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1. 发明授权

US08634972B2 Method and system for integrating engine control and flight control system 有权
标题翻译：整合发动机控制和飞行控制系统的方法和系统
公开(公告)号：US08634972B2
公开(公告)日：2014-01-21
申请号：US13221102
申请日：2011-08-30
申请人： Harry Kirk Mathews, Jr. , Sridhar Adibhatla , Jeffrey Russell Bult
发明人： Harry Kirk Mathews, Jr. , Sridhar Adibhatla , Jeffrey Russell Bult
IPC分类号： G01C23/00
CPC分类号： B64C19/00 , B64D31/06 , F05D2260/80 , H04B7/18506
摘要： A method and system of operating an aircraft system are provided. The aircraft system includes an integrated aircraft flight control system that includes an engine control system configured to generate engine performance and health information. The integrated aircraft flight control system also includes a flight control system configured to generate flight information and trajectory intent information. The integrated aircraft flight control system further includes a communications channel communicatively coupled between the engine control system and the flight control system, where the engine control system is configured to transmit the generated engine performance and health information to the flight control system using the communications channel and the flight control system is configured to transmit the generated flight information and trajectory intent information to the engine control system using the communications channel.
摘要翻译：提供了一种操作飞行器系统的方法和系统。该飞行器系统包括集成的飞行器飞行控制系统，其包括被配置为产生发动机性能和健康信息的发动机控制系统。综合飞行器飞行控制系统还包括配置成产生飞行信息和轨迹意图信息的飞行控制系统。集成飞行器飞行控制系统还包括通信地耦合在发动机控制系统和飞行控制系统之间的通信通道，其中发动机控制系统被配置为使用通信通道向飞行控制系统发送生成的发动机性能和健康信息，以及飞行控制系统被配置为使用通信信道将所生成的飞行信息和轨迹意图信息发送到引擎控制系统。

2. 发明申请

US20130054055A1 METHOD AND SYSTEM FOR INTEGRATING ENGINE CONTROL AND FLIGHT CONTROL SYSTEM 有权
标题翻译：集成发动机控制和飞行控制系统的方法和系统
公开(公告)号：US20130054055A1
公开(公告)日：2013-02-28
申请号：US13221102
申请日：2011-08-30
申请人： Harry Kirk Mathews, JR. , Sridhar Adibhatla , Jeffrey Russell Bult
发明人： Harry Kirk Mathews, JR. , Sridhar Adibhatla , Jeffrey Russell Bult
IPC分类号： G05D1/00 , G06F19/00
CPC分类号： B64C19/00 , B64D31/06 , F05D2260/80 , H04B7/18506
摘要： A method and system of operating an aircraft system are provided. The aircraft system includes an integrated aircraft flight control system that includes an engine control system configured to generate engine performance and health information. The integrated aircraft flight control system also includes a flight control system configured to generate flight information and trajectory intent information. The integrated aircraft flight control system further includes a communications channel communicatively coupled between the engine control system and the flight control system, where the engine control system is configured to transmit the generated engine performance and health information to the flight control system using the communications channel and the flight control system is configured to transmit the generated flight information and trajectory intent information to the engine control system using the communications channel.
摘要翻译：提供了一种操作飞行器系统的方法和系统。该飞行器系统包括集成的飞行器飞行控制系统，其包括被配置为产生发动机性能和健康信息的发动机控制系统。综合飞行器飞行控制系统还包括配置成产生飞行信息和轨迹意图信息的飞行控制系统。集成飞行器飞行控制系统还包括通信地耦合在发动机控制系统和飞行控制系统之间的通信通道，其中发动机控制系统被配置为使用通信通道向飞行控制系统发送生成的发动机性能和健康信息，以及飞行控制系统被配置为使用通信信道将所生成的飞行信息和轨迹意图信息发送到引擎控制系统。

