Patent · US Active

Fuel manifold inlet tube

US7305830B2 · kind B2 · utility

7Cited by
10References
10Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJan 31, 2007
Grant dateDec 11, 2007
Priority date
Expiry dateJan 31, 2027

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02C7/222
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

In a gas turbine engine, a fuel inlet tube comprising a body, a channel defined in the body and in fluid communication with a manifold, and a side inlet in fluid communication with the channel, the side inlet being sealingly isolated by at least two annular sealing members concentric with each other and disposed about the tube body at longitudinally spaced part points thereon.

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