Patent · US Active

Avionic equipment heating

US10183753B2 · kind B2 · utility

1Cited by
8References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 27, 2016
Grant dateJan 22, 2019
Priority date
Expiry dateFeb 17, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02P10/25
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.