3. 发明授权

US07990705B2 Systems and methods for synthetic jet enhanced natural cooling 有权
标题翻译：合成射流的系统和方法增强了自然冷却
公开(公告)号：US07990705B2
公开(公告)日：2011-08-02
申请号：US12118435
申请日：2008-05-09
申请人： Jeffrey Russell Bult , Mehmet Arik , William Dwight Gerstler , Yogen Utturkar
发明人： Jeffrey Russell Bult , Mehmet Arik , William Dwight Gerstler , Yogen Utturkar
IPC分类号： H05K7/20 , B05B1/08 , F04B17/00 , F28F7/00
CPC分类号： F15D1/08 , H01L23/4735 , H01L2924/0002 , H05K7/20909 , H01L2924/00
摘要： A method and system for increasing cooling of an enclosure is provided. The component enclosure includes one or more sidewalls defining a volume, the sidewalls are configured to substantially surround a heat generating component positioned within the volume. The component enclosure further includes a synthetic jet assembly positioned adjacent at least one of the sidewalls. The synthetic jet assembly includes at least one synthetic jet ejector having a jet port. The jet port is aligned at least one of perpendicularly, parallelly, and obliquely with a surface of the at least one sidewall. The synthetic jet assembly is configured to direct a jet of fluid through the port at least one of substantially parallel to the surface, perpendicularly onto the surface, and obliquely toward the surface.
摘要翻译：提供了一种用于增加外壳冷却的方法和系统。部件外壳包括限定一个体积的一个或多个侧壁，该侧壁被配置为基本上围绕定位在该体积内的发热部件。组件外壳还包括邻近至少一个侧壁定位的合成射流组件。合成射流组件包括具有喷射口的至少一个合成射流喷射器。喷射口与至少一个侧壁的表面垂直，平行和倾斜地至少一个排列。合成射流组件构造成将流体射流引导通过端口至少一个基本上平行于表面垂直于表面并且倾斜地朝向表面。

4. 发明申请

US20100271775A1 SYSTEMS AND METHODS FOR SYNTHETIC JET ENHANCED NATURAL COOLING 有权
标题翻译：用于合成喷射增强自然冷却的系统和方法
公开(公告)号：US20100271775A1
公开(公告)日：2010-10-28
申请号：US12118435
申请日：2008-05-09
申请人： Jeffrey Russell Bult , Mehmet Arik , William Dwight Gerstler , Yogen Utturkar
发明人： Jeffrey Russell Bult , Mehmet Arik , William Dwight Gerstler , Yogen Utturkar
IPC分类号： F28D15/00 , H05K7/20
CPC分类号： F15D1/08 , H01L23/4735 , H01L2924/0002 , H05K7/20909 , H01L2924/00
摘要： A method and system for increasing cooling of an enclosure is provided. The component enclosure includes one or more sidewalls defining a volume, the sidewalls are configured to substantially surround a heat generating component positioned within the volume. The component enclosure further includes a synthetic jet assembly positioned adjacent at least one of the sidewalls. The synthetic jet assembly includes at least one synthetic jet ejector having a jet port. The jet port is aligned at least one of perpendicularly, parallelly, and obliquely with a surface of the at least one sidewall. The synthetic jet assembly is configured to direct a jet of fluid through the port at least one of substantially parallel to the surface, perpendicularly onto the surface, and obliquely toward the surface.
摘要翻译：提供了一种用于增加外壳冷却的方法和系统。部件外壳包括限定一个体积的一个或多个侧壁，该侧壁被配置为基本上围绕定位在该体积内的发热部件。组件外壳还包括邻近至少一个侧壁定位的合成射流组件。合成射流组件包括具有喷射口的至少一个合成射流喷射器。喷射口与至少一个侧壁的表面垂直，平行和倾斜地至少一个排列。合成射流组件构造成将流体射流引导通过端口至少一个基本上平行于表面垂直于表面并且倾斜地朝向表面。

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