Patent · US Active

Device for powering the pump of a rocket engine using an inertia wheel

US8632319B2 · kind B2 · utility

2Cited by
11References
19Claims
0Family size

Assignee

Inventor

Key dates

Filing dateOct 3, 2008
Grant dateJan 21, 2014
Priority date
Expiry dateOct 14, 2029

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02K9/563
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An apparatus for driving a pump for fueling a rocket engine of a space vehicle. The apparatus comprises an inertia wheel and a transmitting device to transmit a rotation of the inertia wheel to the pump. The apparatus further comprises a measuring device to measure the rotation speed of the inertia wheel a clutching device to decouple the wheel and the pump for a speed lower than a pre-determined speed lower, which is lower than the nominal rotation speed of the wheel. The invention is particularly applicable to a space vehicle comprising a rocket engine wherein the fuel supply system comprises at least one pump driven by the apparatus of the invention and a starting device to start the apparatus while the space vehicle is in flight.

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