초록 ▼

This invention relates to the field of buoyant aircraft and operation thereof, in particular, airships with improved stability. The present invention is directed to non-rigid, non-spherical airships having an envelop contained within the airship and at least one further envelop contained therein for

This invention relates to the field of buoyant aircraft and operation thereof, in particular, airships with improved stability. The present invention is directed to non-rigid, non-spherical airships having an envelop contained within the airship and at least one further envelop contained therein for holding a volume of lifting gas.

대표청구항 ▼

I claim: 1. A method for operating an airship, the method comprising the steps of: providing a non-rigid, non-spherical airship having a weight and an outer envelope defining a hull having a first volume, said airship having a propulsion system and a directional control system, said airship also ha

I claim: 1. A method for operating an airship, the method comprising the steps of: providing a non-rigid, non-spherical airship having a weight and an outer envelope defining a hull having a first volume, said airship having a propulsion system and a directional control system, said airship also having a second envelope contained within the first volume and the second envelope having a second volume; and a third envelope contained within the second volume and having a third volume for holding lifting gas; said third envelope being expandable within said second envelope to a maximum predetermined volume, inflating said second envelope with a gas having a density greater than said lifting gas; and partially inflating the third envelope with a mass of said lifting gas, thereby permitting the expansion and contraction of the third envelope within the second envelope as the lifting gas expands and contracts during operation, whilst maintaining said mass of said lifting gas within said third envelope during said expansion and contraction; wherein the volume occupied by the lifting gas is sufficient to balance said weight. 2. The method of claim 1 wherein the first envelope provides for fluid communication between the first volume and an exterior of the airship. 3. The method of claim 2 wherein the second envelope provides for fluid communication between the second volume and the first volume. 4. The method of claim 1 wherein a portion of the second volume not containing the third envelope decreases with the expansion of the lifting gas contained within the third envelope, and the sum of the portion of the second volume not containing the third envelope and the volume of the third envelope remains generally constant. 5. The method of claim 1 further comprising the step of operating said airship to a location greater than 10,000 ft above mean sea level. 6. The method of claim 1 wherein the volume occupied by the lifting gas at mean sea level is less than 1/19th of said maximum predetermined volume of said third envelope.