公开(公告)号：US11772830B2

公开(公告)日：2023-10-03

申请号：US16824857

申请日：2020-03-20

Applicant: THALES

Inventor： Claude Sarno ,  Romain Hodot ,  Philippe Oconte

IPC: B64G1/50 ,  B64D15/02 ,  B64G1/36 ,  B64G1/58

CPC classification number: B64G1/506 ,  B64D15/02 ,  B64G1/36 ,  B64G1/58

Abstract: This aeronautical equipment for an aircraft, comprising a part configured to be positioned at the level of a skin of the aircraft and means for reheating this part comprising a closed-circuit thermodynamic loop in which a phase-change heat transfer fluid circulates, is wherein it includes means for monitoring the fluid pressure in the loop in order to detect and report a malfunction of the equipment.

公开(公告)号：US20150083674A1

公开(公告)日：2015-03-26

申请号：US14227184

申请日：2014-03-27

Applicant: THALES

Inventor： Claude Sarno ,  Philippe Oconte ,  Francois Morlet

IPC: H05K7/20 ,  H05K7/18

CPC classification number: H05K7/20136 ,  G11B33/128 ,  G11B33/142 ,  H05K7/1425 ,  H05K7/18 ,  H05K7/20581

Abstract: The invention relates to a rack intended to equip an aeronautical platform (10) comprising two parallel shelves (11, 12) positioned between a front face (13) and a rear face (14) of the platform (10), the rack (15) being intended to be inserted into the platform (10) by translation (16) from the front face (13) to the rear face (14), the rack (15) containing at least one electronic equipment item (18) extending primarily in a plane, the electronic equipment item (18) being positioned in a useful compartment (17) of the rack (15), the electronic equipment item (18) being cooled by forced convection. According to the invention, the electronic equipment item (18) is positioned in the useful compartment (15) in such a way that its main plane is parallel to the shelves (11, 12). The electronic equipment item (18) can be plugged into the rack (15) in the same direction as the direction (16) of insertion of the rack (15) into the platform (10). The rack (15) comprises means (22, 38) for guiding an air flow used for the cooling of the electronic equipment item (18), the air flow penetrating into the useful compartment (17) parallel to the plane of the electronic equipment item (18) and at right angles to the direction (16) of insertion of the rack (15) into the platform (10).

Abstract translation: 本发明涉及一种用于装备航空平台（10）的机架，该航空平台包括位于平台（10）的前表面（13）和后表面（14）之间的两个平行架（11,12），齿条（15） ）通过从前表面（13）到后表面（14）的平移（16）被插入到平台（10）中，所述齿条（15）包含至少一个电子设备项目（18），主要在 一个平面，电子设备项目（18）位于机架（15）的有用隔间（17）中，电子设备项目（18）被强制对流冷却。 根据本发明，电子设备项目（18）以其主平面平行于搁架（11,12）的方式定位在有用隔间（15）中。 电子设备项（18）可以沿与架（15）插入平台（10）的方向（16）相同的方向插入到机架（15）中。 齿条（15）包括用于引导用于电子设备物品（18）的冷却的空气流的装置（22,38），空气流平行于电子设备项目的平面穿入有用室（17） （18）并且与所述齿条（15）插入所述平台（10）中的方向（16）成直角。

公开(公告)号：US09253918B2

公开(公告)日：2016-02-02

申请号：US14227184

申请日：2014-03-27

Applicant: THALES

Inventor： Claude Sarno ,  Philippe Oconte ,  Francois Morlet

IPC: H05K5/00 ,  H05K7/00 ,  G06F1/16 ,  B64C1/00 ,  B64C30/00 ,  G08B21/00 ,  H05K7/20 ,  G11B33/12 ,  G11B33/14 ,  H05K7/14 ,  H05K7/18

CPC classification number: H05K7/20136 ,  G11B33/128 ,  G11B33/142 ,  H05K7/1425 ,  H05K7/18 ,  H05K7/20581

Abstract: A rack for an aeronautical platform comprising two parallel shelves positioned between a front face and a rear face of the platform, the rack being inserted into the platform by translation from the front face to the rear face the rack containing electronic equipment extending primarily in a plane, the electronic equipment being positioned in a useful compartment of the rack and cooled by forced convection. The electronic equipment is positioned in such a way that its main plane is parallel to the shelves. The rack comprises means for guiding an air flow used for the cooling of the electronic equipment item, the air flow penetrating into the useful compartment parallel to the plane of the electronic equipment item and at right angles to the direction of insertion of the rack into the platform.

Abstract translation: 一种用于航空平台的机架，包括位于所述平台的前表面和后表面之间的两个平行架，所述齿条通过从所述前表面到所述后表面平移而插入所述平台中，所述机架包含主要在平面中延伸的电子设备 ，电子设备被定位在机架的有用隔间中并被强制对流冷却。 电子设备的定位方式是使其主平面平行于货架。 机架包括用于引导用于电子设备项目的冷却的空气流的装置，空气流与电子设备项目的平面平行地插入有用室，并且与支架的插入方向成直角。 平台。

公开(公告)号：US20150241144A1

公开(公告)日：2015-08-27

申请号：US14625480

申请日：2015-02-18

Applicant: THALES

Inventor： Claude Sarno ,  Philippe Oconte ,  Romain Hodot

IPC: F28F9/007 ,  F28D1/02

CPC classification number: F28F9/007 ,  F28D1/02 ,  H05K7/20645 ,  H05K7/20681

Abstract: Heat regulation system (1) for at least one equipment item (2) embedded onboard an aircraft, includes a thermal regulation circuit (5) connected to the equipment item(s) (2). The thermal regulation circuit (5) includes a modular thermal regulation device (6) adapted to receive a modifiable number of thermal regulation modules (8).

Abstract translation: 用于至少一个嵌入在飞行器上的设备项目（2）的热调节系统（1）包括连接到设备项目（2）的热调节电路（5）。 热调节电路（5）包括适于接收可修改数量的热调节模块（8）的模块化热调节装置（6）。