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公开(公告)号：US07931740B2
公开(公告)日：2011-04-26
申请号：US12143537
申请日：2008-06-20
IPC分类号： B01D45/12
CPC分类号： B01D45/16 , B04C5/081 , B04C5/103 , B04C11/00 , F02C7/047 , F02C7/052 , F05D2250/15 , F05D2260/604 , F05D2260/607 , Y02T50/671 , Y02T50/675 , Y10S55/34
摘要： Systems and methods for separating contaminants in a contaminated airstream are described. In one embodiment, a contaminated airstream is received and a vortex is created that separates the contaminated airstream into a clean airstream used in the system and contaminants (e.g., debris and particles).
摘要翻译： 描述了污染气流中分离污染物的系统和方法。 在一个实施例中，接收受污染的气流，并且产生涡流，其将被污染的气流分离成系统中使用的干净气流和污染物（例如碎片和颗粒）。
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公开(公告)号：US20090314161A1
公开(公告)日：2009-12-24
申请号：US12143537
申请日：2008-06-20
CPC分类号： B01D45/16 , B04C5/081 , B04C5/103 , B04C11/00 , F02C7/047 , F02C7/052 , F05D2250/15 , F05D2260/604 , F05D2260/607 , Y02T50/671 , Y02T50/675 , Y10S55/34
摘要： Systems and methods for separating contaminants in a contaminated airstream are described. In one embodiment, a contaminated airstream is received and a vortex is created that separates the contaminated airstream into a clean airstream used in the system and contaminants (e.g., debris and particles).
摘要翻译： 描述了污染气流中分离污染物的系统和方法。 在一个实施例中，接收受污染的气流，并且产生涡流，其将被污染的气流分离成系统中使用的干净气流和污染物（例如碎片和颗粒）。
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公开(公告)号：US20120186673A1
公开(公告)日：2012-07-26
申请号：US13012471
申请日：2011-01-24
申请人： Steven A. Heitz
发明人： Steven A. Heitz
IPC分类号： F04B49/035
CPC分类号： F02C7/22 , F02C7/232 , F02C7/236 , F05D2260/601 , F05D2260/604 , Y10T137/86019
摘要： An aircraft fuel system is provided and includes a metering valve having inlet and outlet sides to monitor fuel flow from the inlet to the outlet side, a check valve that, when opened, allows fuel to flow toward the inlet side during start and climb conditions and, when closed, prevents such fuel flow and an ejector pump, which is operably disposed between the check valve and the metering valve, and which, with the check valve closed, pumps fuel toward the inlet side during idle conditions.
摘要翻译： 提供飞机燃料系统并且包括计量阀，该计量阀具有入口和出口侧以监测从入口到出口侧的燃料流量;止回阀，当打开时允许燃料在起动和爬升条件期间朝向入口侧流动， 当关闭时，防止这种燃料流动，并且喷射器泵可操作地设置在止回阀和计量阀之间，并且在单向阀关闭的情况下，在空转条件下将燃料泵送到入口侧。
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公开(公告)号：US20090285680A1
公开(公告)日：2009-11-19
申请号：US12121921
申请日：2008-05-16
申请人： John Raymond Hess , Kenneth Moore , Eric Roush
发明人： John Raymond Hess , Kenneth Moore , Eric Roush
IPC分类号： F01D5/08
CPC分类号： F02C7/185 , F01D5/081 , F01D5/085 , F01D5/087 , F05D2240/63 , F05D2260/604 , Y02T50/676
摘要： A system and a method to supply a coolant to a turbine bucket of a turbine. The system includes an extraction system configured to extract air from a main compressor airflow, a supply circuit, at least a part of which is disposed at an exterior of the gas turbine, coupled to the extraction system and configured to transport the extracted air, as an ingredient of the coolant, from the extraction system to a coolant insertion region, and a cooling system, disposed proximate to the coolant insertion region of the gas turbine and coupled to the supply circuit at a position on-board the gas turbine, the cooling system being configured to supply the turbine bucket with the coolant, including the extracted air.
