Patent · US Active

Gas turbine engine with stacked accessory components

US9816441B2 · kind B2 · utility

3Cited by
40References
30Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 30, 2009
Grant dateNov 14, 2017
Priority date
Expiry dateAug 18, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An engine accessory system for a gas turbine engine includes a first accessory component defined along an accessory axis and a second accessory component mounted to the first accessory component along the accessory axis.

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