초록 ▼

One embodiment of the invention provides an airship having an outer tube formed in the shape of a toroid and defining a central opening, a first compartment positioned within the outer tube and containing a first gas, and a second compartment positioned within the outer tube and containing a second

One embodiment of the invention provides an airship having an outer tube formed in the shape of a toroid and defining a central opening, a first compartment positioned within the outer tube and containing a first gas, and a second compartment positioned within the outer tube and containing a second gas. The airship may also include top and bottom covers further defining and enclosing the central opening, the central opening containing the second gas, and a controller that controls the flow of the first gas into and out of the first compartment to actively control the ascent and descent of the airship.

대표청구항 ▼

What is claimed is: 1. An airship comprising: an outer tube formed in the shape of a toroid and defining a central space; a first compartment positioned within the outer tube and containing a first gas; a second compartment positioned within the outer tube and containing a second different gas; top

What is claimed is: 1. An airship comprising: an outer tube formed in the shape of a toroid and defining a central space; a first compartment positioned within the outer tube and containing a first gas; a second compartment positioned within the outer tube and containing a second different gas; top and bottom covers further defining and enclosing the central space, the central space containing the second gas; and a controller that controls the flow of the first gas into and out of the first compartment to actively control the ascent and descent of the airship. 2. The airship of claim 1 wherein the outer tube is made of a flexible membrane material. 3. The airship of claim 1 wherein the first compartment and the second compartment are made of a gas-impermeable flexible material. 4. The airship of claim 1 wherein the first compartment is a bag made of a gas-impermeable, flexible, inelastic material. 5. The airship of claim 1 wherein the second compartment is a bag made of a gas-impermeable, flexible, inelastic material. 6. The airship of claim 1 wherein the first gas is air and the second gas is helium. 7. The airship of claim 1 wherein the top cover is circumferentially coupled to a top portion of the outer tube and the bottom cover is circumferentially coupled to a bottom portion of the outer tube. 8. The airship of claim 7 wherein the top cover is circumferentially coupled to the top portion using an adhesive and the bottom cover is circumferentially coupled to the bottom portion using an adhesive. 9. The airship of claim 1 wherein the top and bottom covers are made of a rigid composite material or a gas-impermeable, flexible, inelastic material. 10. The airship of claim 1 further comprising a third compartment positioned within the central space and containing the first gas. 11. The airship of claim 1 further comprising a fourth compartment positioned within the central space and containing the second gas. 12. The airship of claim 1 wherein the airship has a lenticular shape and does not have any internal structural support members to maintain the lenticular shape. 13. The airship of claim 1 further comprising a blower configured to maintain the shape of the top and bottom covers. 14. An airship comprising: an outer tube formed in the shape of a toroid and containing a first gas within a first compartment that is pressurized to a pressure greater than atmospheric pressure, the outer tube defining a central space; a second compartment positioned within the outer tube and containing a second different gas; top and bottom covers attached to the outer tube and further defining and enclosing the central space, the central space containing the first gas; a third compartment positioned within the central space and containing the second gas; and a control device that controls the flow of the second gas into and out of the second compartment or third compartment to actively control the ascent and descent of the airship. 15. The airship of claim 14 wherein the outer tube is made of a flexible membrane material. 16. The airship of claim 14 wherein the second compartment and the third compartment are made of a gas-impermeable flexible material. 17. The airship of claim 14 wherein the second compartment is a bag made of a gas-impermeable, flexible, inelastic material. 18. The airship of claim 14 wherein the third compartment is a bag made of a gas-impermeable, flexible, inelastic material. 19. The airship of claim 14 wherein the first gas is helium and the second gas is air. 20. The airship of claim 14 wherein the top cover is circumferentially coupled to a top portion of the outer tube and the bottom cover is circumferentially coupled to a bottom portion of the outer tube. 21. The airship of claim 20 wherein the top cover is circumferentially coupled to the top portion using an adhesive and the bottom cover is circumferentially coupled to the bottom portion using an adhesive. 22. The airship of claim 14 wherein the top and bottom covers are made of a gas-impermeable, flexible, inelastic material. 23. The airship of claim 14 further comprising a first valve coupled to the second compartment to control the flow of the second gas into and out of the second compartment. 24. The airship of claim 14 further comprising a second valve coupled to the third compartment to control the flow of the second gas into and out of the third compartment. 25. The airship of claim 14 wherein the airship has a lenticular shape and does not have any internal structural support members to maintain the lenticular shape. 26. The airship of claim 14 further comprising a blower positioned within the central central space and configured to maintain the shape of the top and bottom covers. 27. The airship of claim 14 further comprising a plurality of propellers coupled to the outer tube to provide yaw control to the airship. 28. The airship of claim 14 further comprising a first catenary cable connected to the top cover and the outer tube and a second catenary cable connected to the bottom cover and the outer tube.