BEVERAGE PREPARATION MATERIAL
    52.
    发明申请
    BEVERAGE PREPARATION MATERIAL 审中-公开
    饮料制备材料

    公开(公告)号:US20100196545A1

    公开(公告)日:2010-08-05

    申请号:US12526932

    申请日:2008-02-28

    IPC分类号: B65D85/804 A47J31/06

    摘要: A beverage preparation material (1) comprising a substantially insoluble and water-permeable tiller matrix (3) having a beverage ingredient (2) dispersed therein, wherein a plurality of layers, cells, or individual particles (2) of said beverage ingredient are held in a spaced-apart relationship within said material by regions of said tiller matrix (3). Also provided are beverage preparation pods and capsules (5) containing a beverage preparation material according to the invention.

    摘要翻译: 1.一种饮料制备材料(1),其包含具有分散在其中的饮料成分(2)的基本上不溶性且水分可渗透的分蘖基质(3),其中所述饮料成分的多个层,细胞或单个颗粒(2)被保持 在所述材料内以所述耕耘机矩阵(3)的区域间隔开的关系。 还提供了含有根据本发明的饮料制备材料的饮料制备容器和胶囊(5)。

    Multiple emulsions
    53.
    发明授权
    Multiple emulsions 失效
    多重乳液

    公开(公告)号:US07722891B2

    公开(公告)日:2010-05-25

    申请号:US10376811

    申请日:2003-02-28

    IPC分类号: A61K9/113 A61K8/06 A61K47/02

    摘要: Storage stable multiple emulsions of a polar phase A1, a nonpolar phase B and a polar phase A2, or of a nonpolar phase B1, a polar phase A and a nonpolar phase B2, employ particulate solids smaller than 1 μm to stabilize the resulting A1/B/A2 or B1/A/B2 multiple emulsions against coalescence, with the proviso that surface-active substances are present only up to a maximum concentration of less than 0.1 times the critical micelle concentration of the surface-active substances in phase A, A1, A2. The multiple emulsions have numerous uses including controlled release of active substances from a dispersed phase.

    摘要翻译: 极性相A1,非极性相B和极性相A2或非极性相B1,极性相A和非极性相B2的储存稳定的多重乳液使用小于1μm的颗粒固体来稳定所得的A1 / B / A2或B1 / A / B2多重乳液防止聚结,条件是表面活性物质仅存在于相A,A1中表面活性物质的临界胶束浓度的最大浓度的最低浓度的0.1倍 , A2。 多重乳液具有许多用途,包括从分散相控制活性物质的释放。

    Work extraction arrangement
    54.
    发明申请
    Work extraction arrangement 审中-公开
    工作提取安排

    公开(公告)号:US20080060340A1

    公开(公告)日:2008-03-13

    申请号:US11979586

    申请日:2007-11-06

    IPC分类号: F02C5/00 F02C1/00

    CPC分类号: F02C6/16 Y02E60/15

    摘要: A work extraction arrangement (10) comprises a cooling assembly (12) for cooling a gas to provide a working fluid capable of doing work. The arrangement (10) further includes storage means (14) for storing the working fluid and a turbine assembly (18) for extracting work from the working fluid. A fluid delivery assembly (16) is also provided to deliver the working fluid to the turbine assembly (18).

    摘要翻译: 工作提取装置(10)包括用于冷却气体以提供能够进行工作的工作流体的冷却组件(12)。 该装置(10)还包括用于存储工作流体的储存装置(14)和用于从工作流体中提取工作的涡轮机组件(18)。 还提供流体输送组件(16)以将工作流体输送到涡轮机组件(18)。

    Gas turbine engine
    56.
    发明申请
    Gas turbine engine 有权
    燃气轮机

    公开(公告)号:US20050193714A1

    公开(公告)日:2005-09-08

    申请号:US11123100

    申请日:2005-05-06

    IPC分类号: F02C3/30 F02C7/10 F02C7/143

    CPC分类号: F02C7/10 F02C3/305 F02C7/1435

    摘要: A gas turbine engine (10) comprises a second compressor (14), a first compressor (16), a heat exchanger (18), a combustor (20), a first turbine (22), a second turbine (24) and a third turbine (26) arranged in flow series. The first turbine (22) is arranged to drive the first compressor (16). The second turbine (24) is arranged to drive the second compressor (14). There are means to inject liquid into the gas turbine engine (10). The means to inject liquid is arranged to inject liquid upstream (46) of the second compressor (14), within (48) the second compressor (14), between (50) the second compressor (14) and the first compressor (16), within (52) the first compressor (16), between (54) the first compressor (16) and the heat exchanger (18) or within (56) the combustor (20) to boost the power of the gas turbine engine (10). The means to inject liquid is arranged to inject liquid between (70) the combustor (20) and the first turbine (22), within (68) the first turbine (22), between (66) the first turbine (22) and the second turbine (24), within (64) the second turbine (24), between (62) the second turbine (24) and the third turbine (26), within (60) the third turbine (26) or between (72) the third turbine (26) and the heat exchanger (18) to reduce the power of the gas turbine engine (10).

