公开(公告)号：US20160201852A1

公开(公告)日：2016-07-14

申请号：US14911015

申请日：2014-08-08

Applicant: MOSAIC TECHNOLOGY DEVELOPMENT PTY LTD

Inventor： Paul Anthony WHITEMAN ,  Derek Shane FEKETE

IPC: F17C5/06

CPC classification number: F17C7/00 ,  F17C5/007 ,  F17C5/06 ,  F17C2201/0109 ,  F17C2201/032 ,  F17C2201/054 ,  F17C2201/056 ,  F17C2203/0617 ,  F17C2203/0663 ,  F17C2205/0142 ,  F17C2205/0146 ,  F17C2221/033 ,  F17C2223/0123 ,  F17C2223/036 ,  F17C2225/0123 ,  F17C2225/036 ,  F17C2227/0192 ,  F17C2227/046 ,  F17C2265/065 ,  F17C2265/066 ,  F17C2270/0168

Abstract: A pressure vessel balanced refuelling system enables greater volumes of gas to be used as working volumes and increases gas storage efficiency. The system includes a plurality of pressure vessels, each vessel having a liquid transfer opening for the entry and exit of a liquid that is used to displace a gas inside each vessel. A liquid transfer line extends from an outside to an inside of each vessel in the plurality of pressure vessels through the liquid transfer opening, and a liquid balance line inter-connects the liquid transfer opening of each vessel with the liquid transfer opening of each other vessel. Thus a balance liquid transfer path extends from an inside to an outside of one vessel, then from the outside to the inside of each other vessel through the liquid balance line, enabling a liquid level in the one vessel to remain approximately equal to a liquid level in each other vessel.

Abstract translation: 压力容器平衡加油系统可使更大量的气体用作工作容积并提高储气效率。 该系统包括多个压力容器，每个容器具有用于液体的进入和离开的液体转移开口，其用于置换每个容器内的气体。 液体输送管线通过液体传送孔从多个压力容器中的每个容器的外部延伸到内部，并且液体平衡管线将每个容器的液体传送开口与每个容器的液体传送开口相互连接 。 因此，平衡液体输送路径从一个容器的内部延伸到外部，然后通过液体平衡管线从每个其他容器的外部延伸到内部，使得一个容器中的液位保持大致等于液面 在彼此的船只。

公开(公告)号：US20160290561A1

公开(公告)日：2016-10-06

申请号：US15036973

申请日：2014-11-18

Applicant: MOSAIC TECHNOLOGY DEVELOPMENT PTY LTD

Inventor： Paul Anthony WHITEMAN ,  Derek Shane FEKETE

IPC: F17C5/00 ,  F17C13/02 ,  F17C5/06

CPC classification number: F17C5/007 ,  F17C5/06 ,  F17C7/00 ,  F17C13/023 ,  F17C13/025 ,  F17C13/026 ,  F17C2201/0104 ,  F17C2201/0109 ,  F17C2201/032 ,  F17C2201/035 ,  F17C2201/056 ,  F17C2203/0663 ,  F17C2205/0107 ,  F17C2205/0142 ,  F17C2205/0326 ,  F17C2205/0335 ,  F17C2205/035 ,  F17C2205/0391 ,  F17C2205/0394 ,  F17C2221/033 ,  F17C2223/0123 ,  F17C2223/036 ,  F17C2225/0123 ,  F17C2225/036 ,  F17C2227/036 ,  F17C2227/0372 ,  F17C2250/032 ,  F17C2250/0421 ,  F17C2250/043 ,  F17C2250/0439 ,  F17C2250/0694 ,  F17C2250/075 ,  F17C2260/023 ,  F17C2265/065 ,  F17C2265/066 ,  F17C2270/0168 ,  F17C2270/0171 ,  F17C2270/0173 ,  F17C2270/0176

Abstract: A system and method enable intelligent refuelling of a pressurised vessel. The method includes receiving a gas at a refuelling port, wherein the refuelling port is coupled to the pressure vessel; determining a temperature 5 of the pressure vessel; determining a pressure of the pressure vessel; directing the gas through a nozzle, wherein the pressure vessel and nozzle are thermally coupled such that Joule-Thomson expansion of a gas flowing through the nozzle cools an interior cavity of the pressure vessel; and controlling a shut-off valve according to an amount of gas in the pressure 10 vessel determined according to the temperature and pressure, wherein the shut-off valve is located between the refuelling port and the pressure vessel, for controlling a flow of gas between the refuelling port and the pressure vessel.

Abstract translation: 一种加压容器的智能加油系统和方法。 该方法包括在加油口处接收气体，其中加油口联接到压力容器; 确定压力容器的温度5; 确定压力容器的压力; 将气体引导通过喷嘴，其中压力容器和喷嘴热耦合，使得流过喷嘴的气体的焦耳 - 汤姆森膨胀冷却压力容器的内腔; 以及根据根据温度和压力确定的压力10容器中的气体量控制截止阀，其中截止阀位于加油口和压力容器之间，用于控制加压口和压力容器之间的气体流动， 加油口和压力容器。