公开(公告)号：US10472074B2

公开(公告)日：2019-11-12

申请号：US15220524

申请日：2016-07-27

Applicant: THALES

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

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

Abstract: 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：US10329024B2

公开(公告)日：2019-06-25

申请号：US15220417

申请日：2016-07-27

Applicant: THALES

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

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

Abstract: A heater of a piece of aeronautic equipment is intended to be arranged at the skin of an aircraft. The equipment includes a part intended to be arranged at the skin of the aircraft and elements for heating the part. The heating element 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 a 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 part of the equipment is made from a material with a low heat conductivity.

公开(公告)号：US10234475B2

公开(公告)日：2019-03-19

申请号：US15220488

申请日：2016-07-27

Applicant: THALES

Inventor： Claude Sarno ,  Romain Hodot ,  Marc Duval-Destin

IPC: G01P5/165 ,  B64D15/12 ,  B64D43/02 ,  F28D15/02 ,  B33Y80/00 ,  B33Y10/00 ,  B33Y50/02 ,  B22F3/105 ,  B22F5/10 ,  F28D21/00

Abstract: Manufacturing method by addition for at least one part of a piece of aeronautic equipment intended to equip an aircraft, the equipment piece including at least one part intended to be arranged at a skin of the aircraft and heating elements for that part, which include a thermodynamic loop including a closed circuit at least partially integrated, 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 being formed by a tubular channel with an empty section at least partially integral with the equipment piece, at least the part of the equipment piece arranged outside the aircraft is made by additive manufacturing and includes a base for fastening on the skin of the aircraft from which support elements for a Pitot tube extend.