发明名称 |
Feed system and a method of suppressing the POGO effect |
摘要 |
A rocket engine feed system, includes a feed circuit including a device for varying a gas volume in the feed circuit to suppress the POGO effect. A method of suppressing the POGO effect varies at least one hydraulic resonant frequency by varying a rate at which gas is injected into the feed circuit. |
申请公布号 |
US9528470(B2) |
申请公布日期 |
2016.12.27 |
申请号 |
US201214118369 |
申请日期 |
2012.05.07 |
申请人 |
SNECMA;CENTRE NATIONAL D'ETUDES SPATIALES CNES |
发明人 |
Kernilis Alain;Lemoine Nicolas;Boulet Ludivine;Le Gonidec Serge |
分类号 |
F02K9/50;F02K9/60;F02K9/56 |
主分类号 |
F02K9/50 |
代理机构 |
Oblon, McClelland, Maier & Neustadt, L.L.P. |
代理人 |
Oblon, McClelland, Maier & Neustadt, L.L.P. |
主权项 |
1. A feed system for feeding a rocket engine with a liquid propellant, the system comprising:
a feed circuit; and a device to vary a volume of gas in the feed circuit, which device is configured to cause a volume of gas in the feed circuit to vary while the rocket engine is in operation, wherein the device to vary the volume of gas comprises a hydraulic accumulator with a variable liquid level, the hydraulic accumulator including a plurality of dip tubes, each including a respective valve and connecting a duct of the feed circuit to a respective distinct liquid level, wherein each dip tube extends to a surface of the liquid at their respective distinct liquid level. |
地址 |
Paris FR |