Patent · US Active

Ice protection system for a multi-segment aircraft component

US7837150B2 · kind B2 · utility

17Cited by
60References
21Claims
0Family size

Assignees

Inventors

Key dates

Filing dateDec 21, 2007
Grant dateNov 23, 2010
Priority date
Expiry dateMay 8, 2029

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49826
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft component includes a first segment having a first leading edge surface that extends to a first end of the first segment. The aircraft component also includes a second segment having a second leading edge surface that extends to a second end of the second segment. The second end is substantially adjacent to the first end of the first segment, and is connected to the first end. The first leading edge surface includes electrical resistance heating that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating that extends to the second end of the second segment. The electrical resistance heating is capable of providing ice protection heating immediately on either side of a juncture between the connected first and second ends.

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