Patent · US Active

Flame prevention device

US7918081B2 · kind B2 · utility

20Cited by
26References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 19, 2006
Grant dateApr 5, 2011
Priority date
Expiry dateFeb 2, 2030

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T442/2631
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine includes an engine casing concentrically disposed around the following: a low pressure compressor; a turbine; and a high pressure compressor having at least one bleed tube and at least one joint proximate to the engine casing; and at least one flame prevention device adapted to cover at least a portion of at least one gas turbine engine component.

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