公开(公告)号：US20110180245A1

公开(公告)日：2011-07-28

申请号：US11725511

申请日：2007-03-20

Applicant: Mitsuru Obana ,  Andrew M. Rolt

Inventor： Mitsuru Obana ,  Andrew M. Rolt

IPC: F28F1/12

CPC classification number: F28D7/0058 ,  F28D7/0041 ,  F28D7/005 ,  F28D2021/0026 ,  F28F2250/04

Abstract: It is known that corrugated plate heat exchangers can have good thermal and hydraulic performance but limitations with regard to operational pressures whilst conventional tube type heat exchangers can achieve high pressure operation but can have high flow pressure losses due to the configuration of such tubes. By arranging a tube stack comprising respective tubes 2a, 3a arranged in layers typically one upon the other with cross junctions 4 between them and interstitial gaps between tubes it is possible to create swirling spinning motion in the flow possibly inside and at least outside the tubes for improved heat exchange with only limited flow restriction. The swirling flow in the heat exchanger matrix outside of the tubes passes along channels formed by the interconnecting interstitial gaps between the tubes and is guided about those tubes for heat exchange. Typically, a multitude of stack layers is combined such that association between the stack layers prevents in operation lateral and vertical movements as well as vibration of the tubes.

Abstract translation: 已知波纹板式热交换器可以具有良好的热和水力性能，但是对于操作压力的限制，而传统的管式热交换器可以实现高压操作，但是由于这种管的构造而可能具有高流量压力损失。 通过布置包括相应管2a，3a的管叠层，通常在它们之间彼此间布置有交叉连接点4和管之间的间隙之间布置成层，可以在流动中可能内部和至少在管外部产生旋转纺纱运动， 改进的热交换只有有限的流量限制。 在管外部的热交换器矩阵中的回旋流通过由管之间的互连间隙隙形成的通道，并且围绕这些管引导以进行热交换。 通常，组合多个堆叠层，使得堆叠层之间的关联在操作中防止横向和垂直运动以及管的振动。

公开(公告)号：US07716913B2

公开(公告)日：2010-05-18

申请号：US11088987

申请日：2005-03-24

Applicant: Andrew M Rolt

Inventor： Andrew M Rolt

IPC: F02K99/00

CPC classification number: F02C7/14 ,  B64D33/08 ,  F02C7/185 ,  Y02T50/675

Abstract: An engine (110, 210) for moving a conveyance (132) through a fluid includes first and second pressure creating means (13, 14) for pressurising an engine airflow, and intercooling means (116, 290, 292) for cooling the engine airflow between the first and second pressure creating means (13, 14). The intercooling means (116, 290, 292) includes a heat exchanger (116) which is arranged to be cooled by a flow of the fluid generated by the relative movement of the conveyance (132) through the fluid.

Abstract translation: 用于使运输工具（132）移动通过流体的发动机（110,210）包括用于加压发动机气流的第一和第二压力产生装置（13,14）和用于冷却发动机气流的中间冷却装置（116,290,292） 在第一和第二压力产生装置（13,14）之间。 中间冷却装置（116,290,292）包括热交换器（116），该热交换器被布置成由通过输送装置132相对运动而产生的流体流冷却。

公开(公告)号：US20090044933A1

公开(公告)日：2009-02-19

申请号：US12219373

申请日：2008-07-21

Applicant: Andrew M. Rolt ,  Anthony G. Razzell

Inventor： Andrew M. Rolt ,  Anthony G. Razzell

IPC: F28D7/00

CPC classification number: F28F3/08 ,  B21D53/02 ,  C25D1/02 ,  F28D1/0333 ,  F28F3/046 ,  Y10T29/4935 ,  Y10T29/49366

Abstract: A heat exchanger is provided in which heat exchanger shells are formed by electro forming about a mandrel. The shells are attached and joined to provide a heat exchanger module. As the shells are not press formed problems with respect to material elongation to achieve deep grooves in the shells are potentially avoided and shells can be created with more desirable thickness to achieve more efficient heat exchange. Furthermore, reduced shell thickness will also reduce weight and therefore improve the acceptability of heat exchangers in particular applications such as those associated with aerospace and automotive sports.

Abstract translation: 提供了一种热交换器，其中热交换器壳通过围绕心轴的电铸而形成。 壳体被连接并连接以提供热交换器模块。 由于壳体不是压制形成的，因此可以避免在壳体中实现深槽的材料伸长的问题，并且可以产生具有更理想厚度的壳体以实现更有效的热交换。 此外，减小的壳厚度还将减轻重量并因此提高热交换器在诸如与航空航天和汽车运动相关的特定应用中的可接受性。

公开(公告)号：US20070214766A1

公开(公告)日：2007-09-20

申请号：US11717159

申请日：2007-03-13

Applicant: Mitsuru Obana ,  Paul Fletcher ,  Christopher J. B. Barkey ,  Torbjorn O. Lindquist ,  Andrew M. Rolt

