Gas generator
US-12060031-B2 · Aug 13, 2024 · US
US12298115B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12298115-B2 |
| Application number | US-202318471828-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 21, 2023 |
| Priority date | Sep 21, 2023 |
| Publication date | May 13, 2025 |
| Grant date | May 13, 2025 |
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A vacuum insulation layer is wrapped around the length of a warhead to thermally insulate the warhead from fire or aerodynamic heating. The vacuum insulation layer may be integrally formed into the warhead casing or provided as a sleeve that may be permanently or removably positioned about the warhead casing. The vacuum insulation layer is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air.
Opening claim text (preview).
We claim: 1. A warhead, comprising: an explosive material positioned inside a warhead casing; and a vacuum insulated casing including inner and outer walls defining an annular void space around a length of the warhead casing and explosive material, wherein the annular void space is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air to form a vacuum insulation layer around the length of the warhead casing and explosive material. 2. The warhead of claim 1 , wherein the pressure in the void space is a medium vacuum between 25 Torr and 10 −3 Torr. 3. The warhead of claim 1 , wherein the pressure in the void space is a high vacuum between 10 −3 Torr and 10 −6 Torr. 4. The warhead of claim 1 , wherein Tcond_vac is less than one-fifth Tcond_air. 5. The warhead of claim 1 , wherein Tcond_vac is approximately 1/6.6 that of Tcond_air. 6. The warhead of claim 1 , wherein the warhead casing is formed of a metal material and the inner and outer walls are integrally formed with the warhead casing. 7. The warhead of claim 1 , wherein the inner and outer walls are formed as a sleeve that fits over the warhead casing. 8. The warhead of claim 7 , wherein the warhead casing wall is formed of a composite material. 9. The warhead of claim 7 , wherein the sleeve is permanently affixed to the warhead casing. 10. The warhead of claim 7 , wherein the sleeve is removable. 11. The warhead of claim 1 , wherein the warhead casing is formed of a metal material that forms a fragmentation layer, which upon detonation of the explosive material fragments with the outer wall to form a fragmentation pattern. 12. A warhead, comprising: an explosive material; and an integrally formed vacuum insulated metal warhead casing including an inner wall around a length of the explosive that forms a fragmentation layer and an outer wall that defines an annular void space, wherein the annular void space is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air to form a vacuum insulation layer around the length of the warhead casing and explosive material. 13. The warhead of claim 12 , wherein the pressure in the void space is a medium vacuum between 25 Torr and 10 −3 Torr. 14. The warhead of claim 12 , wherein the pressure in the void space is a high vacuum between 10 −3 Torr and 10 −6 Torr. 15. The warhead of claim 12 , wherein Tcond_vac is less than one-fifth Tcond_air. 16. The warhead of claim 12 , wherein upon detonation of the explosive material the fragmentation layer and outer wall fragment to form a fragmentation pattern. 17. A warhead, comprising: an explosive material positioned inside a warhead casing; and a sleeve including inner and outer walls defining an annular void space that slides around the warhead casing and explosive material, wherein the annular void space is held under vacuum with a pressure of less than 25 Torr and a thermal conductivity Tcond_vac of less than one-third of the thermal conductivity of air Tcond_air to form a vacuum insulation layer around a length of the warhead casing and explosive material. 18. The warhead of claim 17 , wherein the warhead casing wall is formed of a composite material. 19. The warhead of claim 17 , wherein the sleeve is permanently affixed to the warhead casing. 20. The warhead of claim 17 , wherein the sleeve is removable.
with fragmentation-hull construction · CPC title
characterised by the explosive material or the construction of the high explosive warhead, e.g. insensitive ammunition · CPC title
Heat shields; Thermal insulation · CPC title
Protection against overheating or radiation, e.g. heat shields; Additional cooling arrangements {(thermal protection fitted in or to cosmonautic vehicles B64G1/58)} · CPC title
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