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51. 发明公开

EP3406997A1 ENTWINED TUBULAR ARRANGEMENTS FOR HEAT EXCHANGERS AND COUNTERFLOW HEAT TRANSFER SYSTEMS 有权
公开(公告)号：EP3406997A1
公开(公告)日：2018-11-28
申请号：EP17172935.3
申请日：2017-05-25
申请人： HS Marston Aerospace Limited
发明人： PHILLIPS, Paul , POLLARD, Berwyn
IPC分类号： F28D7/00
摘要： A counterflow heat transfer system comprises a heat exchanger and a flow controller arranged to convey a first fluid through the heat exchanger in a first flow direction and a second fluid through the heat exchanger in a second counterflow direction. The heat exchanger comprises at least one first thermally conductive tube (4) conveying the first fluid and at least one second thermally conductive tube (6a, 6b) conveying the second fluid. The first and second tubes (4, 6a, 6b) are wound around one another and in contact with one another in an entwined tubular arrangement (2).

52. 发明公开

EP3364121A1 FLOW GUIDE FOR HEAT EXCHANGER 无效
公开(公告)号：EP3364121A1
公开(公告)日：2018-08-22
申请号：EP17275021.8
申请日：2017-02-16
申请人： HS Marston Aerospace Limited
发明人： McCORMICK, John
IPC分类号： F24F13/15 , F24F13/08 , F28F9/02 , F28F13/06
CPC分类号： F28F13/06 , F24F13/082 , F28D9/0093 , F28F3/025 , F28F3/08 , F28F9/0268
摘要： There is provided a flow guide (100) for a heat exchanger structure (10), comprising one or more aerofoils (150) configured to distribute a fluid across an inlet face (40,44) of a heat exchanger structure (10).

53. 发明公开

EP3336474A1 HEAT EXCHANGER 有权
公开(公告)号：EP3336474A1
公开(公告)日：2018-06-20
申请号：EP16275174.7
申请日：2016-12-16
申请人： HS Marston Aerospace Limited
发明人： Basini, Neil
IPC分类号： F28F1/40 , F28D7/00 , F28D7/10 , F28F1/00
CPC分类号： F28F1/32 , F28D7/0008 , F28D7/10 , F28F1/003 , F28F1/36 , F28F1/40 , F28F2215/04 , F28F2250/08 , F28F2250/10
摘要： A heat exchanger comprises a conduit (16) with an interior surface (18) which defines a first flow passage (22). A first plurality of fins (26) project inwardly from the interior surface (18) of the conduit (16). The first plurality of fins (26) are angled relative to a longitudinal axis (X) of the conduit (16) so as to form helical flowpaths (27) for fluid flowing through the first flow passage (22). A second flow passage (24) disposed outwardly of the interior surface (18) and radially outwardly of the first plurality of fins (26).

54. 发明公开

EP3335992A1 ICE PROTECTION SYSTEM 有权
公开(公告)号：EP3335992A1
公开(公告)日：2018-06-20
申请号：EP16275173.9
申请日：2016-12-16
申请人： HS Marston Aerospace Limited
发明人： PHILLIPS, Paul P.
IPC分类号： B64D15/02 , B64D37/32
CPC分类号： B64D15/02 , B64D37/32 , F28B1/06
摘要： A system for de-icing an aircraft structure or surface (11) comprises an inert gas generating system comprising a catalyst (2) for receiving fuel and oxygen and converting the fuel and oxygen to CO 2 and H 2 O in gaseous form, and a condenser (4) for condensing the H 2 O to liquid form, the condenser (4) providing heat to the aircraft structure or surface (11).

55. 发明公开

EP2474803A3 Laminated heat exchanger 有权
标题翻译：的叠层热交换器
公开(公告)号：EP2474803A3
公开(公告)日：2015-11-25
申请号：EP12150211.6
申请日：2012-01-04
申请人： HS Marston Aerospace Limited
发明人： Scott, David Russell
IPC分类号： F28D9/00 , F28F3/02
CPC分类号： F28F3/02 , F28D9/005 , F28D9/0056 , F28D9/0075 , F28F3/022
摘要： A laminated heat exchanger (2) includes at least one heat exchange layer (15;16;130;160;190;220) that includes a plurality of side members (62-66;133-135;166-169;194-197;224-228) that define a frame (60;132;164;192;222) having an interior portion (69;136;171;199;236). A plurality of heat exchange members (74;100;107;113;139;175;205;234) extend between at least two of the plurality of side members across the interior portion. The plurality of heat exchange members are linked by a ligament member (93;101;108;115) to form a heat exchange member chain (72;99;106;112;137;173;203;232).

56. 发明公开

EP2474803A2 Laminated heat exchanger 有权
标题翻译： LaminierterWärmetauscher
公开(公告)号：EP2474803A2
公开(公告)日：2012-07-11
申请号：EP12150211.6
申请日：2012-01-04
申请人： HS Marston Aerospace Limited
发明人： Scott, David Russell
IPC分类号： F28D9/00 , F28F3/02
CPC分类号： F28F3/02 , F28D9/005 , F28D9/0056 , F28D9/0075 , F28F3/022
摘要： A laminated heat exchanger (2) includes at least one heat exchange layer (15;16;130;160;190;220) that includes a plurality of side members (62-66;133-135;166-169;194-197;224-228) that define a frame (60;132;164;192;222) having an interior portion (69;136;171;199;236). A plurality of heat exchange members (74;100;107;113;139;175;205;234) extend between at least two of the plurality of side members across the interior portion. The plurality of heat exchange members are linked by a ligament member (93;101;108;115) to form a heat exchange member chain (72;99;106;112;137;173;203;232).
摘要翻译：层压热交换器（2）包括至少一个热交换层（15; 16; 130; 160; 190; 220），其包括多个侧构件（62-66; 133-135; 166-169; 194-197 ; 224-228），其限定具有内部部分（69; 136; 171; 199; 236）的框架（60; 132; 164; 192; 222）。多个热交换构件（74; 100; 107; 113; 139; 175; 205; 234）在穿过内部部分的多个侧构件的至少两个之间延伸。所述多个热交换构件通过韧带构件（93; 101; 108; 115）连接以形成热交换构件链（72; 99; 106; 112; 137; 173; 203; 232）。

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