Inventor： Mitsuru Obana ,  Paul Fletcher ,  Christopher J. B. Barkey ,  Torbjorn O. Lindquist ,  Andrew M. Rolt

IPC: F02C6/00

CPC classification number: F22B1/1815 ,  F01K9/04 ,  F01K13/025 ,  F01K21/047 ,  F02C3/30 ,  F02C6/18 ,  F02C7/143 ,  F05D2260/85 ,  F05D2270/082 ,  Y02E20/14 ,  Y02P80/15

Abstract: A steam injection gas turbine engine having a once-through steam generator (OTSG). A condenser is provided downstream of the OTSG to capture water and is protected from hot flue gasses during startup by a bypass circuit. Optionally, heating the exhaust downstream of the condenser using coolant taken from an intercooler provides plume suppression.

Abstract translation: 具有直流蒸汽发生器（OTSG）的蒸气喷射燃气涡轮发动机。 在OTSG的下游提供冷凝器以捕获水，并在旁路回路启动期间保护热烟道气。 可选地，使用从中间冷却器获取的冷却剂来加热冷凝器下游的排气口提供羽流抑制。

公开(公告)号：US08387248B2

公开(公告)日：2013-03-05

申请号：US12219373

申请日：2008-07-21

Applicant: Andrew M. Rolt ,  Anthony G. Razzell

Inventor： Andrew M. Rolt ,  Anthony G. Razzell

IPC: F28F3/10

CPC classification number: F28F3/08 ,  B21D53/02 ,  C25D1/02 ,  F28D1/0333 ,  F28F3/046 ,  Y10T29/4935 ,  Y10T29/49366

Abstract: A heat exchanger is provided in which heat exchanger shells are formed by electro forming about a mandrel. The shells are attached and joined to provide a heat exchanger module. As the shells are not press formed problems with respect to material elongation to achieve deep grooves in the shells are potentially avoided and shells can be created with more desirable thickness to achieve more efficient heat exchange. Furthermore, reduced shell thickness will also reduce weight and therefore improve the acceptability of heat exchangers in particular applications such as those associated with aerospace and automotive sports.

公开(公告)号：US20110296811A1

公开(公告)日：2011-12-08

申请号：US13067484

申请日：2011-06-03

Applicant: David S. Knott ,  Alexis Lambourne ,  Andrew M. Rolt ,  Cosimo Buffone

Inventor： David S. Knott ,  Alexis Lambourne ,  Andrew M. Rolt ,  Cosimo Buffone

IPC: F02C7/047 ,  F28F13/18 ,  F01D5/08 ,  F28F7/00

CPC classification number: F01D5/18 ,  B64D15/00 ,  F01D25/02 ,  F02C7/047 ,  F05D2220/325 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676 ,  Y10T29/49353

Abstract: A heat transfer arrangement for a fluid-washed body having first and second ends and a fluid-washed surface extending there-between. The arrangement includes a heat transfer member extending from the first end at least part way along the body towards the second end. A heat source is arranged in use to heat the heat transfer member in the vicinity of the first end of the body. A plurality of thermal control layers are provided on the heat transfer member, each of the layers having a different thermal conductivity and being juxtaposed so as to create a thermal conductivity profile which varies along the length of the member. The arrangement may be used for prevention of icing of an aerofoil body such as a blade, vane or the like.

Abstract translation: 用于具有第一和第二端部的流体冲洗体和在其之间延伸的流体冲洗表面的热传递装置。 该装置包括从第一端至少部分地沿主体朝向第二端延伸的传热构件。 热源设置在使用中以加热身体第一端附近的传热构件。 多个热控制层设置在传热构件上，每个层具有不同的导热性并且并置，以便产生沿构件的长度变化的热导率分布。 该装置可以用于防止诸如叶片，叶片等的翼面体的结冰。

公开(公告)号：US20100303616A1

公开(公告)日：2010-12-02

申请号：US12704959

申请日：2010-02-12

Applicant: Adam P. Chir ,  Andrew M. Rolt

Inventor： Adam P. Chir ,  Andrew M. Rolt

IPC: F04D29/58

CPC classification number: F02C7/185 ,  F02C6/08 ,  F02K1/08 ,  F02K1/763 ,  F05D2300/50212 ,  F05D2300/505

Abstract: A cooling system is provided for an aero gas turbine engine. The system has a duct which diverts a portion of a bypass air stream of the engine. A heat exchanger located in the duct receives cooling air for cooling components of the engine. The cooling air is cooled in the heat exchanger by the diverted bypass air stream. After cooling the cooling air, the spent diverted air stream is routed to a tail cone located at the exit of the engine and ejected through a nozzle at the tail cone.