    摘要翻译: 燃气涡轮发动机(10)包括第二压缩机(14),第一压缩机(16),热交换器(18),燃烧器(20),第一涡轮机(22),第二涡轮机(24)和 第三涡轮机(26)以流动系列布置。 第一涡轮(22)布置成驱动第一压缩机(16)。 第二涡轮(24)布置成驱动第二压缩机(14)。 存在将液体注入到燃气涡轮发动机(10)中的装置。 喷射液体的装置被布置成在第二压缩机(14)内(48),第二压缩机(14)和第一压缩机(16)的(50)之间,在第二压缩机(14)的上游(46) 在第一压缩机(16)(54),第一压缩机(16)和热交换器(18)之间(56)内的燃气轮机(10)内, )。 喷射液体的装置被布置成在(68)第一涡轮(22)内(66)第一涡轮机(22)和第二涡轮机(22)之间 第二涡轮机(24)内,第二涡轮机(24)内,第二涡轮机(24)和第三涡轮机(26)之间,在第(60) 第三涡轮机(26)和热交换器(18),以降低燃气涡轮发动机(10)的功率。

    Gas turbine engine
    57.
    发明授权
    Gas turbine engine 失效
    燃气轮机

    公开(公告)号:US06865891B2

    公开(公告)日:2005-03-15

    申请号:US10431400

    申请日:2003-05-08

    摘要: A gas turbine engine (10) comprises a first compressor (16), a combustor (22) and a first turbine (24) arranged in flow series. The first turbine (24) is arranged to drive the first compressor (16). The first compressor (16) has variable inlet guide vanes (38) and the first turbine (24) has variable inlet guide vanes (42). A second compressor (48) is arranged upstream of the first compressor (16). An auxiliary intake (12) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). A valve (54) is arranged upstream of the first compressor (16) and downstream of the second compressor (48). The valve (54) is movable between a first position in which the second compressor (48) supplies air to the first compressor (16) and a second position in which the second compressor (48) does not supply fluid to the second compressor (16) and the auxiliary intake (12) supplies fluid to the first compressor (16). A drive means (60,62,64,66) is arranged to selectively drive the second compressor (48).

    摘要翻译: 燃气涡轮发动机(10)包括以流动系列布置的第一压缩机(16),燃烧器(22)和第一涡轮机(24)。 第一涡轮(24)布置成驱动第一压缩机(16)。 第一压缩机(16)具有可变的入口引导叶片(38),并且第一涡轮机(24)具有可变的入口导向叶片(42)。 第二压缩机(48)布置在第一压缩机(16)的上游。 辅助进气口(12)设置在第一压缩机(16)的上游并且在第二压缩机(48)的下游。 阀(54)布置在第一压缩机(16)的上游和第二压缩机(48)的下游。 阀(54)能够在第二压缩机(48)向第一压缩机16供应空气的第一位置和第二压缩机48不向第二压缩机16供应流体的第二位置之间移动 )和辅助进气(12)向第一压缩机(16)供应流体。 驱动装置(60,66,66,66)被布置成选择性地驱动第二压缩机(48)。

    Gas turbine engine and a method of controlling a gas turbine engine
    58.
    发明授权
    Gas turbine engine and a method of controlling a gas turbine engine 有权
    燃气涡轮发动机和控制燃气涡轮发动机的方法

    公开(公告)号:US06324828B1

    公开(公告)日:2001-12-04

    申请号:US09573562

    申请日:2000-05-19

    IPC分类号: F02C920

    CPC分类号: F02C7/08 F02C3/08 F02C9/20

    摘要: A gas turbine engine comprises a centrifugal compressor (4), an air diffuser (8), a heat exchanger (10), combustion apparatus (12), and first and second turbines (14,18). The combustion chamber assembly (22) comprises a primary, a secondary and a tertiary fuel and air mixing ducts (54,78,98). The compressor (4), diffuser (8), primary and secondary fuel and air mixing ducts (54,78) and turbines (14,18) all comprise means (6,8,16,20) for varying the mass flow area at their inlets such that in operation the amount of air mass through each component may be independently variable. Under part power conditions the mass flow is reduced and under full power conditions the mass flow is increased thereby maintaining a substantially constant gas cycle throughout the engine.

    摘要翻译: 燃气涡轮发动机包括离心式压缩机(4),空气扩散器(8),热交换器(10),燃烧装置(12)以及第一和第二涡轮机(14,18)。 燃烧室组件(22)包括初级,二级和三级燃料和空气混合管道(54,78,98)。 压缩机(4),扩散器(8),初级和次级燃料和空气混合管道(54,78)和涡轮机(14,18)都包括用于改变质量流量面积的装置(6,8,16,20) 它们的入口使得在操作中,通过每个部件的空气质量的量可以独立地变化。 在部分功率条件下,质量流量减小,并且在全功率条件下,质量流量增加,从而在整个发动机中保持基本恒定的气体循环。