摘要翻译： 一种向涡轮机的涡轮机桶供应冷却剂的系统和方法。 该系统包括被配置为从主压缩机气流中提取空气的提取系统，供应回路，其至少一部分设置在燃气轮机的外部，与供油系统相连，并被配置为运送抽取的空气，如 冷却剂的成分，从提取系统到冷却剂插入区域，以及冷却系统，该冷却系统设置在靠近燃气轮机的冷却剂插入区域并且在燃气轮机上的位置处连接到供应回路，冷却 系统被配置为向涡轮机桶提供包括抽取的空气的冷却剂。
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5.发明申请LUBRICATION SYSTEM AND METHOD, AND VORTEX FLOW SEPARATOR FOR USE THEREWITH 有权润滑系统和方法，以及用于其的VORTEX流量分离器公开(公告)号：US20090183950A1
公开(公告)日：2009-07-23
申请号：US12018376
申请日：2008-01-23
CPC分类号： F01D25/20 , F05D2260/601 , F05D2260/604
摘要： An aircraft engine lubrication system has a vortex separator, a first pump line having a first pump, an inlet connected to a separated lubricant area at the outlet end of the separator, and an outlet connectable to the engine. A scavenge line is provided for returning lubricant from the engine to an inlet end of the separator. A lubricant tank is connected in fluid flow communication with the separator by a connection line. A second pump line having a second pump has an inlet connected to the lubricant tank and an outlet connected to the separator for pumping lubricant from the tank to the inlet end of the separator.
摘要翻译： 飞机发动机润滑系统具有涡流分离器，具有第一泵的第一泵管线，连接到分离器出口端处的分离的润滑剂区域的入口和可连接到发动机的出口。 提供清扫线，用于将润滑剂从发动机返回到分离器的入口端。 润滑剂罐通过连接线与分离器流体连通地连接。 具有第二泵的第二泵管线具有连接到润滑剂罐的入口和连接到分离器的出口，用于将润滑剂从罐泵送到分离器的入口端。
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公开(公告)号：US09494049B2
公开(公告)日：2016-11-15
申请号：US14151794
申请日：2014-01-09
申请人： IHI Corporation
CPC分类号： F01D25/186 , F01D25/166 , F01D25/18 , F02B39/14 , F02C6/12 , F05D2220/40 , F05D2240/53 , F05D2260/604 , F05D2260/607 , F16C17/10 , F16C17/18 , F16C27/02 , F16C32/0629 , F16C33/105 , F16C2360/24
摘要： A turbocharger includes a semi-floating metal. The semi-floating metal is provided with a supply opening configured to supply oil to an inner bearing section. The turbocharger is provided with: an oil supply path which extends from inside of a bearing housing to the supply opening, and feeds the oil to be supplied to the inner bearing section; a removal section which changes a flowing direction of the oil supplied from an upstream side to separate minute foreign matter in the oil; and a conveyance path and a retaining region which collect the minute foreign matter separated by the removal section so as to prevent the minute foreign matter from mixing again with the oil flowing toward the supply opening.
摘要翻译： 涡轮增压器包括半浮动金属。 半浮动金属设置有供给开口，该供给开口构造成向内部支承部分供应油。 涡轮增压器设置有：从轴承壳体的内部延伸到供给口的供油路径，并将供给到内侧轴承部的油供给; 从上游侧供给的油的流向改变为在油中分离微小异物的去除部; 以及输送路径和保持区域，其收集由去除部分分离的微小异物，以防止微小的异物与向供给口流动的油再次混合。
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公开(公告)号：US08277170B2
公开(公告)日：2012-10-02
申请号：US12121921
申请日：2008-05-16
申请人： John Raymond Hess , Kenneth Moore , Eric Roush
发明人： John Raymond Hess , Kenneth Moore , Eric Roush
IPC分类号： F04D29/58
CPC分类号： F02C7/185 , F01D5/081 , F01D5/085 , F01D5/087 , F05D2240/63 , F05D2260/604 , Y02T50/676
摘要： A system and a method to supply a coolant to a turbine bucket of a turbine. The system includes an extraction system configured to extract air from a main compressor airflow, a supply circuit, at least a part of which is disposed at an exterior of the gas turbine, coupled to the extraction system and configured to transport the extracted air, as an ingredient of the coolant, from the extraction system to a coolant insertion region, and a cooling system, disposed proximate to the coolant insertion region of the gas turbine and coupled to the supply circuit at a position on-board the gas turbine, the cooling system being configured to supply the turbine bucket with the coolant, including the extracted air.
