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1. 发明申请

US20120321448A1 AIRCRAFT POWERPLANT 有权
标题翻译：飞机POWERPLANT
公开(公告)号：US20120321448A1
公开(公告)日：2012-12-20
申请号：US13523489
申请日：2012-06-14
申请人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
发明人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
IPC分类号： F01D25/00 , F01D1/04
CPC分类号： F02K3/077 , F02C7/18 , F02K3/115 , Y02T50/675
摘要： A gas turbine engine system is disclosed which includes a core passage and a bypass passage which can be configured as a fan bypass duct or a third stream bypass duct. The core passage and bypass passage are routed to flow through a nozzle before exiting overboard an aircraft. The nozzle includes moveable members capable of changing a configuration of the nozzle. In one form the moveable members are capable of changing throat areas for portions of the nozzle that receive working fluid from the core passage and the bypass passage. The bypass passage can include a branch. In one form the branch can include a heat exchanger. The bypass passage can also provide cooling to one or more portions of the nozzle, such as cooling to a deck of the nozzle.
摘要翻译：公开了一种燃气涡轮发动机系统，其包括可以构造为风扇旁通管道或第三流旁路管道的铁芯通道和旁路通道。核心通道和旁路通道在离开飞机之前通过喷嘴流动。喷嘴包括能够改变喷嘴的构造的可动构件。在一种形式中，可移动构件能够改变用于从芯通道和旁路通道接收工作流体的喷嘴的部分的喉部区域。旁路通道可以包括一个分支。在一种形式中，分支可以包括热交换器。旁路通道还可以向喷嘴的一个或多个部分提供冷却，例如冷却到喷嘴的甲板上。

2. 发明授权

US09091229B2 Aircraft powerplant 有权
标题翻译：飞机发动机
公开(公告)号：US09091229B2
公开(公告)日：2015-07-28
申请号：US13523489
申请日：2012-06-14
申请人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
发明人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
IPC分类号： F01D25/00 , F02K3/077 , F02K3/115 , F02C7/18
CPC分类号： F02K3/077 , F02C7/18 , F02K3/115 , Y02T50/675
摘要： A gas turbine engine system is disclosed which includes a core passage and a bypass passage which can be configured as a fan bypass duct or a third stream bypass duct. The core passage and bypass passage are routed to flow through a nozzle before exiting overboard an aircraft. The nozzle includes moveable members capable of changing a configuration of the nozzle. In one form the moveable members are capable of changing throat areas for portions of the nozzle that receive working fluid from the core passage and the bypass passage. The bypass passage can include a branch. In one form the branch can include a heat exchanger. The bypass passage can also provide cooling to one or more portions of the nozzle, such as cooling to a deck of the nozzle.
摘要翻译：公开了一种燃气涡轮发动机系统，其包括可以构造为风扇旁通管道或第三流旁路管道的铁芯通道和旁路通道。核心通道和旁路通道在离开飞机之前通过喷嘴流动。喷嘴包括能够改变喷嘴的构造的可动构件。在一种形式中，可移动构件能够改变用于从芯通道和旁路通道接收工作流体的喷嘴的部分的喉部区域。旁路通道可以包括一个分支。在一种形式中，分支可以包括热交换器。旁路通道还可以向喷嘴的一个或多个部分提供冷却，例如冷却到喷嘴的甲板上。

