Patent · US Active

Forward compartment service system for a geared architecture gas turbine engine

US9410447B2 · kind B2 · utility

4Cited by
29References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 4, 2012
Grant dateAug 9, 2016
Priority date—
Expiry dateFeb 15, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF01D25/18
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine includes a jumper tube that extends through a first passage and a second passage.

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