Patent · US Active

Systems and methods for insulation of aircraft cooling systems

US10472042B2 · kind B2 · utility

1Cited by
1References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 11, 2017
Grant dateNov 12, 2019
Priority date
Expiry dateDec 7, 2037

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldThermal processes and apparatus
  • WIPO sectorMechanical engineering

Abstract

Provided are insulating apparatuses, and methods of operation, for thermal insulation and drainage of cooling system tubing. An example insulating apparatus comprises an elongated strip including a first end and a second end. A medial portion, a first edge, and a second edge, each run from the first end to the second end. The first and second edges curl around respective longitudinal axes toward the medial portion to form a first wrap portion with a first cavity defined by an interior surface of the first wrap portion, and a second wrap portion with a second cavity defined by an interior surface of the second wrap portion. A channel above the medial portion is defined by an exterior surface of each of the first and second wrap portions. The first and second cavities are interconnected with the channel through a first gap and a second gap, respectively.

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