US2024076246A1PendingUtilityA1
Solvated metal fuel combustion system and method
Est. expiryMay 31, 2042(~15.8 yrs left)· nominal 20-yr term from priority
Inventors:Steven F. SonCaleb Nathaniel HarperRyan Tolman MerrellAndrew Ryan NoelDhruval Natubhai Patel
C06B 43/00C06B 33/00
52
PatentIndex Score
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Claims
Abstract
The combustion system includes a metal additive and a polar outer-sphere electron transferring solvent. The metal additive is solvated in the polar outer-sphere electron transferring solvent. The polar outer-sphere electron transferring solvent may include liquid ammonia, methylamine, and/or hexamethylphosphoramide. The metal additive may include an alkali metal and/or an alkaline earth metal. For instance, the metal additive may include lithium, sodium, aluminum, zirconium, titanium, yttrium, hafnium, and/or magnesium.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A combustion system, comprising:
a metal additive; and an outer-sphere electron transferring solvent, wherein the metal additive is solvated in the outer-sphere electron transferring solvent.
2 . The combustion system of claim 1 , wherein the outer-sphere electron transferring solvent includes liquid anhydrous ammonia.
3 . The combustion system of claim 1 , wherein the outer-sphere electron transferring solvent includes at least one of methylamine and hexamethylphosphoramide.
4 . The combustion system of claim 1 , wherein the metal additive includes at least one of an alkali metal and an alkaline earth metal.
5 . The combustion system of claim 4 , wherein the metal additive includes at least one of aluminum, zirconium, titanium, yttrium, hafnium, and magnesium.
6 . The combustion system of claim 4 , wherein the metal additive includes lithium.
7 . The combustion system of claim 4 , wherein the metal additive includes sodium.
8 . The combustion system of claim 1 , further comprising a hypergolic propellant.
9 . The combustion system of claim 8 , wherein the hypergolic propellant includes white fuming nitric acid.
10 . A propellant fuel comprising a combustion system of claim 1 .
11 . A method of manufacturing a combustion system, the method comprising the steps of:
providing an outer-sphere electron transferring solvent; providing a metal additive; and dissolving the metal additive within the outer-sphere electron transferring solvent.
12 . The method of claim 11 , further comprising a step of providing a hypergolic propellant.
13 . The method of claim 12 , further comprising a step of igniting the dissolved metal additive within the outer-sphere electron transferring solvent.
14 . The method of claim 11 , wherein the step of dissolving the metal additive within the outer-sphere electron transferring solvent utilizes an electrolysis process.
15 . The method of claim 11 , wherein the step of dissolving the metal additive within the outer-sphere electron transferring solvent utilizes a dissolution process.
16 . The method of claim 11 , wherein the step of dissolving the metal additive within the outer-sphere electron transferring solvent utilizes a radiation chemistry process.
17 . The method of claim 11 , wherein the step of dissolving the metal additive within the outer-sphere electron transferring solvent includes a reaction having the formula:
M+ m NH 3 →[M(NH 3 ) m ] + e −
18 . The method of claim 11 , wherein the metal additive is a porous metal.
19 . The method of claim 18 , wherein the step of dissolving the metal additive within the outer-sphere electron transferring solvent includes passing the outer-sphere electron transferring solvent through the porous metal.Join the waitlist — get patent alerts
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