Patent · US Active

Electrical quick lock interconnect

US7524214B2 · kind B2 · utility

4Cited by
10References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 21, 2006
Grant dateApr 28, 2009
Priority date
Expiry dateJan 14, 2027

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH01R13/62911
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

Electrical connection devices and systems for the electrical interconnection of systems and components within an aerospace vehicle, such as a production airplane, are disclosed. A typical quick lock interconnect comprises a manually installed and coupled modular electrical connector. The connector receptacles may be designed to “snap” onto a structural support, such as a stamped and formed or extruded rail, providing an inherent electrical ground path. A typical quick lock production interconnect may be fabricated from thermoplastic materials and plated with a metallic finish to provide for electrical bonding and shielding. The connector device may also include a novel slide latch coupling mechanism that provides a positive visual indication of a fully coupled connector eliminating the need for specialized tools. The structural support may be part of an aircraft fuselage section where the plurality of electrical connector shells each support the one or more electrical conductors coupled between separate fuselage sections.

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