Aircraft
US-2018362133-A1 · Dec 20, 2018 · US
US9573670B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9573670-B2 |
| Application number | US-201615090462-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 4, 2016 |
| Priority date | Feb 5, 2014 |
| Publication date | Feb 21, 2017 |
| Grant date | Feb 21, 2017 |
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Methods and apparatuses are disclosed for a self-stabilizing ballonet. A bladder or ballonet is provided within an envelope of a balloon. The bladder includes a spheroid body comprising an equator, a top pole, a bottom pole, and an axis crossing through the top pole and the bottom pole. The distance between two poles may be less than the equatorial distance. The bladder is sized and shaped for insertion into an envelope of a balloon and is inflatable to provide altitude control for the balloon.
Opening claim text (preview).
What is claimed is: 1. A method of manufacturing a variable buoyancy system comprising: providing a plurality of sheets; seaming two or more of the plurality of sheets together to form a ballonet having a spheroid body, wherein the spheroid body comprises an equator, a top pole, a bottom pole, and an axis crossing through the top pole and the bottom pole perpendicular to the equator, and wherein a distance around the equator is greater than a distance around the axis when fully inflated; forming a hole through the ballonet; and inserting the ballonet into an envelope that is fillable with a liquid or gas, wherein the envelope has a corresponding spheroid shape, and wherein the ballonet is formed such that when inflated, at least a portion of an outer surface of the ballonet conforms to an inner surface of the envelope. 2. The method of claim 1 , further comprising: folding the ballonet prior to inserting the ballonet into the envelope. 3. The method of claim 2 , wherein the folding comprises folding the ballonet along the equator of the ballonet. 4. A variable buoyancy system comprising: an envelope, wherein the envelope comprises an interior that is fillable with a liquid or gas; a ballonet within the envelope interior, the ballonet comprising: a spheroid body comprising an equator, a top pole, a bottom pole, and an axis crossing through the top pole and the bottom pole perpendicular to the equator; wherein a distance around the equator is greater than a distance around the axis when fully inflated; wherein the envelope has a corresponding spheroid shape, and wherein when inflated, at least a portion of an outer surface of the ballonet conforms to an inner surface of the envelope. 5. The variable buoyancy system of claim 4 , wherein the variable buoyancy is implemented as part of or takes the form of a balloon. 6. The system of claim 5 , wherein the balloon is a high-altitude balloon that is deployable in the stratosphere. 7. The variable buoyancy system of claim 4 , wherein the envelope is a superpressure envelope. 8. The variable buoyancy system of claim 4 , wherein the ballonet comprises a foldable and inflatable bladder configured to hold liquid or gas. 9. The variable buoyancy system of claim 8 , wherein the ballonet comprises a plastic film coated with a barrier. 10. The variable buoyancy system of claim 8 , wherein the ballonet comprises a plastic film coated with a barrier is foldable for insertion into the envelope. 11. The variable buoyancy system of claim 4 , wherein the spheroid body is an oblate spheroid. 12. The variable buoyancy system of claim 11 , wherein the envelope has a corresponding oblate spheroid shape such that when inflated, at least a portion of the outer surface of the spheroid body conforms with the inner surface of the envelope.
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