Control valve for cryogenic liquid propellant
US6202671A · kind A · utility
Assignee
Inventor
Key dates
| Filing date | Jun 25, 1999 |
| Grant date | Mar 20, 2001 |
| Priority date | — |
| Expiry date | Jun 25, 2019 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T137/5762
- WIPO fieldMechanical elements
- WIPO sectorMechanical engineering
Abstract
A valve for controlling flow of cryogenic liquid propellant in a rocket engine comprises a double acting piston-cylinder unit having a first position in which the valve is closed and a second position in which the valve is open, a locking device being engageable with the double acting piston-cylinder unit to lock the unit in the closed position of the valve is closed while being free from the valve in its open position. The locking device has a control piston connected to a locking member to selectively lock and unlock the piston-cylinder unit against the force of a spring acting to lock the piston-cylinder unit, and a control chamber capable of receiving a pressure medium to move the piston and to unlock the piston-cylinder unit. A two-way control valve controls flow of the pressure to the control chamber and to valve closing and opening operation chambers of the piston-cylinder unit. The valve opening chamber receives the pressure medium from the control chamber via a passageway which is blocked by the piston until the piston-cylinder unit is unlocked.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.