Patent · US Active

Power take-off system and gas turbine engine assembly including same

US8015828B2 · kind B2 · utility

90Cited by
18References
25Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 3, 2007
Grant dateSep 13, 2011
Priority date
Expiry dateMay 24, 2030

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49245
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A power take-off system for a gas turbine engine includes a starter coupled to a second spool, and a clutch assembly coupled between the starter and a first spool, the clutch assembly configured to couple the first spool to the starter when starting the gas turbine engine assembly. A method of assembling a gas turbine engine assembly that includes the power take-off system, and a gas turbine engine assembly including the power take-off system are also described.

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