Abstract translation: 为航空燃气涡轮发动机提供冷却系统。 该系统具有将发动机的旁路气流的一部分转向的管道。 位于管道内的热交换器容纳用于冷却发动机部件的冷却空气。 冷却空气在换热器中通过转向旁路气流冷却。 在冷却冷却空气后，用过的转向空气流被引导到位于发动机出口处的尾锥并通过尾锥处的喷嘴喷射。

公开(公告)号：US09303526B2

公开(公告)日：2016-04-05

申请号：US13119291

申请日：2009-08-19

Applicant: Adam P. Chir ,  Andrew M. Rolt

Inventor： Adam P. Chir ,  Andrew M. Rolt

IPC: F02C7/18 ,  F01D5/08 ,  F01D25/08 ,  F01D25/14 ,  F02C7/141

CPC classification number: F01D25/08 ,  F01D5/081 ,  F01D25/14 ,  F02C7/141 ,  F02C7/185 ,  F05D2260/14 ,  F05D2260/211 ,  Y02T50/673 ,  Y02T50/676

Abstract: A cooling system is provided for cooling a turbine of a gas turbine engine. The system has first and second flow paths for guiding cooling air received from the compressor of the engine. The routes of both flow paths bypass the combustor of the engine. The system also has a preswirler for receiving the cooling air at the ends of the two flow paths, swirling the cooling air tangentially to the engine axis, and delivering the swirled cooling air to a rotor of the turbine. The first flow path is routed through a heat exchanger which cools the cooling air guided by the first flow path relative to the cooling air guided by the second flow path.

Abstract translation: 提供一种用于冷却燃气涡轮发动机的涡轮机的冷却系统。 该系统具有用于引导从发动机的压缩机接收的冷却空气的第一和第二流动路径。 两条流路的路线都绕过发动机的燃烧室。 该系统还具有用于接收在两个流动路径的端部处的冷却空气的预旋流器，使冷却空气与发动机轴线相切地旋转，并将旋转的冷却空气输送到涡轮机的转子。 第一流动路径通过热交换器，热交换器冷却由第一流动路径相对于由第二流动路径引导的冷却空气引导的冷却空气。

公开(公告)号：US08915058B2

公开(公告)日：2014-12-23

申请号：US13067484

申请日：2011-06-03

Applicant: David S Knott ,  Alexis Lambourne ,  Andrew M Rolt ,  Cosimo Buffone

Inventor： David S Knott ,  Alexis Lambourne ,  Andrew M Rolt ,  Cosimo Buffone

IPC: F28F13/14 ,  F02C7/047 ,  F01D5/18

CPC classification number: F01D5/18 ,  B64D15/00 ,  F01D25/02 ,  F02C7/047 ,  F05D2220/325 ,  Y02T50/67 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676 ,  Y10T29/49353

Abstract: A heat transfer arrangement for a fluid-washed body having first and second ends and a fluid-washed surface extending there-between. The arrangement includes a heat transfer member extending from the first end at least part way along the body towards the second end. A heat source is arranged in use to heat the heat transfer member in the vicinity of the first end of the body. A plurality of thermal control layers are provided on the heat transfer member, each of the layers having a different thermal conductivity and being juxtaposed so as to create a thermal conductivity profile which varies along the length of the member. The arrangement may be used for prevention of icing of an aerofoil body such as a blade, vane or the like.

Abstract translation: 用于具有第一和第二端部的流体冲洗体和在其之间延伸的流体冲洗表面的热传递装置。 该装置包括从第一端至少部分地沿主体朝向第二端延伸的传热构件。 热源设置在使用中以加热身体第一端附近的传热构件。 多个热控制层设置在传热构件上，每个层具有不同的导热性并且并置，以便产生沿构件的长度变化的热导率分布。 该装置可以用于防止诸如叶片，叶片等的翼面体的结冰。

公开(公告)号：US08833053B2

公开(公告)日：2014-09-16

申请号：US12704959

申请日：2010-02-12

Applicant: Adam P Chir ,  Andrew M Rolt

Inventor： Adam P Chir ,  Andrew M Rolt

IPC: F02C7/08 ,  F02G1/00 ,  F02G3/00

CPC classification number: F02C7/185 ,  F02C6/08 ,  F02K1/08 ,  F02K1/763 ,  F05D2300/50212 ,  F05D2300/505

Abstract: A cooling system is provided for an aero gas turbine engine. The system has a duct which diverts a portion of a bypass air stream of the engine. A heat exchanger located in the duct receives cooling air for cooling components of the engine. The cooling air is cooled in the heat exchanger by the diverted bypass air stream. After cooling the cooling air, the spent diverted air stream is routed to a tail cone located at the exit of the engine and ejected through a nozzle at the tail cone.

Abstract translation: 为航空燃气涡轮发动机提供冷却系统。 该系统具有将发动机的旁路气流的一部分转向的管道。 位于管道中的热交换器接收用于冷却发动机部件的冷却空气。 冷却空气在换热器中通过转向旁路气流冷却。 在冷却冷却空气后，用过的转向空气流被引导到位于发动机出口处的尾锥并通过尾锥处的喷嘴喷射。