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 a super-pressure balloon (SPB) and/or a zero-pressure balloon (ZPB). The SPB may include two, three, four or more chambers. There may be more than one SPB. The SPB may use a compressor to provide a variable amount of ballast air by pumping in or expelling out ambient air. The zero-pressure balloon (ZPB) may be attached with the multi-chamber SPB. The ZPB may provide lift for the system. The SPB may include lifting gas and ballast air to provide both lifting and descent functions. The SPB may have an internal barrier separating a lift gas compartment from a variable ballast air compartment.
1. A method of controlling a high altitude balloon system, the method comprising:
receiving air from a surrounding atmosphere into a super pressure balloon to increase a downward force to the balloon system;
expelling the air from within the super pressure balloon to the surrounding atmosphere to decrease the downward force to the balloon system, wherein the balloon system comprises a zero-pressure balloon, the super pressure balloon, a payload coupled with the super pressure balloon, and a parafoil coupled with the payload;
releasing the parafoil from the high altitude balloon system;
deploying the parafoil into a deployed flight configuration; and
descending the parafoil toward ground with the payload.
2. The method of claim 1 , further comprising receiving a lighter-than-air gas within the zero-pressure balloon to provide an upward force to the balloon system.
3. The method of claim 1 , wherein the parafoil comprises a canopy and a plurality of flexible rods attached to the canopy.
4. The method of claim 3 , further comprising deploying the canopy, wherein the plurality of flexible rods store potential energy in a flexed, stowed state before deploying the canopy and use the stored potential energy to assist with releasing and deploying the canopy.
5. The method of claim 1 , further comprising:
detecting an environmental attribute with a sensor; and
controlling a compressor and a valve based at least on the detected environmental attribute to control an amount of the air inside the super pressure balloon.
6. The method of claim 1 , further comprising biasing the super pressure balloon into a pumpkin shape using a plurality of tendons.
7. The method of claim 1 , further comprising receiving sunlight using a solar array for conversion to electrical energy.
8. The method of claim 1 , wherein the super pressure balloon comprises a multi-chamber super pressure balloon.
9. A method of operating a high altitude balloon system, the method comprising:
receiving lifting gas into a zero pressure balloon to increase an upward force on the balloon system, wherein the balloon system comprises the zero pressure balloon coupled with a super pressure balloon, and a descent system coupled with a payload;
receiving ambient air into the super pressure balloon to increase a downward force on the balloon system;
expelling the ambient air from the super pressure balloon to decrease the downward force on the balloon system;
releasing the descent system from the balloon system; and
descending the payload via the descent system.
10. The method of claim 9 , wherein the descent system comprises a parafoil having a canopy, and the method further comprises deploying the canopy.
11. The method of claim 9 , wherein the canopy is deployed prior to releasing the descent system from the balloon system.
12. The method of claim 9 , further comprising storing energy in flexible rods that release the energy to assist with deploying the canopy.
13. The method of claim 9 , further comprising reorienting the payload as the payload descends.
14. The method of claim 9 , wherein the super pressure balloon comprises a multi-chamber super pressure balloon.
15. A high altitude balloon system comprising:
a zero-pressure balloon;
a super pressure balloon configured to receive air from a surrounding atmosphere and expel the air from the surrounding atmosphere to control a downward force to the balloon system;
a compressor configured to pump the surrounding atmosphere into the super pressure balloon;
an air hose fluidly coupling the compressor with an interior volume of the super pressure balloon;
a payload support coupled with the super pressure balloon and configured to support a payload; and
a parafoil coupled with the payload support and configured to deploy into a deployed flight configuration to controllably descend with the payload support to a landing sight.
16. The system of claim 15 , wherein the parafoil comprises:
a canopy; and
a plurality of flexible rods coupling the payload support with the canopy.
17. The system of claim 16 , wherein the plurality of flexible rods are configured to store potential energy in a flexed, stowed state and use the stored potential energy to assist with releasing and deploying the canopy.
18. The system of claim 15 , further comprising
a sensor configured to detect an environmental attribute; and
a control system in communication with the sensor, the compressor, and the valve, the control system configured to control the compressor and the valve based at least on the detected environmental attribute to control the amount of air from the surrounding atmosphere inside the super pressure balloon.
19. The system of claim 15 , further comprising a valve configured to expel the air from the surrounding atmosphere from the super pressure balloon.
20. The system of claim 15 , wherein the super pressure balloon comprises a multi-chamber super pressure balloon.