Inflatable folding wings for a very high altitude aircraft
View Patent ↗A foldable wing for use with a very high altitude aircraft capable of operating at an altitude at or above 85,000 feet is disclosed. The foldable wing may employ a spiral fold deployment, wherein a hinge between each segment of the foldable wing is slightly offset from the perpendicular. Successively positioned wing segments fold over one another. Alternatively, the hinges are substantially perpendicular so that each respective wing segment folds linearly against the next wing segment. An inflatable rib, with inflatable arms, can be inflated to provide a force against two adjacent arms, thereby deploying the wing segments through a full 180° of rotation.
1. A wing segment for a very high altitude aircraft capable of operating at an altitude at or above 85,000 feet, comprising:
at least two inflatable ribs, each inflatable rib comprising:
a plurality of inflatable tubes including an innermost tube;
a plurality of outer connecting surfaces, wherein each outer connecting surface connects one of the plurality of tubes to an adjacent one of the plurality of tubes;
an innermost connecting surface that connects an inner perimeter of the innermost tube to itself; and
a linking inflatable tube that is connected to each of the plurality of tubes, and is configured to receive gas and to distribute the received gas to the plurality of tubes, thereby inflating each of the tubes to form the inflatable rib;
a wing flexible skin disposed between the at least two inflatable ribs;
a plurality of stringers and a trailing edge, which are configured to maintain the wing segment in a predetermined airfoil shape.
2. The wing segment according to claim 1 , wherein at least one of the stringers comprises an inflatable tube.
3. The wing segment according to claim 1 , wherein at least one of the stringers comprises a rigid member comprising a metal.
4. The wing segment according to claim 1 , wherein the trailing edge comprises a rigid member comprising a metal.
5. The wing segment according to claim 1 , wherein each of the stringers comprises (i) one or more rigid materials on an exterior of the wing segment and (ii) an inflatable tube inside the wing segment, and wherein the inflatable tube is configured to provide stiffness with a predetermined stowed volume and to provide a predetermined wing segment shape.
6. The wing segment according to claim 1 , wherein the trailing edge comprises an inflatable tube.
7. The wing segment according to claim 1 , wherein at least one of the stringers comprises a rigid shape comprising a composite material.
8. The wing segment according to claim 1 , wherein the trailing edge comprises a rigid shape comprising a composite material.