专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08257024B1 Geared turbomachine fluid delivery system 有权
标题翻译：齿轮涡轮机输液系统
公开(公告)号：US08257024B1
公开(公告)日：2012-09-04
申请号：US13359897
申请日：2012-01-27
申请人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
IPC分类号： F01D25/18
CPC分类号： F01D25/18 , F01M5/005 , F02C7/14 , Y02T50/675
摘要： An exemplary geared turbomachine fluid delivery system includes a first fluid path configured to communicate fluid from a supply to a gear system of a geared turbomachine, and a second fluid path configured to communicate fluid from the supply to the gear system. The fluid introduced to the gear system by the first fluid path is cooler than that the fluid introduced to the gear system by the second fluid path.
摘要翻译：示例性的齿轮涡轮机输送系统包括被配置为将流体从供应件传递到齿轮传动涡轮机的齿轮系统的第一流体路径和被配置为将流体从供应件传递到齿轮系统的第二流体路径。通过第一流体路径引入齿轮系统的流体比通过第二流体路径引入齿轮系统的流体更冷。

2. 发明授权

US08443582B1 Gas turbine engine with geared turbofan and oil thermal management system 有权
标题翻译：燃气涡轮发动机带有齿轮涡轮风扇和油热管理系统
公开(公告)号：US08443582B1
公开(公告)日：2013-05-21
申请号：US13361997
申请日：2012-01-31
申请人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
发明人： Kathleen R. Phillips , Thomas G. Phillips , Ethan K. Stearns , Federico Papa
IPC分类号： F02C7/06 , F02C1/00 , F02K99/00 , F01D25/18 , F02K9/64
CPC分类号： F01D25/20 , F01D25/18 , F01M5/002 , F02C7/06 , F02C7/14 , F02K9/64 , F05D2260/213 , F05D2260/40311 , Y02T50/676
摘要： A lubricant supply system for a gas turbine engine has a lubricant lube pump delivering lubricant to an outlet line. The outlet line is split into at least a hot line and into a cool line, with the hot line directed primarily to locations associated with an engine that are not intended to receive cooler lubricant, and the cool line directed through one or more heat exchangers at which lubricant is cooled. The cool line then is routed to a fan drive gear for an associated gas turbine engine. A method and apparatus are disclosed.
摘要翻译：用于燃气涡轮发动机的润滑剂供应系统具有将润滑剂输送到出口管线的润滑剂润滑剂泵。出口管线被分成至少一个热管线并进入冷却管线，热管线主要指向与不用于接收较冷润滑剂的发动机相关联的位置，并且冷管线通过一个或多个热交换器哪种润滑剂被冷却。然后，冷却管线被路由到用于相关联的燃气涡轮发动机的风扇驱动齿轮。公开了一种方法和装置。

3. 发明授权

US08495857B2 Gas turbine engine thermal management system 有权
标题翻译：燃气轮机发动机热管理系统
公开(公告)号：US08495857B2
公开(公告)日：2013-07-30
申请号：US13285454
申请日：2011-10-31
申请人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips
IPC分类号： F02C7/06 , F02C1/00 , F02K99/00
CPC分类号： F02C7/14 , F02C7/08 , F02C7/185 , F02C7/224 , F05D2260/4031 , F05D2260/98
摘要： A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.
摘要翻译：用于燃气涡轮发动机的热管理系统包括提供第一调节流体的第一热交换器，与第一热交换器串联流动连通的第二热交换器，并与第一调节流体交换热量以提供第二调节流体，以及与所述第二热交换器并联流动连通的第三热交换器，并且与所述第一调节流体选择性地交换热量以提供第三调节流体。第二调理流体和第三调理流体组合以提供混合的调节流体。包括第一温度的混合调节流体的第一部分被传送到第一发动机系统。包括第二温度的混合调节流体的第二部分被传递到第二发动机系统。第二温度包括比第一温度更高的温度。

4. 发明申请

US20130104559A1 GAS TURBINE ENGINE THERMAL MANAGEMENT SYSTEM 有权
标题翻译：气体涡轮发动机热管理系统
公开(公告)号：US20130104559A1
公开(公告)日：2013-05-02
申请号：US13285454
申请日：2011-10-31
申请人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips
发明人： Federico Papa , Thomas G. Phillips , Kathleen R. Phillips
IPC分类号： F02C7/141 , F01P9/00 , F02C3/00
CPC分类号： F02C7/14 , F02C7/08 , F02C7/185 , F02C7/224 , F05D2260/4031 , F05D2260/98
摘要： A thermal management system for a gas turbine engine includes a first heat exchanger that provides a first conditioned fluid, a second heat exchanger in series flow communication with the first heat exchanger and that exchanges heat with the first conditioned fluid to provide a second conditioned fluid, and a third heat exchanger in parallel flow communication with the second heat exchanger and that selectively exchanges heat with the first conditioned fluid to provide a third conditioned fluid. The second conditioned fluid and the third conditioned fluid combine to provide a mixed conditioned fluid. A first portion of the mixed conditioned fluid including a first temperature is communicated to a first engine system. A second portion of the mixed conditioned fluid including a second temperature is communicated to a second engine system. The second temperature includes a greater temperature than the first temperature.
摘要翻译：用于燃气涡轮发动机的热管理系统包括提供第一调节流体的第一热交换器，与第一热交换器串联流动连通的第二热交换器，并与第一调节流体交换热量以提供第二调节流体，以及与所述第二热交换器并联流动连通的第三热交换器，并且与所述第一调节流体选择性地交换热量以提供第三调节流体。第二调理流体和第三调理流体组合以提供混合的调节流体。包括第一温度的混合调节流体的第一部分被传送到第一发动机系统。包括第二温度的混合调节流体的第二部分被传递到第二发动机系统。第二温度包括比第一温度更高的温度。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式