Patent · US Active

Counter-rotatable fan gas turbine engine with axial flow positive displacement worm gas generator

US8708643B2 · kind B2 · utility

7Cited by
32References
60Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 14, 2007
Grant dateApr 29, 2014
Priority date
Expiry dateSep 16, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K5/00
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A counter-rotatable fan turbine engine includes a counter-rotatable fan section, a worm gas generator, and a low pressure turbine to power the counter-rotatable fan section. The low pressure turbine maybe counter-rotatable or have a single direction of rotation in which case it powers the counter-rotatable fan section through a gearbox. The gas generator has inner and outer bodies having offset inner and outer axes extending through first, second, and third sections of a core assembly. At least one of the bodies is rotatable about its axis. The inner and outer bodies have intermeshed inner and outer helical blades wound about the inner and outer axes and extending radially outwardly and inwardly respectively. The helical blades have first, second, and third twist slopes in the first, second, and third sections respectively. A combustor section extends through at least a portion of the second section.

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