公开(公告)号：US20190276307A1

公开(公告)日：2019-09-12

申请号：US16293330

申请日：2019-03-05

申请人： Thales

发明人： Bertrand LEVERRIER ,  Claude Sarno ,  Claude Rougeot ,  Romain Hodot

IPC分类号： B81B7/00 ,  B81B7/02

摘要： The present invention relates to an electronic system comprising an electronic system comprising an electromechanical microsystem and a hermetic box encapsulating said microsystem. The box includes a fastening plane. The electromechanical microsystem includes a sensitive part and at least two beams connecting the sensitive part to the fastening plane.The beams are thermally coupled to the sensitive part and are electrically coupled to one another. The system further includes a thermal regulator of the electromechanical microsystem including an electrical circuit including at least two ends connected to the beams, and a circuit controller able to generate an electrical current in the electrical circuit to modify the temperature of the sensitive part.

公开(公告)号：US09975639B2

公开(公告)日：2018-05-22

申请号：US15220644

申请日：2016-07-27

申请人： THALES

发明人： Romain Hodot ,  Claude Sarno ,  Frederic Martin ,  Adrien Desjardins ,  Jean-Philippe Pineau

IPC分类号： G01F1/46 ,  B64D15/06 ,  B64D15/12 ,  B64D43/02 ,  G01P5/165 ,  B33Y80/00 ,  F28D15/04 ,  B33Y50/02 ,  B22F3/105 ,  B22F5/10 ,  F28D21/00

CPC分类号： B64D15/06 ,  B22F3/1055 ,  B22F5/10 ,  B22F2202/13 ,  B22F2203/00 ,  B33Y50/02 ,  B33Y80/00 ,  B64D15/12 ,  B64D43/02 ,  F28D15/043 ,  F28D2021/0021 ,  G01F1/46 ,  G01P5/165 ,  Y02P10/295

摘要： A piece of aeronautic equipment intended to equip an aircraft, the equipment piece (25) including at least one part intended to be arranged at a skin (27) outside of the aircraft and heating elements for that part, which include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator and a zone in which condensation of the heat transfer fluid can occur in the appendage to heat it, outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section, at least the part of the piece of equipment arranged outside the aircraft is made by additive manufacturing and includes a fastening base (120) for fastening on the skin of the aircraft from which support elements (130) for a Pitot tube (140) provided with lateral static pressure taps (150) extend.

公开(公告)号：US11300332B2

公开(公告)日：2022-04-12

申请号：US16232779

申请日：2018-12-26

申请人： THALES

发明人： Romain Hodot ,  Claude Sarno

IPC分类号： F25B21/02 ,  G01P1/02 ,  H01L35/32 ,  G05D23/19 ,  G05D23/24

摘要： The present invention relates to a thermal control device of a component, the control device including: a power source, a converter able to convert a temperature variation into a resistance variation, and a cooling module including two faces, a first face at a first temperature and a second face at a second temperature, the difference between the first temperature and the second temperature depending on the current supplying the cooling module, the first face being in, contact with the component, the cooling module, the converter and the power source being arranged electrically so that the current supplying the converter decreases with a temperature increase and the current supplying the cooling module remains constant.

公开(公告)号：US10183753B2

公开(公告)日：2019-01-22

申请号：US15220481

申请日：2016-07-27

申请人： THALES

发明人： Jean-Philippe Pineau ,  Claude Sarno ,  Romain Hodot ,  Frederic Martin

IPC分类号： B64D15/02 ,  B64D15/06 ,  B64D15/12 ,  B64D43/02 ,  G01P5/165 ,  F28D15/02 ,  G01P13/02 ,  B33Y10/00 ,  B64F5/00 ,  F28D15/04 ,  B64D33/08 ,  F28D21/00 ,  B33Y50/02 ,  B33Y80/00

摘要： A piece of aeronautic equipment intended to equip an aircraft, the equipment (25) including a part intended to be arranged at a skin (27) of the aircraft and elements for heating the part, characterized in that the heating elements include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator (14) associated with functional elements (25a) of the aircraft forming a heat source giving off heat during their operation and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator (14), the circuit in which the fluid circulates is formed by a tubular channel with an empty section.

公开(公告)号：US10035603B2

公开(公告)日：2018-07-31

申请号：US15221170

申请日：2016-07-27

申请人： THALES

发明人： Claude Sarno ,  Romain Hodot

IPC分类号： B33Y50/02 ,  B33Y80/00 ,  B64D33/08 ,  F28D21/00 ,  B64D15/06 ,  B64D15/12 ,  B64D43/02 ,  G01P5/165 ,  F28D15/02 ,  B33Y10/00 ,  G01F1/46

CPC分类号： B64D15/06 ,  B33Y10/00 ,  B33Y50/02 ,  B33Y80/00 ,  B64D15/12 ,  B64D33/08 ,  B64D43/02 ,  F28D15/0266 ,  F28D2021/0021 ,  G01F1/46 ,  G01P5/165

摘要： An aircraft provided with at least one piece of aeronautic equipment, the equipment (25) including a part intended to be arranged at a skin (27) of the aircraft and elements for heating the part, characterized in that the heating elements include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator (14) associated with functional elements (70) of the aircraft forming a heat source giving off heat during their operation and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator, the circuit in which the fluid circulates is formed by a tubular channel with an empty section.

