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公开(公告)号：US20130259687A1
公开(公告)日：2013-10-03
申请号：US13437265
申请日：2012-04-02
CPC分类号： F01D25/12 , F01D25/02 , F01D25/14 , F02C7/04 , F02C7/047 , F02C7/055 , F02C7/14 , F02C7/18 , F02C7/185 , F05D2250/141 , F05D2250/232 , F05D2250/51 , F05D2260/213 , F05D2260/98 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine. The nose cone provides an aperture that communicates air to an interior of the nose cone.
摘要翻译： 涡轮机组件的示例尤其包括涡轮机的鼻锥体。 鼻锥提供将空气连通到鼻锥内部的孔。
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公开(公告)号：US09062566B2
公开(公告)日：2015-06-23
申请号：US13437265
申请日：2012-04-02
CPC分类号： F01D25/12 , F01D25/02 , F01D25/14 , F02C7/04 , F02C7/047 , F02C7/055 , F02C7/14 , F02C7/18 , F02C7/185 , F05D2250/141 , F05D2250/232 , F05D2250/51 , F05D2260/213 , F05D2260/98 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine. The nose cone provides an aperture that communicates air to an interior of the nose cone.
摘要翻译： 涡轮机组件的示例尤其包括涡轮机的鼻锥体。 鼻锥提供将空气连通到鼻锥内部的孔。
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公开(公告)号：US20130259639A1
公开(公告)日：2013-10-03
申请号：US13437375
申请日：2012-04-02
IPC分类号： F01D1/00
CPC分类号： F01D13/02 , F01D15/08 , F01D15/12 , F02C7/047 , F02C7/14 , F02C7/32 , F02K3/06 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump that is selectively driven by a motor or a shaft to communicate air to an interior of the nose cone. The pump shaft is driven by a dedicated geared architecture.
摘要翻译： 示例性的涡轮机组件包括涡轮机的鼻锥体和由马达或轴选择性驱动以将空气传送到鼻锥体的内部的泵。 泵轴由专用的齿轮架构驱动。
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公开(公告)号：US09115593B2
公开(公告)日：2015-08-25
申请号：US13437375
申请日：2012-04-02
CPC分类号： F01D13/02 , F01D15/08 , F01D15/12 , F02C7/047 , F02C7/14 , F02C7/32 , F02K3/06 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump that is selectively driven by a motor or a shaft to communicate air to an interior of the nose cone. The pump shaft is driven by a dedicated geared architecture.
摘要翻译： 示例性的涡轮机组件包括涡轮机的鼻锥体和由马达或轴选择性驱动以将空气传送到鼻锥体的内部的泵。 泵轴由专用的齿轮架构驱动。
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公开(公告)号：US20130259638A1
公开(公告)日：2013-10-03
申请号：US13437296
申请日：2012-04-02
IPC分类号： F01D1/00
CPC分类号： F01D9/065 , F01D1/02 , F01D5/02 , F01D9/02 , F01D25/12 , F02C7/04 , F02C7/047 , F02C7/18 , F02C7/32 , F05D2220/30 , F05D2260/20 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.
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公开(公告)号：US09127566B2
公开(公告)日：2015-09-08
申请号：US13437296
申请日：2012-04-02
CPC分类号： F01D9/065 , F01D1/02 , F01D5/02 , F01D9/02 , F01D25/12 , F02C7/04 , F02C7/047 , F02C7/18 , F02C7/32 , F05D2220/30 , F05D2260/20 , F05D2260/213 , Y02T50/675
摘要： An example turbomachine assembly includes, among other things, a nose cone of a turbomachine, and a pump at least partially within an interior of the nose cone. The pump is selectively rotated by a motor to communicate air to the interior.
