Patent · US Active

Surface deicing device configured not to generate electromagnetic interference

US11358726B2 · kind B2 · utility

0Cited by
4References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 22, 2019
Grant dateJun 14, 2022
Priority date
Expiry dateSep 14, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D15/04
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A device for deicing a wall of an aircraft, comprising a closed circuit. The closed circuit comprises at least one condenser, positioned in the environment of the wall that is to be deiced, and in which a heat-transfer fluid condenses, generating energy in the form of latent heat which is transmitted to the wall that is to be deiced, at least one evaporator positioned in the environment of a heat source sited remotely with respect to the wall, and in which the heat-transfer fluid evaporates, absorbing energy in the form of latent heat coming from the heat source. At least part of the closed circuit is facing, in contact with, or positioned in, the wall that is to be deiced, being made of a material transparent to electromagnetic fields.

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