Controlling lifting gas in inflatable structures
Devices, systems, and methods are directed to controlling lifting gas in a volume defined by an inflatable structure of an aircraft. For example, controlling lifting gas in the volume of the inflatable structure may account for variations in ambient and tactical conditions experienced by the aircraft over the course of flight, as may be useful for lifting the aircraft to a target altitude and/or carrying out a particular mission. Additionally, or alternatively, controlling lifting gas in the volume of the inflatable structure may facilitate lifting the aircraft using lifting gas generated by reacting stable materials with one another at a launch site in the field. As an example, aluminum may react with water to form a lifting gas including hydrogen and steam. As the steam condenses to water in the inflatable structure, a valve may expel water from the inflatable structure to assist in maintaining buoyancy of the aircraft.
1. An aircraft comprising:
an inflatable structure defining a volume;
activated aluminum;
a reactor defining a chamber, an inlet region, and an outlet region, the inlet region and the outlet region in fluid communication with one another via the chamber, the activated aluminum disposed in the chamber, the inlet region releasably securable in fluid communication with a source of water from which water is flowable into the chamber, via the inlet region, under a pressure difference across the inlet region, and the activated aluminum reactive with water in the chamber to generate a hydrogen-containing lifting gas receivable into the volume of the inflatable structure via fluid communication between the volume and the outlet region of the reactor; and
an exhaust in fluid communication between the chamber of the reactor and the volume of the inflatable structure, wherein the chamber of the reactor and the exhaust are movable with the inflatable structure, in a direction away from the source of water, under buoyancy of lifting gas in the volume of the inflatable structure.
2. The aircraft of claim 1 , wherein the inlet region and the outlet region are disposed along a single side of the reactor.
3. The aircraft of claim 1 , wherein water is flowable into the chamber, via the inlet region, under a pressure difference associated with gravitational force across the inlet region.
4. The aircraft of claim 1 , wherein the inflatable structure includes a balloon formed of a compliant material.
5. The aircraft of claim 1 , further comprising a drain valve in fluid communication between the outlet region of the reactor and the volume of the inflatable structure, the drain valve actuatable to expel condensate from the volume while maintaining a substantially gas-tight steal between the volume and an environment outside of the volume.
6. The aircraft of claim 5 , wherein the drain valve is a float valve.
7. The aircraft of claim 5 , wherein the drain valve is self-actuatable to open and close based on a level of the condensate in the volume of the inflatable structure.
8. The aircraft of claim 5 , wherein the inflatable structure is hydrophobic along the volume.
9. An aircraft comprising:
an inflatable structure defining a volume;
activated aluminum; and
a reactor defining a chamber, an inlet region, and an outlet region, the inlet region and the outlet region in fluid communication with one another via the chamber, the activated aluminum disposed in the chamber, the inlet region releasably securable in fluid communication with a source of water from which water is flowable into the chamber, via the inlet region, under a pressure difference across the inlet region, and the activated aluminum reactive with water in the chamber to generate a hydrogen-containing lifting gas receivable into the volume of the inflatable structure via fluid communication between the volume and the outlet region of the reactor;
wherein the reactor includes a housing and a liner, the liner defining the chamber, the activated aluminum reactive with water in the liner and, and with reaction byproducts contained herein, the liner removable from the housing.
10. The aircraft of claim 9 , wherein the liner is removable from and placeable into the housing with the inlet region and the outlet region each remaining connected to the housing.
11. The aircraft of claim 9 , wherein the liner is formed of one or more polymers.
12. The aircraft of claim 9 , wherein the liner is a bag.
13. The aircraft of claim 9 , wherein water is flowable into the chamber, via the inlet region, under a pressure difference associated with gravitational force across the inlet region.
14. The aircraft of claim 9 , wherein the liner is mechanically coupled to the inflatable structure, and the liner is movable away from the housing under buoyancy of the inflatable structure.
15. The aircraft of claim 14 , wherein the liner is tethered to the inflatable structure.
16. The aircraft of claim 9 , wherein the reactor includes a door separate from the inlet region and the outlet region, and the liner is removable from the housing via the door.
17. The aircraft of claim 16 , wherein the liner is at least partially compressible as the liner moves into and out of the housing via the door.
18. The aircraft of claim 9 , wherein the door is spaced apart from the inlet region and the outlet region.