Patent · US Active

Rocket turbopump valves and associated systems and methods

US9217389B1 · kind B1 · utility

9Cited by
36References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 10, 2011
Grant dateDec 22, 2015
Priority date
Expiry dateAug 24, 2034

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16K3/03
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

Rocket turbopump valves and associated system and methods. A valve in accordance with at least one embodiment includes a housing having a valve aperture, and first and second valve elements positioned in the housing and movable relative to the valve aperture between a closed position and an open position. Each valve element can be pivotably connected to the housing toward a first end and supported by the other valve element toward a second end. A drive mechanism is coupled to the first and second valve elements to pivot the valve elements toward and away from their open and closed positions.

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