Patent · US Active

Jet propulsion device and fuel supply method

US9771897B2 · kind B2 · utility

9Cited by
5References
10Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 8, 2012
Grant dateSep 26, 2017
Priority date
Expiry dateSep 21, 2034

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64G1/002
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A reaction propulsion device in which a first feed circuit for feeding a main thruster with a first propellant includes a branch connection downstream from a pump of a first turbopump, which branch connection passes through a first regenerative heat exchanger and a turbine of a first turbopump, and in which a second feed circuit for feeding the main thruster with a second propellant includes, downstream from a pump of a second turbopump, a branch-off passing through a second regenerative heat exchanger and a turbine of the second turbopump. At least one secondary thruster is connected downstream from the turbines of the first and second turbopumps.

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