Regeneration cooler of ramjet engine, and manufacturing method of the same

US11512852B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11512852-B2
Application numberUS-201716498033-A
CountryUS
Kind codeB2
Filing dateNov 16, 2017
Priority dateApr 10, 2017
Publication dateNov 29, 2022
Grant dateNov 29, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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 ).

First claim

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.

Assignees

Inventors

Classifications

  • 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

  • F02C7/224Primary

    Heating fuel before feeding to the burner · CPC title

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Frequently asked questions

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What does patent US11512852B2 cover?
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 passa…
Who is the assignee on this patent?
Mitsubishi Heavy Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F02C7/224. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 29 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).