Patent · US Active

Gas turbine engine with attached nosecone

US9540939B2 · kind B2 · utility

8Cited by
15References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 26, 2013
Grant dateJan 10, 2017
Priority date
Expiry dateJun 4, 2035

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49321
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine includes a compressor section and a nosecone assembly. The compressor section includes an inlet guide vane assembly including an inner shroud, an outer shroud, and an inlet guide vane extending from the inner shroud to the outer shroud. The nosecone assembly is attached to the inner shroud.

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