초록 ▼

Various embodiments of the invention relate generally to systems for providing active vertical control of an airship. More particularly, at least one embodiment of the invention relates to a system for actively controlling the aerostatic lift of an airship by manipulating the ratio of air to lifting

Various embodiments of the invention relate generally to systems for providing active vertical control of an airship. More particularly, at least one embodiment of the invention relates to a system for actively controlling the aerostatic lift of an airship by manipulating the ratio of air to lifting gas contained within the airship, and thus the overall mass of the airship. This manipulation is accomplished by actively compressing and/or decompressing the lifting gas or internal air, with the resulting pressure differential borne primarily by the hull and/or an internal pressure tank depending upon the configuration.

대표청구항 ▼

What is claimed is: 1. A system for controlling the aerostatic lift of an airship, comprising: a self-supporting monocoque hull made of a gas-impermeable material and containing a first gas under an internal pressure greater than an external pressure outside the self-supporting monocoque hull; a c

What is claimed is: 1. A system for controlling the aerostatic lift of an airship, comprising: a self-supporting monocoque hull made of a gas-impermeable material and containing a first gas under an internal pressure greater than an external pressure outside the self-supporting monocoque hull; a compartment located within the self-supporting monocoque hull and containing a second gas; a first device coupled to the compartment to control a flow of the second gas into the compartment to increase the static weight of the compartment and to increase the internal pressure and out of the compartment to decrease the static weight of the compartment and to decrease the internal pressure; at least two propulsion devices positioned at opposite ends of the self-supporting monocoque hull; and a cabin coupled to the self-supporting monocoque hull, the cabin does not provide structural support to the self supporting monocoque hull. 2. The system of claim 1 wherein the self-supporting monocoque hull has a fixed-volume. 3. The system of claim 1 wherein the first gas is lighter than the second gas. 4. The system of claim 1 wherein the first gas is helium and the second gas is air. 5. The system of claim 1 wherein the compartment is a fixed-volume tank. 6. The system of claim 1 wherein the compartment is a flexible compartment. 7. The system of claim 1 wherein the first device is a valve. 8. The system of claim 1 wherein the first device is a pump. 9. The system of claim 1 further comprising a tank configured to contain at least a portion of the first gas. 10. The system of claim 9 further comprising a second device coupled to the tank to control a flow of the first gas into the tank to decrease the static weight of the tank and out of the tank to increase the static weight of the tank. 11. The system of claim 10 wherein the second device is a valve. 12. The system of claim 10 wherein the second device is a pump. 13. A system for controlling the aerostatic lift of an airship, comprising: a self-supporting monocoque hull having an inner surface and configured to hold a lifting gas under a pressure greater than atmospheric pressure, the lifting gas being in contact with the inner surface of the self-supporting monocoque hull; a flexible compartment contained within the self-supporting monocoque hull and configured to hold air; a first device coupled to the flexible compartment for allowing air into the flexible compartment to expand the flexible compartment and increase the pressure of the lifting gas and for removing air from the flexible compartment to contract the flexible compartment and decrease the pressure of the lifting gas; and a cabin coupled to the self-supporting monocoque hull, the cabin does not provide structural support to the self-supporting monocoque hull. 14. The system of claim 13 wherein the flexible compartment is positioned on a bottom surface of the self-supporting monocoque hull. 15. The system of claim 13 wherein the flexible compartment is made of a gas-impermeable material and has a toroidal shape. 16. The system of claim 13 further comprising one or more baffles positioned within the flexible compartment to partition the flexible compartment into one or more sections, for providing support and stability to the flexible compartment, and for regulating the air flow between the one or more sections. 17. The system of claim 13 wherein the first device is selected from a group consisting of a controller, a pump, a valve, and combinations thereof. 18. The system of claim 13 further comprising a tank configured to hold at least a potion of the lifting gas. 19. The system of claim 18 further comprising a second device coupled to the tank to control a flow of the lifting gas from the self-supporting monocoque hull to the tank to increase the pressure of the lifting gas in the tank and from the tank to the self-supporting monocoque hull to decrease the pressure of the lifting gas in the tank. 20. A system for controlling the aerostatic lift of an airship, comprising: a self-supporting monocoque hull made of a gas-impermeable material arid configured to hold a lifting gas; a first flexible compartment contained within the self-supporting monocoque hull and configured to hold air that is above atmospheric pressure; a first outlet device for releasing air from the first flexible compartment to decrease the static weight of the airship; a first inlet device for introducing air into the first flexible compartment to increase the static weight of the airship; and a cabin coupled to the self-supporting monocoque hull, the cabin does not provide structural support to the self-supporting monocoque hull. 21. The system of claim 20 wherein the first outlet device is a valve and the first inlet device is a pump. 22. The system of claim 20 further comprising a second flexible compartment contained within the self-supporting monocoque hull and configured to hold air. 23. The system of claim 22 further comprising: a second outlet device for releasing air from the second flexible compartment to decrease the static weight of the airship; and a second inlet device for introducing air into the second flexible compartment to increase the static weight of the airship. 24. The system of claim 20 further comprising a tank positioned within the self-supporting monocoque hull. 25. The system of claim 24 further comprising a device coupled to the tank to control a flow of the lifting gas from the self-supporting monocoque hull to the tank to increase the pressure of the lifting gas in the tank and from the tank to the self-supporting monocoque hull to decrease the pressure of the lifting gas in the tank. 26. The system of claim 24 further comprising a device coupled to the tank to control a flow of air into the tank to increase the static weight of the airship and out of the tank to decrease the static weight of the airship. 27. A system for controlling the aerostatic lift of an airship, comprising: a single lenticular self-supporting hull made of a gas-impermeable material and containing a first gas under an internal pressure greater than an external pressure outside the single lenticular self-supporting hull; a compartment located within the single lenticular self-supporting hull and containing a second gas; a first device coupled to the compartment to control a flow of the second gas into the compartment to increase the static weight of the compartment and to increase the internal pressure and out of the compartment to decrease the static weight of the compartment and to decrease the internal pressure; at least two propulsion devices positioned at opposite ends of the single lenticular self-supporting hull; and a cabin coupled to the single lenticular self-supporting hull, the cabin does not provide structural support to the single lenticular self-supporting hull. 28. The system of claim 27 further comprising a tank configured to contain at least a portion of the first gas. 29. The system of claim 28 further comprising a second device coupled to the tank to control a flow of the first gas into the tank to decrease the static weight of the tank and out of the tank to increase the static weight of the tank. 30. The system of claim 27 wherein the first device is selected from a group consisting of a controller, a pump, a valve, and combinations thereof.