Patent · US Active

Pressure assisted direct drive proportional hot-gas thruster

US8707675B2 · kind B2 · utility

1Cited by
14References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 20, 2011
Grant dateApr 29, 2014
Priority date
Expiry dateJan 27, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K9/30
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A hot-gas thruster is actuated using a relatively small electric motor. The hot-gas thruster includes a pressure assisted pilot shaft to keep electric power demand to only a few hundred watts peak and only tens of watts on average, while exhibiting relatively fast response times.

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