Heat exchanger

公开(公告)号:
GB202002302D0
公开(公告)日:
2020-04-01
申请号:
GB2020002302
申请日:
2020-02-19
授权日:
-
受理局:
英国
专利类型:
发明申请
简单法律状态:
有效
法律状态/事件:
授权
IPC分类号:
-
战略新兴产业分类:
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国民经济行业分类号:
-
当前申请(专利权)人:
REACTION ENGINES LIMITED
原始申请(专利权)人:
REACTION ENGINES LIMITED
当前申请(专利权)人地址:
Building F5, Culham Science Centre, ABINGDON, Oxfordshire, OX14 3DB, United Kingdom
工商统一社会信用代码:
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工商登记状态:
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工商注册地址:
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工商成立日期:
1989-01-01
工商企业类型:
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发明人:
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代理机构:
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代理人:
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摘要:
A shell and tube type heat exchanger 1 comprising a shell 2 and a tube arrangement 5 located within the shell. The tube arrangement has a flow tube 6, 8 that furcates at a plurality of nodes along its length and may further furcate into sub-tubes 18, 19 at these aligned nodes in a fractal or quasi-fractal form. The shell and tube type heat exchanger further comprise a tube matrix 13 fluidly coupled to the flow tube; the tube matrix being made of parallel tubes. The heat exchanger may feature a plurality of tube modules 9 that are formed into a ring structure with an aperture through the centre of the ring, with a plug 16 provided in the aperture.
技术问题语段:
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技术功效语段:
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权利要求:
CLAIMS 9. A shell and tube type heat exchanger comprising: a shell; a tube arrangement within said shell, said tube arrangement comprising a flow tube, wherein said flow tube furcates at a plurality of nodes along its length; and a tube matrix fluidly coupled to said flow tube. 2. A shell and tube type heat exchanger of claim 1 wherein at a respective node, the flow tube furcates into a plurality of sub-tubes. 3. A shell and tube type heat exchanger of any of the preceding claims wherein said tube arrangement is formed as a tube module. 4. A shell and tube type heat exchanger of claim 3 wherein the heat exchanger comprises a plurality of tube modules. S. A shell and tube type heat exchanger of claim 4, wherein the plurality of tube modules are arranged about a rotational axis of the shell. 6. A shell and tube type heat exchanger of claim 5 wherein the plurality of tube modules form a generally ring shaped structure. 7. A shell and tube type heat exchanger of claim 6 wherein the ring-shaped structure comprises an aperture defined therethrough and wherein a plug is provided in said aperture. 8. A shell and tube type heat exchanger of any preceding claim when dependent on claim 3, wherein said tube matrix is provided in said module. 9. A shell and tube type heat exchanger of any of the preceding claims wherein the tube matrix comprises a plurality of generally parallel tubes. 10. A shell and tube type heat exchanger of any of the preceding claims wherein at the downstream side of the tube matrix each flow tube consolidates at a plurality of nodes along its length. 11. A shell and tube type heat exchanger of any of the preceding claims wherein the tube matrix is located between and fluidly connected to a furcating tube section or manifold and a consolidating tube section or manifold. 12. A shell and tube type heat exchanger according to claim 11, wherein the furcating tube section is substantially similar in form to the consolidating tube section. 13. A shell and tube type heat exchanger according to any of the preceding claims wherein progressive furcation of the flow tubes into sub-tubes at node points along the length of the flow tube has a fractal or quasi-fractal form. 14. A shell and tube type heat exchanger according to any of the preceding claims, wherein the internal cross-sectional area of the flow tube remains constant or generally constant through a furcation or branching node. 15. A shell and tube type heat exchanger according to any of the preceding claims, wherein the flow tube successively furcates into sub-tubes at nodes which are aligned. 16. A shell and tube type heat exchanger according to claim 15, wherein the respective nodes at which furcation or branching occurs in each sub-tube may be aligned in a common flat plane extending generally perpendicular to the extent of the sub-tubes. 17. A shell and tube type heat exchanger according to claim 15, wherein the respective nodes at which furcation or branching occurs in each sub-tube may be aligned in a curved plane. 18. A shell and tube type heat exchanger according to any of the preceding claims, wherein supporting fins or ribs may be provided at spaced or staggered intervals between adjacent tubes within the matrix. 19. A shell and tube type heat exchanger of any of the preceding claims, wherein a portion of the flow tube arrangement includes a helical tube. 20. A shell and tube type heat exchanger of any of the preceding claims, wherein: the shell is rounded, for example spherical. 21. The shell and tube type heat exchanger of any of the preceding claims wherein the inlet of the shell is in fluid communication with the inner volume of the shell via a diffuser. 22. A shell and tube type heat exchanger of any of preceding claims wherein the shell comprises a thermal liner which substantially conforms to an inner surface of the shell. 23. A shell and tube type heat exchanger of any of the preceding claims, wherein the flow tube has substantially teardrop-like cross section between nodes. 24. A shell and tube type heat exchanger of any of the preceding claims, wherein one or more baffles are provided within said shell providing support to the flow tube and/or tube arrangement. 25. A shell and tube type heat exchanger of any of the preceding claims, wherein the matrix has a curved or circular perimeter. 26. A shell and tube type heat exchanger of any of the preceding claims, wherein the matrix includes a shell adjoining its perimeter. 27. A shell and tube type heat exchanger of any of the preceding claims, wherein the flow tube and matrix are integrally formed, for example, using an additive manufacturing technique. 28. A method of operating a shell and tube type heat exchanger according to any of claims 1 to 27, including the steps of: supplying a heatant or coolant to the shell to fill said shell; and supplying a fluid to the tube arrangement in said shell. 29. A method of operating a shell and tube type heat exchanger according to claim 29, wherein a bleed flow of the heatant or coolant may be supplied to a thermal liner. 30. An engine or vehicle comprising a shell and tube type heat exchanger according to any of claims 1to 27.
技术领域:
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背景技术:
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发明内容:
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具体实施方式:
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