Aluminized parachute as solar shield
View Patent ↗Aspects of the disclosure relate to fabricating high-altitude balloons having a prebuilt parachute overlying the surface of the balloon envelope to handle catastrophic envelope failures. The balloon envelope is formed from a number of gore panels. Tendons are positioned adjacent to corresponding ones of the gore panels. Each tendon is configured to carry a load caused by pressurized lifting gas within the balloon envelope. The parachute is affixed to at least some of the tendons, and covers at least a portion of the balloon envelope adjacent to the apex of the envelope. The parachute may be sewn onto the tendons. An outer surface of the parachute is covered with a UV-protective material. For instance, an aluminum coating may be vapor-deposited onto the parachute's outer surface. An IR-reflective material may cover an inner surface of the parachute.
1. A balloon structure, comprising:
a plurality of gore panels affixed to one another to form a balloon envelope, each gore panel comprising a film, a first end of each gore panel terminating at a top member along an apex of the balloon envelope, and a second end of each gore panel terminating at a base member along a bottom of the balloon envelope, wherein the balloon envelope has an upper hemisphere, a lower hemisphere and an equator therebetween;
a plurality of tendons, each tendon being positioned adjacent a corresponding one of the plurality of gore panels, each tendon being configured to carry a load caused by pressurized lifting gas within the balloon envelope; and
at least one parachute segment affixed to at least one of the plurality of tendons on the upper hemisphere of the balloon envelope, the at least one parachute segment covering at least a portion of the upper hemisphere of the balloon envelope adjacent the apex thereof, wherein the at least one parachute segment does not extend below the equator of the balloon envelope.
2. The balloon structure of claim 1 , wherein the at least one parachute segment is sewn onto the at least one of the plurality of tendons.
3. The balloon structure of claim 1 , wherein an outer surface of the at least one parachute segment facing away from the balloon envelope includes a UV light-protective material.
4. The balloon structure of claim 3 , wherein the UV light-protective material includes an aluminum coating.
5. The balloon structure of claim 3 , wherein the UV light-protective material comprises a UV blocker or a UV absorber.
6. The balloon structure of claim 3 , wherein the UV light protective material comprises a hindered amine light stabilizer.
7. The balloon structure of claim 3 , wherein an inner surface of the at least one parachute segment arranged adjacent to the balloon envelope includes an IR-light reflective material.
8. The balloon structure of claim 7 , wherein the IR light-reflective material on the inner surface of the at least one parachute segment is a reflective metallic layer.
9. The balloon structure of claim 8 , wherein the reflective metallic layer is a deposited aluminum layer.
10. A method of manufacturing a balloon structure, the method comprising:
preparing one or more gore panels on a work area, each gore panel comprising a film;
securing adjacent gore panels to one another to form a balloon envelope, a first end of each gore panel terminating at an apex of the balloon envelope, and a second end of each gore panel terminating at a base of the balloon envelope, wherein the balloon envelope has an upper hemisphere, a lower hemisphere and an equator therebetween;
securing a plurality of tendons to the balloon envelope, each tendon being positioned adjacent a corresponding one of the plurality of gore panels, each tendon being configured to carry a load caused by pressurized lifting gas within the balloon envelope; and
affixing at least one parachute segment to at least one of the plurality of tendons on the upper hemisphere of the balloon envelope, the at least one parachute segment covering at least a portion of the upper hemisphere of the balloon envelope adjacent the apex thereof, an outer surface of the at least one parachute segment facing away from the balloon envelope and an inner surface of the parachute being arranged adjacent to the balloon envelope, wherein the at least one parachute segment does not extend below the equator.
11. The method of claim 10 , wherein the at least one parachute segment is affixed by being sewn onto the at least some of the plurality of tendons.
12. The method of claim 10 , further comprising applying a UV light-protective material to the outer surface of the at least one parachute segment.
13. The method of claim 12 , wherein the UV light-protective material comprises an aluminum coating.
14. The method of claim 13 , wherein applying the UV light-protective material is done by vacuum depositing the aluminum coating onto the outer surface of the at least one parachute segment.
15. The method of claim 12 , wherein the UV light-protective material comprises a UV blocker or a UV absorber.
16. The method of claim 12 , wherein the UV light protective material comprises a hindered amine light stabilizer.
17. The method of claim 12 , further comprising applying an IR light-reflective material to the inner surface of the at least one parachute segment.
18. The method of claim 17 , wherein applying the IR light-reflective material is done by vacuum depositing an aluminum coating onto the inner surface of the at least one parachute segment.
19. The method of claim 12 , wherein the inner surface of the at least one parachute segment incorporates an IR light-reflective material.
20. The method of claim 19 , wherein the IR light-reflective material comprises a reflective metallic layer.