Methods and apparatus for operating a refrigeration system characterized
by controlling engine coolant
    2.
    发明授权
    Methods and apparatus for operating a refrigeration system characterized by controlling engine coolant 失效
    用于操作制冷系统的方法和装置,其特征在于控制发动机冷却剂

    公开(公告)号:US5465586A

    公开(公告)日:1995-11-14

    申请号:US369432

    申请日:1995-01-06

    摘要: A refrigeration system of the type having an economizer cycle is provided with a null cycle, in addition to heating and cooling cycles, without shutting a compressor prime mover down, to preserve air flow in a conditioned space. First, second and third controllable valves respectively: (1) select main and auxiliary condensers, (2) open and close a liquid line, and (3) open and close a line which provides a warm liquid to an economizer heat exchanger. The valves are controlled in at least one predetermined open/close pattern during a null cycle, and preferably in a plurality of selectable predetermined open/close patterns, to provide a null cycle at any instant which substantially matches the net heat gain or loss taking place in the conditioned space. Thus, the temperature of the served space will be more apt to remain in a null temperature range close to set point, providing smoother and more accurate control over the temperature of the conditioned space for longer shelf life of perishables stored therein. The system achieves the latter by controlling cooling circulation in the compressor oil cooler.

    摘要翻译: 具有省煤器循环的类型的制冷系统除了加热和冷却循环之外还提供零循环,而不关闭压缩机原动机,以保持调节空间中的气流。 第一,第二和第三个可控阀门:(1)选择主冷凝器和辅助冷凝器,(2)打开和关闭液体管线,(3)打开和关闭向节能换热器提供暖液体的管线。 在空循环期间,并且优选以多个可选择的预定打开/关闭模式,阀被控制在至少一个预定的打开/关闭模式,以在与实际匹配的净热增益或损失发生的任何瞬间提供零循环 在空调空间。 因此,被处理空间的温度将更加容易地保持在接近设定点的零点温度范围内,从而为存储在其中的易腐品的更长的保存期限提供了对调节空间的温度的更平滑和更精确的控制。 该系统通过控制压缩机油冷却器中的冷却循环来实现后者。

    Methods and apparatus for operating a refrigeration system
    4.
    发明授权
    Methods and apparatus for operating a refrigeration system 失效
    用于操作制冷系统的方法和装置

    公开(公告)号:US5228301A

    公开(公告)日:1993-07-20

    申请号:US919799

    申请日:1992-07-27

    摘要: A refrigeration system of the type having an economizer cycle is provided with a null cycle, in addition to heating and cooling cycles, without shutting a compressor prime mover down, to preserve air flow in a conditioned space. First, second and third controllable valves respectively: (1) select main and auxiliary condensers, (2) open and close a liquid line, and (3) open and close a line which provides a warm liquid to an economizer heat exchanger. The valves are controlled in at least one predetermined open/close pattern during a null cycle, and preferably in a plurality of selectable predetermined open/close patterns, to provide a null cycle at any instant which substantially matches the net heat gain or loss taking place in the conditioned space. Thus, the temperature of the served space will be more apt to remain in a null temperature range close to set point, providing smoother and more accurate control over the temperature of the conditioned space for longer shelf life of perishables stored therein.

    摘要翻译: 具有省煤器循环的类型的制冷系统除了加热和冷却循环之外还提供零循环,而不关闭压缩机原动机,以保持调节空间中的气流。 第一,第二和第三个可控阀门:(1)选择主冷凝器和辅助冷凝器,(2)打开和关闭液体管线,(3)打开和关闭向节能换热器提供暖液体的管线。 在空循环期间,并且优选以多个可选择的预定打开/关闭模式,阀被控制在至少一个预定的打开/关闭模式,以在与实际匹配的净热增益或损失发生的任何瞬间提供零循环 在空调空间。 因此,被处理空间的温度将更加容易地保持在接近设定点的零点温度范围内,从而为存储在其中的易腐品的更长的保存期限提供了对调节空间的温度的更平滑和更精确的控制。

    Method of operating a transport refrigeration system having a six
cylinder compressor
    7.
    发明授权
    Method of operating a transport refrigeration system having a six cylinder compressor 失效
    操作具有六缸压缩机的运输制冷系统的方法

    公开(公告)号:US4735055A

    公开(公告)日:1988-04-05

    申请号:US61765

    申请日:1987-06-15

    IPC分类号: F25B49/02 F25D29/00 F25B49/00

    摘要: A method of operating a transport refrigeration system having a six cylinder compressor and a prime mover operable at a selected one of low and high speeds, to control the temperature of a served space by cooling and hot gas heating modes. Below a set point temperature 100, system heating capacity is controlled at the low compressor speed by the step 127 of unloading compressor cylinders and the step 129 of reloading compressor cylinders. A temperature rise of the served space above a set point temperature 106 controls cooling capacity by a combination of alternative steps 135, 137, 139, 141, and 143 which may or may not change the number of loaded compressor cylinders, and may or may not change compressor speed, based upon two predetermined trigger events which relate to what the temperature of the served space does relative to time 136 and 142, a set point temperature 106, and a temperature 108 above set point which is normally associated with a change in compressor speed.

