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1. 发明申请

US20090321607A1 Three point mounting arrangement for a power system 审中-公开
标题翻译：电力系统的三点安装方式
公开(公告)号：US20090321607A1
公开(公告)日：2009-12-31
申请号：US12216120
申请日：2008-06-30
申请人： Peter John Baron , Martin Regis Habel
发明人： Peter John Baron , Martin Regis Habel
IPC分类号： F16F15/023 , F16M13/00
CPC分类号： F16F15/022 , F16M5/00
摘要： A mounting system for supporting a power system is disclosed. The mounting system may have a support structure including a first end spaced from a second end of the support structure. The mounting system may further have a first mounting assembly attached near the first end of the support structure. The first mounting assembly may have a first mounting support and a second mounting support for supporting the support structure, each of the first mounting support and the second mounting support attached to the support structure offset to a side of a longitudinal axis. The mounting system may also have a second mounting assembly attached near the second end of the support structure. The second mounting assembly may have a third mounting support attached to the support structure below the longitudinal axis for supporting the support structure. The second mounting assembly may have at least one shock absorber mounted near the third mounting support.
摘要翻译：公开了一种用于支撑电力系统的安装系统。安装系统可以具有包括与支撑结构的第二端间隔开的第一端的支撑结构。安装系统还可以具有附接在支撑结构的第一端附近的第一安装组件。第一安装组件可以具有第一安装支撑件和用于支撑支撑结构的第二安装支撑件，第一安装支撑件和附接到支撑结构的第二安装支撑件中的每一个偏移到纵向轴线的一侧。安装系统还可以具有附接在支撑结构的第二端附近的第二安装组件。第二安装组件可以具有第三安装支撑件，该第三安装支撑件在纵向轴线下方附接到支撑结构，用于支撑支撑结构。第二安装组件可以具有安装在第三安装支架附近的至少一个减震器。

2. 发明申请

US20090060725A1 Engine with intake air temperature control system 有权
标题翻译：发动机带进气温度控制系统
公开(公告)号：US20090060725A1
公开(公告)日：2009-03-05
申请号：US12073148
申请日：2008-02-29
申请人： Peter John Baron , David Anthony Pocengal , Rainer Kurz
发明人： Peter John Baron , David Anthony Pocengal , Rainer Kurz
IPC分类号： F01D25/08
CPC分类号： F02C7/04 , F02C3/22 , F02C7/224 , F02C9/16 , F02C9/40 , F05D2270/082 , F05D2270/303 , Y02T10/16 , Y02T50/677
摘要： A gas turbine engine system includes a gas turbine engine using vaporized liquefied gas as fuel. The gas turbine engine is configured to ingest intake air from an intake port and direct exhaust gases to an exhaust port. The gas turbine engine system also includes a heat exchanger with a heat transfer fluid therein. The heat exchanger is configured to create at least a part of the fuel by heating the liquefied gas. The gas turbine engine system also includes an intake air temperature control circuit. The intake air temperature control circuit includes conduits configured to direct the heat transfer fluid to the intake port and the exhaust port. The gas turbine engine system also includes a control system configured to selectively direct the heat transfer fluid to one of the intake port and the exhaust port.
摘要翻译：燃气涡轮发动机系统包括使用气化液化气体作为燃料的燃气涡轮发动机。燃气涡轮发动机被配置为从进气口摄取进气并将排气直接排到排气口。燃气涡轮发动机系统还包括其中具有传热流体的热交换器。热交换器被配置为通过加热液化气体来产生至少一部分燃料。燃气涡轮发动机系统还包括进气温度控制电路。进气温度控制电路包括构造成将传热流体引导到进气口和排气口的导管。燃气涡轮发动机系统还包括被配置为选择性地将传热流体引导到进气口和排气口中的一个的控制系统。

3. 发明授权

US08474241B2 Engine with intake air temperature control system 有权
公开(公告)号：US08474241B2
公开(公告)日：2013-07-02
申请号：US12073148
申请日：2008-02-29
申请人： Peter John Baron , David Anthony Pocengal , Rainer Kurz
发明人： Peter John Baron , David Anthony Pocengal , Rainer Kurz
IPC分类号： F02C7/10 , F02C1/00 , F02K99/00
CPC分类号： F02C7/04 , F02C3/22 , F02C7/224 , F02C9/16 , F02C9/40 , F05D2270/082 , F05D2270/303 , Y02T10/16 , Y02T50/677
摘要： A gas turbine engine system includes a gas turbine engine using vaporized liquefied gas as fuel. The gas turbine engine is configured to ingest intake air from an intake port and direct exhaust gases to an exhaust port. The gas turbine engine system also includes a heat exchanger with a heat transfer fluid therein. The heat exchanger is configured to create at least a part of the fuel by heating the liquefied gas. The gas turbine engine system also includes an intake air temperature control circuit. The intake air temperature control circuit includes conduits configured to direct the heat transfer fluid to the intake port and the exhaust port. The gas turbine engine system also includes a control system configured to selectively direct the heat transfer fluid to one of the intake port and the exhaust port.

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