Fuel supply system, scramjet engine and method for operating the same
US-10190540-B2 · Jan 29, 2019 · US
US11512852B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11512852-B2 |
| Application number | US-201716498033-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 16, 2017 |
| Priority date | Apr 10, 2017 |
| Publication date | Nov 29, 2022 |
| Grant date | Nov 29, 2022 |
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A regeneration cooler ( 2 ) includes a passage forming structure ( 10 ) in which a fuel passage ( 11 ) is formed for liquid fuel to be supplied. A coating ( 12, 12 A) is formed in the fuel passage ( 11 ) to at least partially cover a wall surface of the fuel passage ( 11 ). The coating ( 12, 12 A) contains metal particles ( 13 ) adhered and fixed to the wall surface ( 11 a ) of the fuel passage ( 11 ) and a coating material ( 14, 17 ).
Opening claim text (preview).
The invention claimed is: 1. A method of manufacturing a regeneration cooler of a ramjet engine the regeneration cooler comprising a plurality of fuel passages through which liquid fuel comprising hydrocarbon flows, the method comprising: preparing a first metal plate; preparing a second metal plate which has a proximal section, a plurality of wall sections connected with the proximal section, and a plurality of ditches configured such that one ditch is formed between every adjacent two of the plurality of wall sections; disposing metal particles, coating material particles, and a binder in each of the ditches, wherein the coating material particles comprise a material that controls a thermal decomposition reaction of the hydrocarbon of the liquid fuel; after the disposing of the metal particles, the coating material particles and the binder in the ditches, arranging the first metal plate on the second metal plate so as to close the ditches with the first metal plate; after the arranging of the first metal plate, welding the first metal plate with the wall sections of the second metal plate to form the fuel passages by closing the ditches with the first metal plate, wherein part of the metal particles in each ditch are adhered and fixed to wall surfaces of the fuel passages by heat caused by the welding; and removing part of the metal particles and the coating material particles which are not adhered and fixed to the wall surfaces of the fuel passages formed by closing the ditches by the first metal plate. 2. A method of manufacturing a regeneration cooler of a ramjet engine, the regeneration cooler comprising a plurality of fuel passages through which liquid fuel comprising hydrocarbon flows, the method comprising: preparing a first metal plate; preparing a second metal plate which has a proximal section, a plurality of wall sections connected with the proximal section, and a plurality of ditches configured such that one ditch is formed between every adjacent two of the plurality of wall sections; disposing metal particles in each of the ditches; after the disposing of the metal particles in each of the ditches, arranging the first metal plate on the second metal plate so as to close the ditches with the first metal plate; after the arranging of the first metal plate, welding the first metal plate with the wall sections of the second metal plate to form the fuel passages by closing the ditches with the first metal plate, wherein part of the metal particles in each ditch are adhered and fixed to wall surfaces of the fuel passages by heat caused by the welding; and forming a coating material to at least partially cover the wall surfaces of the fuel passages and the metal particles adhered and fixed to the wall surfaces, the coating material controlling a thermal decomposition reaction of the hydrocarbon of the liquid fuel. 3. The method of manufacturing a regeneration cooler according to claim 2 , wherein the coating material contains a material which restrains thermal decomposition reaction of liquid fuel, compared with materials of the first metal plate and the second metal plate. 4. The method of manufacturing a regeneration cooler according to claim 2 , wherein the coating material contains at least one of silica, alumina and zirconia. 5. The method of manufacturing a regeneration cooler according to claim 2 , wherein the coating material contains a catalyst which promotes thermal decomposition reaction of liquid fuel. 6. The method of manufacturing a regeneration cooler according to claim 2 , wherein the metal particles are formed of a same material as that of the first metal plate and the second metal plate.
characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines · CPC title
by the provision of a heat exchanger within the cooling circuit · CPC title
in ram-jet engines or ram-jet driven vehicles · CPC title
Efficient propulsion technologies, e.g. for aircraft · CPC title
Heating fuel before feeding to the burner · CPC title
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