Fill port for a balloon
US-9643707-B1 · May 9, 2017 · US
US10322789B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10322789-B2 |
| Application number | US-201715797273-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 30, 2017 |
| Priority date | Apr 10, 2014 |
| Publication date | Jun 18, 2019 |
| Grant date | Jun 18, 2019 |
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Official abstract text for this publication.
High-altitude balloons and apparatuses for filling such high-altitude balloons are provided. As an example, an apparatus for filling a high-altitude balloon includes a tube extending through envelope material of the balloon is provided. The apparatus also includes a flange connected to a first end of the tube. The flange is connected to an interior surface of the balloon. A fitting is connected to a second end of the tube. The fitting is configured for attachment with an apparatus for filling the balloon with lift gas. In addition, methods of filling high-altitude balloons with lift gas and methods of manufacturing balloons are also provided.
Opening claim text (preview).
The invention claimed is: 1. A system comprising: a filling apparatus for filling a balloon, the apparatus comprising: a tube having a first end and a second end; and a plug member connected to the second end such that the tube extends through at least a portion of the plug member to provide a conduit for gas between the first end and a second end and through the plug, the plug member having a flange portion arranged around the tube, and the plug member further having at least one groove arranged around an external surface of the plug member; and an o-ring arranged in the at least one groove. 2. The system of claim 1 , wherein the flange portion corresponds to a disc with a lip that extends outwardly relative to a surface of the plug member in which the at least one groove is arranged. 3. The system of claim 1 , wherein the tube is comprised of a first metal and the plug member is comprised of a second metal. 4. The system of claim 3 , wherein the tube is comprised of copper. 5. The system of claim 3 , wherein the plug member is comprised of stainless steel. 6. The system of claim 3 , wherein the first metal is different from the second metal. 7. The system of claim 1 , wherein the materials of the o-ring and plug member are selected to compensate for changing dimensions of the materials at predetermined temperatures. 8. The system of claim 1 , wherein the tube is configured for cold welding to seal lift gas in the balloon. 9. The system of claim 1 , wherein the plug member includes a second groove arranged between the first groove and the flange. 10. The system of claim 8 , further comprising a second O-ring arranged in the second groove. 11. The system of claim 10 , wherein high vacuum grease is arranged on the O-ring and the second O-ring. 12. The system of claim 10 , wherein each of the O-ring and the second O-ring includes flourosilicone in order to reduce shrinkage of the each of the O-rings at a predetermined altitude. 13. The system of claim 10 , wherein the at least one groove and the second groove extends around a complete circumference of the plug member. 14. The system of claim 10 , wherein the at least one groove and the second groove are arranged parallel to one another on the plug member. 15. The system of claim 10 , wherein the at least one groove and the second groove are arranged below a first side of the flange and the tube extends above a second side of the flange, the first side is opposite of the second side. 16. The system of claim 1 , further comprising a fitting attached to the first end, the fitting is configured for attachment to a filling apparatus. 17. The system of claim 16 , wherein the fitting is braze welded to the first end. 18. The system of claim 1 , wherein the filling apparatus is configured for attachment to a top plate of a balloon envelope such that the first end extends away from the balloon envelope. 19. The system of claim 1 , wherein each of the O-ring includes flourosilicone in order to reduce shrinkage of the each of the O-rings at a predetermined altitude. 20. The system of claim 10 , wherein high vacuum grease is arranged on the O-ring.
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