公开(公告)号：EP2894666B1

公开(公告)日：2018-12-26

申请号：EP15150254.9

申请日：2015-01-07

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Wicks, Curtis ,  Lovaasen, Eric ,  Anderson, Kaleb ,  Boer, Jonathan

IPC: H01L23/40 ,  H01L23/427 ,  F28D15/02 ,  H05K7/20

CPC classification number: H05K7/20418 ,  B23P15/26 ,  B23P2700/10 ,  F28D15/0275 ,  F28D2021/0028 ,  F28F2275/08 ,  F28F2275/20 ,  H01L23/4006 ,  H01L23/427 ,  H01L2924/0002 ,  Y10T29/4935 ,  H01L2924/00

Abstract: A heat exchanger system (10;20) may have a base (30), a mounting apparatus for attaching the base to a device, a gasket shelf (60) for placing a gasket, a dissipation member (70) for dissipating heat, and heat generator attachment sites for absorbing heat. A mounting apparatus may have finger-like extensions which flex and draw the base (30) into contact with an underlying electronic device from which the system conducts heat. A base (30) may also have an integrated heat pipe clamp attachment (100) forming an aperture in the base (30) into which a heat pipe may extend and may be clamped in thermal communication. The dissipation member (70) may be a series of fins and troughs and a fan (130) may direct air over the dissipation member (70) to cool the apparatus.

公开(公告)号：EP2275901A3

公开(公告)日：2015-09-16

申请号：EP10006593.7

申请日：2010-06-24

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Wicks, Curtis

IPC: G06F1/20

CPC classification number: G06F1/203 ,  B64D2045/0075 ,  G06F1/1658

Abstract: An electronic flight bag computer (EFB) includes a housing defining first and second compartments that are fluidly isolated from and in thermal communication with one another. The first compartment contains electronic components connected to a user interface on an exterior portion of the housing for providing interactive flight related computation functions to a user. The second compartment contains a forced convection cooling component in thermal communication with the electronic components. The forced convection cooling component directs a flow of cooling fluid into the second compartment to convey heat produced by the electronic components out of the housing, such that the cooling fluid in the second compartment remains fluidly isolated from the electronic components in the first compartment of the housing.

Abstract translation: 电子飞行计算机（EFB）包括限定第一和第二隔室的壳体，其与彼此流体隔离并且彼此热连通。 第一隔室包含连接到外壳的外部部分上的用户界面的电子部件，用于向用户提供与飞行有关的计算功能。 第二隔室包含与电子部件热连通的强制对流冷却部件。 强制对流冷却部件将冷却流体流引导到第二隔间以将由电子部件产生的热量传送出外壳，使得第二隔室中的冷却流体保持与第一隔室中的电子部件流体隔离 住房。

公开(公告)号：EP2894666A1

公开(公告)日：2015-07-15

申请号：EP15150254.9

申请日：2015-01-07

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Wicks, Curtis ,  Lovaasen, Eric ,  Anderson, Kaleb ,  Boer, Jonathan

IPC: H01L23/40 ,  H01L23/427

CPC classification number: H05K7/20418 ,  B23P15/26 ,  B23P2700/10 ,  F28D15/0275 ,  F28D2021/0028 ,  F28F2275/08 ,  F28F2275/20 ,  H01L23/4006 ,  H01L23/427 ,  H01L2924/0002 ,  Y10T29/4935 ,  H01L2924/00

Abstract: A heat exchanger system (10;20) may have a base (30), a mounting apparatus for attaching the base to a device, a gasket shelf (60) for placing a gasket, a dissipation member (70) for dissipating heat, and heat generator attachment sites for absorbing heat. A mounting apparatus may have finger-like extensions which flex and draw the base (30) into contact with an underlying electronic device from which the system conducts heat. A base (30) may also have an integrated heat pipe clamp attachment (100) forming an aperture in the base (30) into which a heat pipe may extend and may be clamped in thermal communication. The dissipation member (70) may be a series of fins and troughs and a fan (130) may direct air over the dissipation member (70) to cool the apparatus.

Abstract translation: 热交换器系统（10; 20）可以具有基座（30），用于将基座附接到设备的安装设备，用于放置垫圈的垫圈架（60），用于散热的散热构件（70），以及 用于吸热的发热器附件。 安装设备可以具有指状的延伸部，其弯曲并拉动基部（30）与系统传导热的下面的电子设备接触。 基座（30）还可以具有在基座（30）中形成孔的集成热管夹附件（100），热管可以延伸到该孔中并且可以热连接夹紧。 散热构件（70）可以是一系列翅片和槽，并且风扇（130）可以将空气引导到散热构件（70）上以冷却设备。

公开(公告)号：EP2275901A2

公开(公告)日：2011-01-19

申请号：EP10006593.7

申请日：2010-06-24

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： Wicks, Curtis

IPC: G06F1/20

CPC classification number: G06F1/203 ,  B64D2045/0075 ,  G06F1/1658

Abstract: An electronic flight bag computer (EFB) includes a housing defining first and second compartments that are fluidly isolated from and in thermal communication with one another. The first compartment contains electronic components connected to a user interface on an exterior portion of the housing for providing interactive flight related computation functions to a user. The second compartment contains a forced convection cooling component in thermal communication with the electronic components. The forced convection cooling component directs a flow of cooling fluid into the second compartment to convey heat produced by the electronic components out of the housing, such that the cooling fluid in the second compartment remains fluidly isolated from the electronic components in the first compartment of the housing.