Modular articulated-wing aircraft
First Claim
1. An autonomous modular flyer operable to loiter over an area of interest at a first high altitude, comprising:
- a solar-electric powered airborne object having two wings, each wing having an upper wing surface having a photovoltaic array thereon exposed to solar flux during flight of the autonomous modular flyer and a wingtip, the wingtips being operably joinable to at least one other solar-electric powered autonomous modular flyer'"'"'s wingtips to form an aggregation when a first predetermined condition is met, and being operably disaggregable from the at least one other autonomous modular flyer'"'"'s wingtips when a second predetermined condition is met;
the aggregation forming an autonomous solar-electric powered multiple-articulated flying system having a high aspect ratio wing platform, operable to loiter over the area of interest at an altitude at least as high as the first high altitude, each autonomous modular flyer in the aggregation being of the same type; and
means for controlling the number of autonomous modular flyers of the autonomous multiple-articulated flying system based on the amount of solar flux to which the photovoltaic arrays are exposed.
1 Assignment
0 Petitions
Accused Products
Abstract
Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.
-
Citations
22 Claims
-
1. An autonomous modular flyer operable to loiter over an area of interest at a first high altitude, comprising:
-
a solar-electric powered airborne object having two wings, each wing having an upper wing surface having a photovoltaic array thereon exposed to solar flux during flight of the autonomous modular flyer and a wingtip, the wingtips being operably joinable to at least one other solar-electric powered autonomous modular flyer'"'"'s wingtips to form an aggregation when a first predetermined condition is met, and being operably disaggregable from the at least one other autonomous modular flyer'"'"'s wingtips when a second predetermined condition is met; the aggregation forming an autonomous solar-electric powered multiple-articulated flying system having a high aspect ratio wing platform, operable to loiter over the area of interest at an altitude at least as high as the first high altitude, each autonomous modular flyer in the aggregation being of the same type; and means for controlling the number of autonomous modular flyers of the autonomous multiple-articulated flying system based on the amount of solar flux to which the photovoltaic arrays are exposed. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
-
-
14. A method of forming an autonomous multiple-articulated flying system having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude, the method comprising:
-
providing at least two solar-electric powered autonomous modular flyers, each having two wings with wingtips thereon and being of the same type, wherein each wing has an upper wing surface having a photovoltaic array thereon exposed to solar flux during flight of the autonomous modular flyer; joining the wingtips of the at least two autonomous modular flyers to form the autonomous multiple-articulated flying system when a first predetermined condition is met; and controlling the number of autonomous modular flyers of the autonomous multiple-articulated flying system based on the amount of solar flux to which the photovoltaic arrays are exposed. - View Dependent Claims (15, 16, 17, 18, 19, 20, 21, 22)
-
Specification