Propulsive assembly, in particular for an aircraft, for protection against an unbalance force and method of protection
US-2022348314-A1 · Nov 3, 2022 · US
US9828081B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-9828081-B1 |
| Application number | US-201414227096-A |
| Country | US |
| Kind code | B1 |
| Filing date | Mar 27, 2014 |
| Priority date | Mar 27, 2013 |
| Publication date | Nov 28, 2017 |
| Grant date | Nov 28, 2017 |
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A balloon is provided having an exostructure comprised of hollow struts or rods and an envelope positioned over the exostructure, and a pump for pumping air out of the balloon to create an air pressure differential between the pressure inside the envelope and the atmospheric pressure outside the envelope, a control system configured to allow air to flow into the envelope to control the altitude of the balloon, and to operate the pump to pump air out of the envelope to control the altitude of the balloon, wherein the material of the envelope is arranged so as to sag between the struts or rods and form at least one catenary surface when there is an air pressure differential between the pressure inside of the balloon envelope and the atmospheric pressure outside the envelope.
Opening claim text (preview).
What is claimed is: 1. A balloon, comprising: an exostructure comprised of hollow struts or rods; an envelope material positioned over the exostructure; a pump for pumping air out of the balloon to create an air pressure differential between the pressure inside the envelope and atmospheric pressure outside the envelope; a control system configured to: allow air to flow into the envelope to control the altitude of the balloon; and operate the pump to pump air out of the envelope to control the altitude of the balloon; wherein the exostructure is comprised of triangles formed by the hollow struts or rods; and wherein the envelope material is comprised of a plurality of sections; where each section is sized in an amount greater in size than the triangles and is positioned over a triangle, where the sections of the envelope material have a generally rounded shape that is used to extend between the struts or rods of a triangle such that each section of the envelope material is arranged so as to sag between the struts or rods of a triangle before attachment to an adjacent section, and before a vacuum is applied. 2. The balloon of claim 1 , wherein the exostructure is comprised of equilateral triangles formed by the hollow struts or rods. 3. The balloon of claim 1 , wherein the hollow struts or rods are comprised of thin-walled carbon fiber tubes having an outer diameter of 2-3 centimeters. 4. The balloon of claim 3 , wherein the hollow struts or rods are on the order of 10 centimeters+/−50 percent in length. 5. The balloon of claim 1 , wherein the envelope material is comprised of thermoplastic film. 6. The balloon of claim 1 , wherein after the envelope material has been placed over the hollow struts or rods, the envelope material has been stretched prior to being finally attached to the exostructure. 7. The balloon of claim 6 , wherein after the envelope material has been placed over the hollow struts or rods, the envelope material has been heated prior to being finally attached to the exostructure. 8. The balloon of claim 1 , further including a bladder that may contain a lighter-than-air gas to provide additional buoyant force to the balloon. 9. A vessel comprising: a plurality of balloons attached to or positioned within the vessel, wherein the plurality of balloons are each comprised of: an exostructure comprised of hollow struts or rods; an envelope positioned over the exostructure; a pump for pumping air out of the balloon to create an air pressure differential between the pressure inside the envelope and the atmospheric pressure outside the envelope; a control system configured to: allow air to flow into the envelope to control the altitude of the balloon; and operate the pump to pump air out of the envelope to control the altitude of the balloon; wherein the exostructure is comprised of triangles formed by the hollow struts or rods; wherein the envelope material is comprised of a plurality of sections; where each section is sized in an amount greater in size than the triangles and is positioned over a triangle, where the sections of the envelope material have a generally rounded shape that is used to extend between the struts or rods of a triangle such that each section of the envelope material is arranged so as to sag between the struts or rods of a triangle before attachment to an adjacent section, and before a vacuum is applied; and wherein air may be pumped out of the balloon envelope, or introduced into the balloon envelope, to control the altitude of the vessel. 10. The vessel of claim 9 , where the exostructure is comprised of equilateral triangles formed by the hollow struts or rods. 11. The vessel of claim 9 , wherein the hollow struts or rods are comprised of thin-walled carbon fiber tubes having an outer diameter of 2-3 centimeters. 12. The vessel of claim 9 , wherein the plurality of balloons have an envelope material comprised of thermoplastic film. 13. A method, comprising: providing a balloon having an exostructure comprised of hollow struts or rods, an envelope material positioned over the exostructure, a pump for pumping air out of the balloon to create an air pressure differential between the pressure inside the envelope and atmospheric pressure outside the envelope, a control system configured to allow air to flow into the envelope to control the altitude of the balloon, and operate the pump to pump air out of the envelope to control the altitude of the balloon, wherein the exostructure is comprised of triangles formed by the hollow struts or rods; and wherein the envelope material is comprised of a plurality of sections; where each section is sized in an amount greater in size than the triangles and is positioned over a triangle, where the sections of the envelope material have a generally rounded shape that is used to extend between the struts or rods of a triangle such that each section of the envelope material is arranged so as to sag between the struts or rods of a triangle before attachment to an adjacent section, and before a vacuum is applied; controlling the altitude of the balloon by:; pumping air out of the envelope to increase an air pressure differential between the pressure within the envelope and the atmospheric pressure outside the envelope to provide a more buoyant upward force and increase the altitude of the balloon; and pumping or letting air into the envelope to decrease the air pressure differential between the pressure within the envelope and the atmospheric pressure outside the envelope to provide a less buoyant upward force and decrease the altitude of the balloon. 14. The method of claim 13 , wherein the exostructure is comprised of equilateral triangles formed by the hollow struts or rods. 15. The method of claim 13 , wherein the hollow struts or rods are comprised of thin-walled carbon fiber tubes having an outer diameter of 2-3 centimeters. 16. The method of claim 15 , wherein the hollow struts or rods are on the order of 10 centimeters in length.
Controlling gas pressure, heating, cooling, or discharging gas · CPC title
Rigid airships; Semi-rigid airships (B64B1/58 takes precedence) · CPC title
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adapted to maintain predetermined altitude · CPC title
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