公开(公告)号：US09849993B2

公开(公告)日：2017-12-26

申请号：US15220428

申请日：2016-07-27

申请人： THALES

发明人： Claude Sarno ,  Romain Hodot

IPC分类号： G01F1/68 ,  B64D15/06 ,  B64D15/12 ,  B64D43/02 ,  F28D15/02 ,  G01P5/165 ,  B33Y10/00 ,  B64F5/10 ,  B33Y80/00 ,  B33Y50/02 ,  B64D33/08 ,  F28D21/00

CPC分类号： B64D15/06 ,  B33Y10/00 ,  B33Y50/02 ,  B33Y80/00 ,  B64D15/12 ,  B64D33/08 ,  B64D43/02 ,  B64F5/10 ,  F28D15/02 ,  F28D15/0266 ,  F28D2021/0021 ,  G01P5/165

摘要： An aircraft provided with at least two pieces of aeronautic equipment, a first piece of equipment (25) including a part intended to be arranged at a skin (27) of the aircraft and elements for heating the part, characterized in that the heating elements include a thermodynamic loop including a closed circuit in which a heat transfer fluid circulates, the closed circuit including an evaporator (14) associated with functional elements (80) of the second piece of equipment (81) of the aircraft forming a heat source giving off heat during their operation and a zone in which a condensation of the heat transfer fluid can occur in the appendage to heat it, and in that outside the evaporator (14), the circuit in which the fluid circulates is formed by a tubular channel with an empty section.

公开(公告)号：US20150241144A1

公开(公告)日：2015-08-27

申请号：US14625480

申请日：2015-02-18

申请人： THALES

发明人： Claude Sarno ,  Philippe Oconte ,  Romain Hodot

IPC分类号： F28F9/007 ,  F28D1/02

CPC分类号： F28F9/007 ,  F28D1/02 ,  H05K7/20645 ,  H05K7/20681

摘要： 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).

摘要翻译： 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）。

公开(公告)号：US10994988B2

公开(公告)日：2021-05-04

申请号：US16293330

申请日：2019-03-05

申请人： THALES

发明人： Bertrand Leverrier ,  Claude Sarno ,  Claude Rougeot ,  Romain Hodot

IPC分类号： B81B7/02 ,  B81B7/00

摘要： The present invention relates to an electronic system comprising an electronic system comprising an electromechanical microsystem and a hermetic box encapsulating said microsystem. The box includes a fastening plane. The electromechanical microsystem includes a sensitive part and at least two beams connecting the sensitive part to the fastening plane. The beams are thermally coupled to the sensitive part and are electrically coupled to one another. The system further includes a thermal regulator of the electromechanical microsystem including an electrical circuit including at least two ends connected to the beams, and a circuit controller able to generate an electrical current in the electrical circuit to modify the temperature of the sensitive part.

公开(公告)号：US10667330B2

公开(公告)日：2020-05-26

申请号：US15094882

申请日：2016-04-08

申请人： THALES

发明人： Claude Sarno ,  Romain Hodot

IPC分类号： H05B3/00 ,  B64D43/02 ,  G01P5/165 ,  B33Y80/00 ,  B64D15/00

摘要： An aerodynamic measurement probe comprises a part to be sited in the region of the skin of an aircraft and means for heating the part. The heating means comprise a thermodynamic loop comprising a closed circuit in which a heat-transfer fluid circulates, the closed circuit comprising an evaporator and a zone in which the heat-transfer fluid can be condensed in the appendage in order to heat it. Outside the evaporator, the circuit in which the fluid circulates is formed by a tubular duct of open cross section.

公开(公告)号：US10472074B2

公开(公告)日：2019-11-12

申请号：US15220524

申请日：2016-07-27

申请人： THALES

发明人： Adrien Desjardins ,  Frederic Martin ,  Claude Sarno ,  Romain Hodot ,  Jean-Philippe Pineau

IPC分类号： B64D15/06 ,  B64D43/02 ,  G01P5/165 ,  F28D15/02 ,  B33Y10/00 ,  B33Y50/02 ,  B33Y80/00 ,  B64F5/00 ,  F25B39/00 ,  B64D15/12 ,  F28D21/00 ,  F25B39/02

摘要： The invention relates to an aircraft provided with at least one piece of aeronautic equipment fastened to the outside skin of the aircraft and a heater for heating the piece of aeronautic equipment. The heater is in the form of a thermodynamic closed circuit loop circulating heat-transfer fluid and including an evaporator and a heat source located inside the aircraft and a condenser located in the piece of aeronautic equipment or an appendage thereto. Fasteners in the form of tubular tabs include tubular channels for circulating the heat-transfer fluid.