Patent · US Active

Method and apparatus for providing a current return network in an aircraft structure

US9681527B2 · kind B2 · utility

4Cited by
7References
21Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 29, 2013
Grant dateJun 13, 2017
Priority date
Expiry dateFeb 1, 2035

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49117
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

According to an embodiment a current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone. According to an embodiment, an aircraft has a predetermined potential lightning strike zone. A current return network assembly is within the zone. An electrically conductive honeycomb central core is provided for conducting electrical current through the assembly and through the zone wherein the electrical current has been caused by a lightning strike on the aircraft at the zone.

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