摘要翻译： 一种向涡轮机的涡轮机桶供应冷却剂的系统和方法。 该系统包括被配置为从主压缩机空气流中提取空气的提取系统，供应回路，其至少一部分设置在燃气涡轮机的外部，与供气系统相连，并配置成运送抽取的空气，如 冷却剂的成分，从提取系统到冷却剂插入区域，以及冷却系统，该冷却系统设置在靠近燃气轮机的冷却剂插入区域并且在燃气轮机上的位置处连接到供应回路，冷却 系统被配置为向涡轮机桶提供包括抽取的空气的冷却剂。
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8.发明授权Lubrication system and method, and vortex flow separator for use therewith 有权润滑系统和方法，以及与其一起使用的涡流分离器公开(公告)号：US08201664B2
公开(公告)日：2012-06-19
申请号：US12018376
申请日：2008-01-23
CPC分类号： F01D25/20 , F05D2260/601 , F05D2260/604
摘要： An aircraft engine lubrication system has a vortex separator, a first pump line having a first pump, an inlet connected to a separated lubricant area at the outlet end of the separator, and an outlet connectable to the engine. A scavenge line is provided for returning lubricant from the engine to an inlet end of the separator. A lubricant tank is connected in fluid flow communication with the separator by a connection line. A second pump line having a second pump has an inlet connected to the lubricant tank and an outlet connected to the separator for pumping lubricant from the tank to the inlet end of the separator.
摘要翻译： 飞机发动机润滑系统具有涡流分离器，具有第一泵的第一泵管线，连接到分离器出口端处的分离的润滑剂区域的入口和可连接到发动机的出口。 提供清扫线，用于将润滑剂从发动机返回到分离器的入口端。 润滑剂罐通过连接线与分离器流体连通地连接。 具有第二泵的第二泵管线具有连接到润滑剂罐的入口和连接到分离器的出口，用于将润滑剂从罐泵送到分离器的入口端。
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公开(公告)号：US20170030233A1
公开(公告)日：2017-02-02
申请号：US15303449
申请日：2015-04-15
CPC分类号： F01M11/03 , B01D45/04 , B01D45/08 , B01D45/14 , B01D45/16 , B64D33/02 , B64D2033/0293 , F01M2011/038 , F01M2013/0422 , F02C7/06 , F05D2260/604 , F05D2260/607 , F16N39/06 , F16N2210/02
摘要： A device for filtering a flow of gas conveying liquid or solid particles in a flow channel. According to the invention, the particles are imparted a speed that is high enough to project same by inertia into the opening of a recovery channel formed inside the flow channel, while the gas from the flow bypasses said opening due to a specific configuration of the flow conditions of a perfect fluid in the flow channel and in the collection channel.
摘要翻译： 用于过滤流动通道中的气体输送液体或固体颗粒流的装置。 根据本发明，颗粒被赋予足够高的速度以通过惯性将其突出到形成在流动通道内部的回收通道的开口中，而来自流体的气体由于流动的特定构造而绕过所述开口 在流动通道和收集通道中的完美流体的条件。
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公开(公告)号：US20150352477A1
公开(公告)日：2015-12-10
申请号：US14831271
申请日：2015-08-20
发明人： Hiroshi FUJII , Hirohito SHIMIZU , Ryo YASUDA , Yuji YAMAZAKI , Hidenori ARISAWA , Masahide KAZARI , Kazuo TANAKA
IPC分类号： B01D45/14
CPC分类号： B01D45/14 , F01D25/18 , F01M2013/0422 , F05D2260/604 , F05D2260/609 , Y02T50/671
摘要： A mist separator for separating liquid mist from a gas containing the liquid mist includes a rotor fixed to a hollow rotary shaft and includes main rotating vanes; and a stator axially juxtaposed to the rotor. The stator includes main fixed vanes located downstream of the main rotating vanes on a flow path for the gas; and a cover that covers outer peripheries of the main fixed vanes and the main rotating vanes. The main fixed vanes are formed so as to cause the gas to flow radially inward from the outer peripheries thereof while a flow rate of the gas is decreased, and the cover is provided with a cover discharge port to discharge a recovery liquid which is a collection of the liquid mist to the outside of the cover.
摘要翻译： 用于从含有液雾的气体中分离液雾的雾化分离器包括固定在中空旋转轴上并包括主旋转叶片的转子; 以及与转子轴向并置的定子。 定子包括位于主旋转叶片的下游的主固定叶片，用于气体的流路; 以及覆盖主固定叶片和主旋转叶片的外周的盖。 主固定叶片形成为使得气体从其外周径向向内流动，同时气体的流量减小，并且盖设置有盖排出口以排出作为收集物的回收液体 的液体雾到盖的外部。
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