3. 发明申请

US20120317957A1 AIRCRAFT POWERPLANT 有权
标题翻译：飞机POWERPLANT
公开(公告)号：US20120317957A1
公开(公告)日：2012-12-20
申请号：US13523315
申请日：2012-06-14
申请人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
发明人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
IPC分类号： F02K3/02 , F02K99/00 , F02K1/46
CPC分类号： F02K3/077 , F02C7/18 , F02K3/115 , Y02T50/675
摘要： A gas turbine engine system is disclosed which includes a core passage and a bypass passage which can be configured as a fan bypass duct or a third stream bypass duct. The core passage and bypass passage are routed to flow through a nozzle before exiting overboard an aircraft. The nozzle includes moveable members capable of changing a configuration of the nozzle. In one form the moveable members are capable of changing throat area for portions of the nozzle that receive working fluid from the core passage and the bypass passage. The bypass passage can include a branch. In one form the branch can include a heat exchanger. The bypass passage can also provide cooling to one or more portions of the nozzle, such as cooling to a deck of the nozzle.
摘要翻译：公开了一种燃气涡轮发动机系统，其包括可以构造为风扇旁通管道或第三流旁路管道的铁芯通道和旁路通道。核心通道和旁路通道在离开飞机之前通过喷嘴流动。喷嘴包括能够改变喷嘴的构造的可动构件。在一种形式中，可移动构件能够改变从芯通道和旁路通道接收工作流体的喷嘴的部分的喉部区域。旁路通道可以包括一个分支。在一种形式中，分支可以包括热交换器。旁路通道还可以向喷嘴的一个或多个部分提供冷却，例如冷却到喷嘴的甲板上。

4. 发明授权

US10001084B2 Aircraft powerplant with moveable nozzle member 有权
公开(公告)号：US10001084B2
公开(公告)日：2018-06-19
申请号：US13523315
申请日：2012-06-14
申请人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
发明人： Kenneth M. Pesyna , Bryan Henry Lerg , Michael Abraham Karam
IPC分类号： F02K3/077 , F02K3/115 , F02C7/18
CPC分类号： F02K3/077 , F02C7/18 , F02K3/115 , Y02T50/675
摘要： A gas turbine engine system is disclosed which includes a core passage and a bypass passage which can be configured as a fan bypass duct or a third stream bypass duct. The core passage and bypass passage are routed to flow through a nozzle before exiting overboard an aircraft. The nozzle includes moveable members capable of changing a configuration of the nozzle. In one form the moveable members are capable of changing throat area for portions of the nozzle that receive working fluid from the core passage and the bypass passage. The bypass passage can include a branch. In one form the branch can include a heat exchanger. The bypass passage can also provide cooling to one or more portions of the nozzle, such as cooling to a deck of the nozzle.

5. 发明申请

US20120256044A1 FLIGHT VEHICLE, PROPULSION SYSTEM AND THRUST VECTORING SYSTEM 有权
标题翻译：飞行车辆，推进系统和推力系统
公开(公告)号：US20120256044A1
公开(公告)日：2012-10-11
申请号：US13336301
申请日：2011-12-23
申请人： Bryan Henry Lerg
发明人： Bryan Henry Lerg
IPC分类号： B64C15/02 , F02K1/00 , F02K1/28
CPC分类号： F02K1/28 , F02K1/002 , F02K1/008 , F05D2250/713 , F05D2270/18
摘要： One embodiment of the present invention is a unique flight vehicle. Another embodiment is a unique propulsion system. Another embodiment is a unique thrust vectoring system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for flight vehicles, propulsion systems and thrust vectoring systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译：本发明的一个实施例是独特的飞行器。另一个实施例是独特的推进系统。另一个实施例是独特的推力矢量化系统。其他实施例包括用于飞行车辆，推进系统和推力矢量系统的装置，系统，装置，硬件，方法和组合。本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。

6. 发明授权

US08783605B2 Flight vehicle, propulsion system and thrust vectoring system 有权
标题翻译：飞行器，推进系统和推力矢量系统
公开(公告)号：US08783605B2
公开(公告)日：2014-07-22
申请号：US13336301
申请日：2011-12-23
申请人： Bryan Henry Lerg
发明人： Bryan Henry Lerg
IPC分类号： B64B1/36
CPC分类号： F02K1/28 , F02K1/002 , F02K1/008 , F05D2250/713 , F05D2270/18
摘要： One embodiment of the present invention is a unique flight vehicle. Another embodiment is a unique propulsion system. Another embodiment is a unique thrust vectoring system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for flight vehicles, propulsion systems and thrust vectoring systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译：本发明的一个实施例是独特的飞行器。另一个实施例是独特的推进系统。另一个实施例是独特的推力矢量化系统。其他实施例包括用于飞行车辆，推进系统和推力矢量系统的装置，系统，装置，硬件，方法和组合。本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。

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