Loitering craft
A craft is provided comprising: a propulsion system; a fuselage coupled with the propulsion system, wherein the fuselage is configured to carry a payload and fuel for the propulsion system; and a pre-assembled wing coupled with the fuselage; wherein the craft is designed to take-off without using a runway and does not have landing gear to land.
1 . A craft comprising:
a propulsion system;
a fuselage configured to carry a payload;
a wing coupled to the fuselage, the wing comprising:
a first spar and a second spar, wherein the first spar and the second spar are arranged substantially perpendicular to the fuselage;
a plurality of ribs, wherein each rib extends between the first spar and the second spar, and wherein each rib is arranged substantially parallel to the fuselage; and
at least one surface comprising a flexible membrane;
a control system comprising data storage having instruction code stored thereon that, when executed by one or more processors, causes the craft to:
fly above water at a distance above the water that is less than one fourth of a chord length of the wing;
while flying above the water, determine that a condition of the craft meets a criterion; and
after determining that the condition meets the criterion, disengage the fuselage from the wing.
2 . The craft of claim 1 , wherein the fuselage is further configured to carry fuel for the propulsion system, wherein the fuselage is coupled with the propulsion system.
3 . The craft of claim 1 , wherein the criterion comprises the craft being within a threshold distance of the water.
4 . The craft of claim 1 , wherein the criterion comprises the craft being in contact with the water.
5 . The craft of claim 1 , wherein the criterion comprises the craft being within a threshold distance of a destination.
6 . The craft of claim 1 , wherein the criterion comprises at least one of (a) the craft determining the craft has been damaged and (b) the craft determining the craft may become damaged.
7 . The craft of claim 1 , wherein the criterion comprises the craft receiving a signal transmitted by a remote device.
8 . The craft of claim 1 , wherein disengaging the fuselage comprises disengaging one or more connecting elements via one or more actuators.
9 . The craft of claim 1 , wherein the data storage further has instruction code stored thereon that, when executed by one or more processors, causes the craft to:
after disengaging the fuselage from the wing, propell the fuselage within the water.
10 . The craft of claim 9 , wherein the propulsion system is a first propulsion system, and the craft further comprises a second propulsion system, wherein propelling the fuselage within the water comprises propelling the fuselage within the water via the second propulsion system.
11 . The craft of claim 1 , wherein at least one of (a) the first spar comprises a D-tube (b) and the second spar comprises carbon.
12 . The craft of claim 1 , wherein the wing further comprises one or more control surfaces.
13 . The craft of claim 1 , further comprising a box tail.
14 . The craft of claim 13 , wherein the box tail comprises a first side panel comprising a first rudder and a second side panel comprising a second rudder.
15 . The craft of claim 1 , wherein the fuselage comprises the control system, at least one sensor, and at least one battery.
16 . The craft of claim 1 , wherein the wing further comprises a plurality of ultrasonic sensors affixed to a bottom surface of the wing.
17 . The craft of claim 1 , wherein the craft does not comprise cither a hydrofoil or a wheel.
18 . The craft of claim 1 , further comprising an attaching mechanism configured to attach the craft to a launcher.