion of the fuselage. 9. The parasite aircraft of claim 8 , wherein the propulsion system comprises a proprotor.
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