摘要翻译： 示例性的涡轮机组件包括涡轮机的鼻锥，以及至少部分地在鼻锥内部的泵。 泵通过电动机选择性地旋转以将空气传送到内部。
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公开(公告)号：US20140010639A1
公开(公告)日：2014-01-09
申请号：US13541935
申请日：2012-07-05
申请人： Nathan Snape , Gabriel L. Suciu , Simon Pickford
发明人： Nathan Snape , Gabriel L. Suciu , Simon Pickford
CPC分类号： F01D25/18 , B64D29/08 , B64D33/00 , F01D25/12 , F01M5/002 , F02C7/06 , F02C7/14 , F02C7/32 , F05D2260/2214 , F16N19/00 , Y02T50/675
摘要： A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft mount flange. An oil tank is mounted to at least one of the fan case or the front and aft mount flanges. The oil tank has a cooling structure integrated into an outer surface such that the oil tank is subjected to cooling air flow from a plurality of air sources.
摘要翻译： 燃气涡轮发动机包括在核心隔室的径向外侧的风扇壳体。 压缩机部分位于发动机核心舱内，并且包括前安装法兰和后安装法兰。 油箱安装到风扇壳体或前后安装法兰中的至少一个上。 油箱具有集成到外表面中的冷却结构，使得油箱经受来自多个空气源的冷却空气流。
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公开(公告)号：US09945252B2
公开(公告)日：2018-04-17
申请号：US13541935
申请日：2012-07-05
申请人： Nathan Snape , Gabriel L. Suciu , Simon Pickford
发明人： Nathan Snape , Gabriel L. Suciu , Simon Pickford
IPC分类号： F01D25/18 , F01D25/12 , F02C7/06 , F02C7/14 , F02C7/32 , B64D33/00 , B64D29/08 , F01M5/00 , F16N19/00
CPC分类号： F01D25/18 , B64D29/08 , B64D33/00 , F01D25/12 , F01M5/002 , F02C7/06 , F02C7/14 , F02C7/32 , F05D2260/2214 , F16N19/00 , Y02T50/675
摘要： A gas turbine engine includes a fan case radially outwardly of a core compartment. A compressor section is located within an engine core compartment and includes a front mount flange and an aft mount flange. An oil tank is mounted to at least one of the fan case or the front and aft mount flanges. The oil tank has a cooling structure integrated into an outer surface such that the oil tank is subjected to cooling air flow from a plurality of air sources.
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公开(公告)号：US20140096534A1
公开(公告)日：2014-04-10
申请号：US13645067
申请日：2012-10-04
申请人： Nathan Snape , Gabriel L. Suciu , Simon Pickford , Allan R. Penda
发明人： Nathan Snape , Gabriel L. Suciu , Simon Pickford , Allan R. Penda
CPC分类号： F02C6/08 , F02C7/14 , F05D2260/213 , Y02T50/672 , Y02T50/675
摘要： An air-oil cooler (AOC) for a gas turbine engine is disclosed. The AOC may comprise an oil inlet, an oil outlet, and heat exchange elements between the oil inlet and the oil outlet. The AOC may be longitudinally positioned between a fan and a V-groove of the engine and radially spaced between a low pressure compressor and a low pressure compressor panel. A gas turbine engine comprising an AOC is disclosed. The AOC of the engine may comprise an oil inlet, an oil outlet, and heat exchange elements between the oil inlet and the oil outlet. The AOC of the engine may be longitudinally positioned between a fan and a V-groove of the engine and radially spaced between a low pressure compressor and a low pressure compressor panel. A method of operating an AOC for use on a gas turbine engine is also disclosed.
摘要翻译： 公开了一种用于燃气涡轮发动机的空气 - 油冷却器（AOC）。 AOC可以包括进油口，出油口以及进油口和出油口之间的热交换元件。 AOC可以纵向定位在发动机的风扇和V形槽之间，并且在低压压缩机和低压压缩机面板之间径向间隔开。 公开了一种包括AOC的燃气涡轮发动机。 发动机的AOC可以包括进油口，出油口和进油口和出油口之间的热交换元件。 发动机的AOC可以纵向地定位在发动机的风扇和V形槽之间，并且在低压压缩机和低压压缩机板之间径向间隔开。 还公开了一种操作用于燃气涡轮发动机的AOC的方法。
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