Lighter than air balloon systems and methods
Described herein are features for a high altitude lighter-than-air (LTA) system and associated methods. The LTA may include one or more super-pressure balloons (SPB). One or more of the SPB's may include one or more interior volumes. One or more of the interior volumes may be configured to receive an LTA gas therein to supplement the free lift of the LTA system. There may be an adjustable valve or vent to release the LTA gas. One or more of the interior volumes may be configured to receive ambient air to provide a variable downward force. The SPB may use a compressor to pump in ambient air. The compressor or another valve may release ambient air to decrease the downward force. A zero-pressure balloon (ZPB) may be attached with the one or more SPB's. The ZPB may supplement lift for the system.
1. A lighter-than-air (LTA) high altitude balloon system comprising:
a zero-pressure balloon (ZPB) configured to receive therein a first mass of LTA gas to provide a first upward lifting force to the balloon system;
a super-pressure balloon (SPB) configured to couple with the ZPB, the SPB comprising an interior volume configured to receive therein a second mass of LTA gas to provide a second upward lifting force to the balloon system; and
the SPB comprising a first valve configured to be opened and closed, wherein the first valve when opened allows for release of at least a portion of the second mass of LTA gas from the SPB through the first valve to a surrounding atmosphere to decrease the second upward lifting force, and the first valve when closed does not allow for release of the second mass of LTA gas from the SPB through the first valve to the surrounding atmosphere,
wherein the interior volume of the SPB is further configured, after release of the at least a portion of the second mass of LTA gas from the SPB, to receive therein a variable amount of ambient air from the surrounding atmosphere to provide a variable downward force to the balloon system.
2. The high altitude balloon system of claim 1 , wherein a total mass of the first and second mass of LTA gas is configured to provide from about 5% free lift to about 15% free lift at launch.
3. The high altitude balloon system of claim 1 , wherein the lifting gas is helium or hydrogen.
4. The high altitude balloon system of claim 1 , further comprising:
a compressor; and
a fill tube fluidly connecting the compressor to the interior volume of the SPB, the fill tube configured to receive the second mass of LTA gas and to allow the second mass of LTA gas to flow through the fill tube to the interior volume of the SPB.
5. The high altitude balloon system of claim 4 , the compressor configured to provide the variable amount of ambient air from the surrounding atmosphere to the interior volume of the SPB.
6. The high altitude balloon system of claim 4 , further comprising:
an LTA gas inlet fluidly connected with the fill tube along an inlet flow path, the LTA gas inlet configured to receive the second mass of LTA gas and to allow the second mass of LTA gas to flow along the inlet flow path to the fill tube; and
a one-way valve located within the inlet flow path and configured to prevent backflow of the LTA gas across the valve.
7. The high altitude balloon system of claim 1 , wherein, after the interior volume of the SPB receives therein the variable amount of ambient air from the surrounding atmosphere, the first valve when opened allows for release of at least some of the ambient air to the surrounding atmosphere to decrease the downward force.
8. The high altitude balloon system of claim 1 , further comprising a second valve in fluid communication with the ambient air and with the interior volume of the SPB, the second valve configured to be adjusted, after the interior volume of the SPB receives therein the variable amount of ambient air from the surrounding atmosphere, to release the ambient air from the interior volume of the SPB to the surrounding atmosphere to decrease the downward force.
9. The high altitude balloon system of claim 1 , the SPB comprising:
an upper chamber; and
a lower chamber fluidly connected with the upper chamber, wherein the first valve is located on the upper chamber.
10. The high altitude balloon system of claim 9 , further comprising:
a compressor; and
a fill tube fluidly connecting the compressor to the interior volume of the SPB via a connection on the lower chamber, the fill tube configured to receive the second mass of LTA gas and to allow the second mass of LTA gas to flow through the fill tube to the interior volume of the SPB via the connection on the lower chamber.
11. The high altitude balloon system of claim 10 , the compressor configured to provide the variable amount of ambient air from the surrounding atmosphere to the interior volume of the SPB.
12. A lighter-than-air (LTA) high altitude balloon system comprising:
a zero-pressure balloon (ZPB) configured to receive therein a first LTA gas;
a super-pressure balloon (SPB) configured to couple with the ZPB, the SPB configured to receive therein a second LTA gas; and
a first valve configured to be adjusted to control release of at least a portion of the second LTA gas from the SPB,
wherein the SPB is further configured, after release of the at least a portion of the second LTA gas from the SPB, to receive therein a variable amount of ambient air from the surrounding atmosphere.
13. The high altitude balloon system of claim 12 , further comprising:
a compressor; and
a fill tube fluidly connecting the compressor to the SPB, the fill tube configured to provide the second LTA gas to the SPB.
14. The high altitude balloon system of claim 13 , the compressor configured to provide the variable amount of ambient air from the surrounding atmosphere to the SPB.