    摘要翻译: 一种操作具有六缸压缩机和原动机的运输制冷系统的方法,所述原动机可以以低速和高速选定的一个运行,以通过冷却和热气体加热模式来控制所服务空间的温度。 在设定点温度100以下,通过卸载压缩机气缸的步骤127和重新装载压缩机气缸的步骤129,将系统加热能力控制在低压缩机速度。 受控空间在设定点温度106以上的温度上升通过替代步骤135,137,139,141和143的组合控制冷却能力,可替代步骤135,137,139,141和143可以改变或不改变加载的压缩机气缸的数量,并且可以或不可以 基于两个预定的触发事件来改变压缩机速度,这两个预定触发事件涉及所服务空间的温度相对于时间136和142,设定点温度106以及通常与压缩机变化相关联的设定点上方的温度108 速度。

    Sealing structures for gas turbine engines
    8.
    发明授权
    Sealing structures for gas turbine engines 失效
    燃气轮机发动机密封结构

    公开(公告)号:US5470198A

    公开(公告)日:1995-11-28

    申请号:US299061

    申请日:1994-08-31

    摘要: A cooling and sealing arrangement in a gas turbine engine comprises a seal assembly extending between nozzle guide vanes and combustion chamber discharge nozzles. The nozzle guide vanes have platforms having extensions which in one embodiment overlap the downstream ends of the discharge nozzles. Cooling air is supplied to the upstream edge portions of the platforms through holes in flanges on the discharge nozzles. The seal assembly defines a chamber adjacent the platform extensions which is supplied with cooling air through metering holes in the seal assembly which provides part of a boundary for a cooling air chamber, the boundary of the chamber having cooling air holes for metering cooling air into the chamber to cool the upstream portion of the nozzle guide vane outer platforms. Cooling air exits the chamber through holes in the platform extensions to film cool them.

    摘要翻译: 燃气涡轮发动机中的冷却和密封装置包括在喷嘴导向叶片和燃烧室排出喷嘴之间延伸的密封组件。 喷嘴导叶具有具有延伸部的平台,在一个实施例中,该延伸部与排放喷嘴的下游端重叠。 冷却空气通过排放喷嘴上的凸缘中的孔被供应到平台的上游边缘部分。 密封组件限定了邻近平台延伸部分的室,该冷却空气通过密封组件中的计量孔供应冷却空气,该冷却空气为冷却空气室提供了一部分边界,该室的边界具有冷却空气孔,用于将冷却空气计入 以冷却喷嘴导向叶片外平台的上游部分。 冷却空气通过平台延伸部分中的孔离开室以使其冷却。

    Sealing structures for gas turbine engines
    9.
    发明授权
    Sealing structures for gas turbine engines 失效
    燃气轮机发动机密封结构

    公开(公告)号:US5407319A

    公开(公告)日:1995-04-18

    申请号:US207626

    申请日:1994-03-09

    摘要: A cooling and sealing arrangement in a gas turbine engine comprises a seal assembly (42,30) extending between nozzle guide vanes (20) and combustion chamber discharge nozzles (22). The nozzle guide vanes (20) have platforms (34,36) having extensions (34A,36A) which in one embodiment overlap the downstream ends of the discharge nozzles (22). Cooling air is supplied to the upstream edge portions of the platforms through holes (26,28C) in flanges (24,28) on the discharge nozzles (22). The seal assembly (42,30) defines a chamber (58,70) adjacent the platform extensions which is supplied with cooling air through metering holes (56,68) in the seal assembly. Cooling air exits the chamber (58,70) through holes (34B,36B) in the platform extensions to film cool them.

    摘要翻译: 燃气涡轮发动机中的冷却和密封装置包括在喷嘴导向叶片(20)和燃烧室排出喷嘴(22)之间延伸的密封组件(42,30)。 喷嘴导向叶片(20)具有在一个实施例中与排放喷嘴(22)的下游端重叠的延伸部(34A,36A)的平台(34,36)。 冷却空气通过排放喷嘴(22)上的凸缘(24,28)中的孔(26,28C)供应到平台的上游边缘部分。 密封组件(42,30)限定了邻近平台延伸部的腔室(58,70),其通过密封组件中的计量孔(56,68)供应冷却空气。 冷却空气通过平台延伸部中的孔(34B,36B)离开室(58,70),以使其冷却。

    Means for trapping oil lost during startup of refrigerant compressors
    10.
    发明授权
    Means for trapping oil lost during startup of refrigerant compressors 失效
    用于捕获制冷剂压缩机启动过程中油损失的方法

    公开(公告)号:US3978685A

    公开(公告)日:1976-09-07

    申请号:US595983

    申请日:1975-07-14

    申请人: David H. Taylor

    发明人: David H. Taylor

    摘要: This invention relates to a compression refrigeration system having means for removing some of the oil refrigerant foam which is formed in a crankcase at startup. The removal of foam with entrained oil from the crankcase is to reduce the amount of oil pumped with the refrigerant through condenser and evaporator and at the same time rapidly return oil to the crankcase during startup. In one embodiment of the invention, oil refrigerant foam goes from the crankcase to a foam trap where the foam collapses, the oil drains back to the crankcase, and the refrigerant vapor is drawn to an intake of the compressor. In another embodiment, oil refrigerant foam passes to a suction accumulator where the foam collapses, refrigerant vapor is drawn to an intake of the compressor and the vapor carries droplets of separated oil to a point where they drain back to the crankcase.

    摘要翻译: 本发明涉及一种压缩式制冷系统,其具有用于去除启动时在曲轴箱中形成的一些油制冷剂泡沫的装置。 从曲轴箱中去除具有夹带油的泡沫是通过冷凝器和蒸发器减少用制冷剂泵送的油量,同时在启动期间迅速将油返回到曲轴箱。 在本发明的一个实施例中,油致冷剂泡沫从曲轴箱流到泡沫陷阱,泡沫破裂,油排出回到曲轴箱,并且制冷剂蒸气被抽吸到压缩机的入口。 在另一个实施方案中,油制冷剂泡沫通过吸收储存器,其中泡沫破裂,制冷剂蒸汽被抽吸到压缩机的入口,并且蒸汽携带分离的油的液滴到它们排回到曲轴箱的点。