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公开(公告)号：US09422060B2
公开(公告)日：2016-08-23
申请号：US13979065
申请日：2012-01-06
Applicant: Stephen John Richard Smith , Kieran James Watt
Inventor： Stephen John Richard Smith , Kieran James Watt
CPC classification number: B64D13/00 , B64D13/06 , B64D13/08 , B64D15/02 , B64D2013/0614 , B64D2013/0633 , B64F1/362 , Y02T50/56
Abstract: A method and apparatus are disclosed for a turboprop-powered medium altitude long endurance (MALE) aircraft, having: a heat exchanger with a heat-storage material, for example a heat-storage wax; and an air recirculation path. The heat exchanger can be arranged to cool air recirculating around the air recirculation path which is arranged to provide cooling to the MALE aircraft, for example to an equipment bay. The heat-storage material may be cooled by ground-based cooling apparatus when the aircraft is on the ground and/or by ram air when the aircraft is in flight. The heat-storage material may have a melting point selected so as to be rendered solid during ground-based cooling and/or ram air cooling, and/or selected so as to undergo melting while cooling the air recirculating around the air recirculation path.
Abstract translation: 公开了一种用于涡轮螺旋桨发动机的中等高度长寿命（MALE）飞行器的方法和装置，其具有：具有储热材料的热交换器，例如储热蜡; 和空气再循环路径。 热交换器可以布置成冷却空气再循环路径周围循环的空气，该空气循环路径被布置成向MALE飞机提供冷却，例如到设备舱。 当飞机在飞行中时，飞机在地面上和/或冲压空气时，储热材料可以被地面冷却装置冷却。 储热材料可以具有选择的熔点，以在基于地面的冷却和/或冲压空气冷却期间变得固体，和/或选择为在冷却在空气再循环路径周围循环的空气的同时进行熔融。
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公开(公告)号：US09429076B2
公开(公告)日：2016-08-30
申请号：US13979120
申请日：2012-01-06
Applicant: Stephen John Richard Smith , Kieran James Watt , Andrew Charles White
Inventor： Stephen John Richard Smith , Kieran James Watt , Andrew Charles White
CPC classification number: F02C7/24 , B64C39/024 , B64C2201/044 , B64D13/08 , B64D15/02 , B64D15/04 , B64D27/10 , B64D33/08 , B64D2013/0607 , B64D2013/0614 , B64D2013/0648 , B64D2013/0674 , F28D2020/0013 , F28D2020/0017 , F28F13/003 , Y02T50/56
Abstract: A turboprop-powered medium altitude long endurance aircraft, having a gas turbine engine; a heat scavenging device to scavenge heat from the gas turbine engine; and a heating device to use the scavenged heat to provide heating to the aircraft. The heat scavenging device may be placed on an engine casing and/or on or in an engine exhaust duct. The heating device may include a circulation path routed directly to a location in the aircraft where heating is to be performed, for example a leading edge of an engine support pylon or a leading edge of an engine-carrying wing. The heating device can include a heat exchanger.
Abstract translation: 具有燃气涡轮发动机的涡轮螺旋桨发动机中型高空耐久型飞机; 用于清除来自燃气涡轮发动机的热的除热装置; 以及使用清扫热量来向飞机提供加热的加热装置。 除热装置可以放置在发动机壳体上和/或在发动机排气管道上或发动机排气管道中。 加热装置可以包括直接路由到飞行器中要进行加热的位置的循环路径，例如发动机支撑塔的前缘或发动机承载翼的前缘。 加热装置可以包括热交换器。
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公开(公告)号：US20130283816A1
公开(公告)日：2013-10-31
申请号：US13979120
申请日：2012-01-06
Applicant: Stephen John Richard Smith , Kieran James Watt , Andrew Charles White
Inventor： Stephen John Richard Smith , Kieran James Watt , Andrew Charles White
IPC: F02C7/24
CPC classification number: F02C7/24 , B64C39/024 , B64C2201/044 , B64D13/08 , B64D15/02 , B64D15/04 , B64D27/10 , B64D33/08 , B64D2013/0607 , B64D2013/0614 , B64D2013/0648 , B64D2013/0674 , F28D2020/0013 , F28D2020/0017 , F28F13/003 , Y02T50/56
Abstract: A turboprop-powered medium altitude long endurance aircraft, having a gas turbine engine; a heat scavenging device to scavenge heat from the gas turbine engine; and a heating device to use the scavenged heat to provide heating to the aircraft. The heat scavenging device may be placed on an engine casing and/or on or in an engine exhaust duct. The heating device may include a circulation path routed directly to a location in the aircraft where heating is to be performed, for example a leading edge of an engine support pylon or a leading edge of an engine-carrying wing. The heating device can include a heat exchanger.
Abstract translation: 具有燃气涡轮发动机的涡轮螺旋桨发动机中型高空耐久型飞机; 用于清除来自燃气涡轮发动机的热的除热装置; 以及使用清扫热量来向飞机提供加热的加热装置。 除热装置可以放置在发动机壳体上和/或在发动机排气管道上或发动机排气管道中。 加热装置可以包括直接路由到飞行器中要进行加热的位置的循环路径，例如发动机支撑塔的前缘或发动机承载翼的前缘。 加热装置可以包括热交换器。
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