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    • 8. 发明公开
    • INTERMEDIATE PRESSURE STORAGE SYSTEM FOR THERMAL STORAGE
    • ZWISCHENDRUCKSPEICHERSYSTEMFÜRWÄRMESPEICHER
    • EP2411672A4
    • 2017-08-09
    • EP10756978
    • 2010-03-26
    • SOLAR STORAGE COMPANY
    • MIERISCH ROBERT CHARLESBISSET STEPHEN JAMES
    • F03G6/02F01K3/00F01K13/02F01K27/00F03G6/06F22B1/00F24J2/42F28D20/00
    • F01K3/008F01K13/02F22B1/006F28D20/00Y02E10/46
    • In some implementations, there is provided an apparatus. The apparatus may include a first steam engine, an intermediate storage, and a second steam engine. The first steam engine may include a first inlet and a first exhaust, wherein the first inlet receives steam from a source of thermal energy. The intermediate storage may be coupled to the first exhaust, wherein the intermediate storage stores thermal energy provided by steam from the first exhaust. The second steam engine may include a second inlet coupled to the intermediate storage. Moreover, at least one of the first steam engine and the second steam engine may produce work. Furthermore, the first steam engine may be driven by the steam received from the source of thermal energy, and the second steam engine may be driven by steam from at least one of the intermediate storage and the first exhaust. Related apparatus and methods are also described.
    • 在一些实现中,提供了一种装置。 该装置可以包括第一蒸汽机,中间储存器和第二蒸汽机。 第一蒸汽机可以包括第一入口和第一排气口,其中第一入口接收来自热能源的蒸汽。 中间储存器可联接到第一排气,其中中间储存器储存来自第一排气的蒸汽提供的热能。 第二蒸汽机可以包括联接到中间储存器的第二入口。 此外,第一蒸汽机和第二蒸汽机中的至少一个可以产生功。 此外,第一蒸汽机可以由从热能源接收的蒸汽驱动,并且第二蒸汽机可以由来自中间存储装置和第一排气装置中的至少一个的蒸汽驱动。 还描述了相关的装置和方法。
    • 9. 发明公开
    • HEAT STORAGE MEMBER AND METHOD FOR PRODUCING SAME
    • WÄRMESPEICHERELEMENTUND HERSTELLUNGSVERFAHRENDAFÜR
    • EP2540791A4
    • 2017-08-02
    • EP11747487
    • 2011-02-25
    • MITSUBISHI HEAVY IND LTDNICHIAS CORP
    • TSUKAHARA AIICHIROABE ISAMIMIHARA TETSUYAMORIKAWA SHUWATANABE TOMOKAZU
    • C09K5/06F24V30/00
    • C09K5/063F28D20/00F28D20/023H01L23/4275H01L2924/0002H05K7/2039Y02E60/142Y02E60/145Y10T29/4935H01L2924/00
    • A light and inexpensive heat storage member applicable to spacecrafts is provided. The heat storage member includes a honeycomb structural body (3) having a plurality of cells. Each of the cells is filled with a capsule, which contains a heat storage material, and a heat conductive filler. Since the capsule containing the heat storage material and the heat conductive filler are provided in the honeycomb structural body (3), the light and inexpensive heat storage member having favorable heat conductivity even when the storage member is thick can be provided. The heat storage member is provided by bringing a starting material (2) that is a mixture of the capsule containing the heat storage material and the heat conductive filler into contact with the honeycomb structural body (3) to cover at least one surface of the opening of the cells of the honeycomb structure body (3), subjecting the same to uniaxial pressure molding under the pressure of 4 MPa or more and 10 MPa or less, and filling each cell with the starting material (2).
    • 提供适用于航天器的轻便且便宜的蓄热构件。 蓄热部件包括具有多个单元的蜂窝结构体(3)。 每个细胞填充有包含储热材料和导热填充物的胶囊。 由于在蜂窝结构体(3)中设置有包含蓄热材料和导热性填料的胶囊,所以即使在收纳部件厚的情况下,也能够提供导热性良好且廉价的蓄热部件。 通过使作为包含蓄热材料和导热填料的胶囊的混合物的起始材料(2)与蜂窝结构体(3)接触以覆盖开口的至少一个表面 在蜂窝结构体(3)的单元中,在4MPa以上,10MPa以下的压力下进行单轴加压成型,在各单元中填充原料(2)。