Hanson-Haber aircraft enhine for the production of stratospheric compounds and for the creation of atmospheric reflectivity and absorption...

公开(公告)号：
GB202104525D0
公开(公告)日：
2021-05-12
申请号：
GB2021004525
申请日：
2021-03-30
授权日：
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受理局：
英国
专利类型：
发明申请
简单法律状态：
失效
法律状态/事件：
撤回-未指定类型
IPC分类号：
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战略新兴产业分类：
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国民经济行业分类号：
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当前申请(专利权)人：
MATTHEW VERNON HANSON
原始申请(专利权)人：
MATTHEW VERNON HANSON
当前申请(专利权)人地址：
74 Foster Street #3, Cambridge, Massachusetts, 02138, United States of America
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摘要：
Modifying existing commercial jet engine technology to leverage the temperature and pressure available in the combustion of kerosene A-1 jet fuel (or other fuels) to include the Haber process (or other industrial processes requiring high temperatures and high pressures) presents possibilities for the creation of ammonia and other down-stream compounds suitable for atmospheric seeding of reflective or absorptive compounds. Compounds such as ammonia and urea (or other compounds—as time goes on) provide alternatives to high-altitude (20 km) seeding of sulfur dioxide (which is destructive to atmosphere, vegetation, and ozone alike). Additionally, the changes required to existing engine technology analogous to adding a catalytic converter to the exhaust system of a car, provide, through the leveraging of the strong chemical bond of atmospheric nitrogen (N2), additional overall energy output to the engine system (through heat) and the production of a potentially combustible liquid or gas (ammonia and downstream ammonia compounds or other compounds) which may be used as a downstream fuel source by the engine itself.
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权利要求：
Claims An aircraft engine modification consisting of a ring of structures containing Haber Processes surrounding and lying longitudinally along the high pressure and high temperature area of an aircraft engine consisting of two cooperating pathways: Pathway A (particulate dispersion), wherein a) an initial Haber Process would lead to b) a higher temperature, higher pressure, higher efficiency Haber Process sitting above it with c) both Haber processes leading to, d) an ammonia bypass chamber, e) a Urea production chamber (CO2 + NH3), f) a Urea distillation chamber and flash drum and/or vacuum evaporator and g) a miniature Prilling tower where various sections could be combined or repurposed for the different steps in the Urea production process, and where the entire pathway would produce a mixture of Ammonia and Urea which can be ejected into the aircraft engine contrail, and Pathway B (thrust) which would be identical to Pathway A except instead of structures dedicated to Urea production there would be h) an ammonia combustion chamber, i) a nitrous oxide creation chamber which could either be ported directly into j) the main combustion area of the engine via nozzles or k) into a secondary (Jet A, ammonia/methane mix, or other fuels) combustion chamber which produces thrust.
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