Outer membrane for aerial vehicles
Aspects of the disclosure relate to an aerial vehicle. The aerial vehicle may include an envelope having a plurality of tendons and formed from a first plurality of gores. The aerial vehicle may also include one or more ballonets arranged within the envelope. An outer membrane may be arranged around at least part of the envelope and formed from a second plurality of gores. The outer membrane may include at least one panel attached at one side to the outer membrane between a pair of the second plurality of gores and attached at an opposite side to the envelope. The outer membrane may be arranged to improve aerodynamics of the envelope when the aerial vehicle is in flight.
1. An aerial vehicle comprising:
an envelope having a plurality of tendons and formed from a first plurality of gores;
one or more ballonets arranged within the envelope;
an outer membrane arranged around at least part of the envelope and formed from a second plurality of gores; and
at least one panel attached at one side to the outer membrane between a pair of the second plurality of gores and attached at an opposite side to the envelope, and wherein the outer membrane is arranged to improve aerodynamics of the envelope when the aerial vehicle is in flight.
2. The aerial vehicle of claim 1 , wherein the envelope includes lateral and longitudinal tendons, and wherein the opposite side is attached to one of the lateral tendons.
3. The aerial vehicle of claim 1 , wherein the outer membrane is formed from a first material of a first thickness, and wherein the envelope is formed from the first material of a second thickness, the first thickness being less than the second thickness.
4. The aerial vehicle of claim 1 , wherein the outer membrane is formed from a first material of a first thickness, and wherein the envelope is formed from a second material, the first material being different from the second material.
5. The aerial vehicle of claim 1 , wherein the envelope is a pumpkin shaped envelope.
6. The aerial vehicle of claim 5 , wherein the outer membrane is attached to a top end plate of the envelope.
7. The aerial vehicle of claim 6 , wherein the outer membrane is sealed completely around the top end plate.
8. The aerial vehicle of claim 6 , wherein the outer membrane is sealed partially around the top end plate such that air may pass between the top end plate and the outer membrane and between the outer membrane and the envelope.
9. The aerial vehicle of claim 6 , wherein the outer membrane is attached to a bottom end plate of the envelope.
10. The aerial vehicle of claim 1 , wherein the envelope is a prolate spheroid shaped envelope.
11. The aerial vehicle of claim 10 , wherein the outer membrane is attached to an end plate of the envelope.
12. The aerial vehicle of claim 11 , wherein the outer membrane is sealed completely around the end plate.
13. The aerial vehicle of claim 11 , wherein the outer membrane is sealed partially around the end plate such that air may pass between the end plate and the outer membrane and between the outer membrane and the envelope.
14. The aerial vehicle of claim 11 , wherein the outer membrane is attached to a second end plate of the envelope.
15. The aerial vehicle of claim 1 , wherein the envelope is an airship shaped envelope.
16. The aerial vehicle of claim 15 , wherein the outer membrane is attached to a forward end plate of the envelope.
17. The aerial vehicle of claim 16 , wherein the outer membrane is sealed completely around the forward end plate.
18. The aerial vehicle of claim 16 , wherein the outer membrane is sealed partially around the forward end plate such that air may pass between the forward end plate and the outer membrane and between the outer membrane and the envelope.
19. The aerial vehicle of claim 16 , wherein the outer membrane is attached to a rearward end plate of the envelope.
20. The aerial vehicle of claim 1 , wherein the outer membrane is configured to stretch over the envelope when the envelope is pressurized.