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.

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.