公开(公告)号：US20100074736A1

公开(公告)日：2010-03-25

申请号：US12284391

申请日：2008-09-22

Applicant: Larry Allen Junod

Inventor： Larry Allen Junod

IPC: F02C7/141 ,  F02C9/18 ,  F02C3/32

CPC classification number: F02C7/14 ,  F02C3/32 ,  F02K1/825 ,  F05D2260/601 ,  F41A13/10 ,  F41H13/0043 ,  Y02T50/675

Abstract: In one embodiment a gas turbine engine is disclosed having a heat exchanger at least partially disposed in a bypass duct. In one form the gas turbine engine is a high bypass ratio engine. The heat exchanger may be coupled with a directed energy weapon to provide coolant flow and regulate the temperature of the directed energy weapon. Other devices may also be coupled with the heat exchanger, either as an alternative to in addition to the directed energy weapon.

Abstract translation: 在一个实施例中，公开了一种具有至少部分地布置在旁路管道中的热交换器的燃气涡轮发动机。 在一种形式中，燃气涡轮发动机是高旁路比发动机。 热交换器可以与定向能量武器联接以提供冷却剂流动并调节定向能量武器的温度。 除了定向能量武器之外，其它装置也可以与热交换器耦合，作为替代。

公开(公告)号：US08544256B2

公开(公告)日：2013-10-01

申请号：US12214703

申请日：2008-06-20

Applicant: Larry Allen Junod

Inventor： Larry Allen Junod

IPC: F02K99/00 ,  F25B1/00 ,  F04D29/44

CPC classification number: F02C7/141 ,  F01D15/00 ,  F01D15/08 ,  F05D2260/205 ,  Y02T50/676

Abstract: One embodiment of a heat exchange system is disclosed having a heat exchange compressor and multiple evaporators capable of operating at different heat transfer requirements. The heat exchange compressor may be a single-stage or multi-stage compressor. In one form the evaporators return working fluid in separate streams to the heat exchange compressor. The heat exchange compressor may be integrated with a gas turbine engine and includes a number of inlets that correspond to a number of separate evaporators. Each inlet can be configured to receive working fluid at different locations within a pressure and velocity flow field created in the compressor. The heat exchange compressor may be driven by a shaft of the gas turbine engine and may be positioned at a variety of locations.

公开(公告)号：US08157503B2

公开(公告)日：2012-04-17

申请号：US12284391

申请日：2008-09-22

Applicant: Larry Allen Junod

Inventor： Larry Allen Junod

IPC: F01D25/08 ,  F04D29/58

CPC classification number: F02C7/14 ,  F02C3/32 ,  F02K1/825 ,  F05D2260/601 ,  F41A13/10 ,  F41H13/0043 ,  Y02T50/675

Abstract: In one embodiment a gas turbine engine is disclosed having a heat exchanger at least partially disposed in a bypass duct. In one form the gas turbine engine is a high bypass ratio engine. The heat exchanger may be coupled with a directed energy weapon to provide coolant flow and regulate the temperature of the directed energy weapon. Other devices may also be coupled with the heat exchanger, either as an alternative to in addition to the directed energy weapon.

Abstract translation: 在一个实施例中，公开了一种具有至少部分地布置在旁路管道中的热交换器的燃气涡轮发动机。 在一种形式中，燃气涡轮发动机是高旁路比发动机。 热交换器可以与定向能量武器联接以提供冷却剂流动并调节定向能量武器的温度。 除了定向能量武器之外，其它装置也可以与热交换器耦合，作为替代。

公开(公告)号：US20090314006A1

公开(公告)日：2009-12-24

申请号：US12214703

申请日：2008-06-20

Applicant: Larry Allen Junod

Inventor： Larry Allen Junod

IPC: F02C7/141

CPC classification number: F02C7/141 ,  F01D15/00 ,  F01D15/08 ,  F05D2260/205 ,  Y02T50/676

Abstract: One embodiment of a heat exchange system is disclosed having a heat exchange compressor and multiple evaporators capable of operating at different heat transfer requirements. The heat exchange compressor may be a single-stage or multi-stage compressor. In one form the evaporators return working fluid in separate streams to the heat exchange compressor. The heat exchange compressor may be integrated with a gas turbine engine and includes a number of inlets that correspond to a number of separate evaporators. Each inlet can be configured to receive working fluid at different locations within a pressure and velocity flow field created in the compressor. The heat exchange compressor may be driven by a shaft of the gas turbine engine and may be positioned at a variety of locations.

Abstract translation: 公开了一种具有热交换压缩机和能够以不同传热要求运行的多个蒸发器的热交换系统的一个实施例。 热交换压缩机可以是单级或多级压缩机。 在一种形式中，蒸发器将分离的流中的工作流体返回到热交换压缩机。 热交换压缩机可以与燃气涡轮发动机集成，并且包括对应于多个分开的蒸发器的多个入口。 每个入口可以被配置为在压缩机内产生的压力和速度流场内的不同位置处接收工作流体。 热交换压缩机可以由燃气涡轮发动机的轴驱动，并且可以位于各种位置。