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公开(公告)号:US3701262A
公开(公告)日:1972-10-31
申请号:US3701262D
申请日:1970-10-12
Applicant: SYSTEMS CAPITAL CORP
Inventor: CONNELL JOSEPH A , BARANYI ANTHONY J
CPC classification number: F17C3/005 , F17C2201/0104 , F17C2201/0119 , F17C2201/032 , F17C2201/052 , F17C2203/016 , F17C2203/0341 , F17C2203/0391 , F17C2203/0604 , F17C2203/0629 , F17C2203/0643 , F17C2203/0646 , F17C2203/0663 , F17C2203/0673 , F17C2203/0678 , F17C2205/0367 , F17C2209/228 , F17C2221/033 , F17C2223/0161 , F17C2223/033 , F17C2223/047 , F17C2227/0135 , F17C2227/0178 , F17C2227/0353 , F17C2227/0388 , F17C2250/0439 , F17C2250/0631 , F17C2270/0147
Abstract: Liquified gas is stored underground in a large double walled container seated in an opening in the earth''s surface. Between the walls of the liner, thermal insulation is distributed in a continuous layer along the floor and wall of the opening. A diaphragm is supported across the top of the opening with a seal being provided between the diaphragm and the double walled liner to form a container for the liquified gas. Surrounding the lip of the opening is a concrete ring across which a net of cables is stretched to support a thermally insulating ceiling. A cooling system is provided for freezing the earth to aid in the excavation of the opening and this system is subsequently used to maintain the wall and floor of the opening frozen to a controlled thickness by cooling them in response to a rise in the temperature of the surrounding earth above a predetermined temperature level. Also disclosed are various techniques for constructing a storage tank of the type described.
Abstract translation: 液化天然气储存在位于地球表面开口的大型双壁容器中。 在衬套的墙壁之间,隔热层沿着开口的地板和墙壁分布在连续的层中。 隔膜支撑在开口的顶部,隔膜和双壁衬套之间设有密封件,以形成用于液化气体的容器。 围绕开口的唇缘是一个混凝土环,电缆网被拉伸以支撑绝热天花板。 提供冷却系统用于冷冻地面以帮助开口的开挖,并且该系统随后被用于通过冷却它们来将开口的壁和地板冷却到受控的厚度,以响应于 周围地球超过预定温度水平。
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公开(公告)号:US3591962A
公开(公告)日:1971-07-13
申请号:US3591962D
申请日:1969-05-26
Applicant: SYSTEMS CAPITAL CORP
Inventor: CONNELL JOSEPH A
CPC classification number: F02C7/272 , F02C7/277 , Y02T50/671
Abstract: A method and apparatus for starting a gas turbine engine by vaporizing a cryogenic liquid such as liquid nitrogen, raising the resulting gas to a high temperature and pressure and applying the hot pressurized gas to the air-driven turbine starter of the gas turbine engine.
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