公开(公告)号：US08313062B2

公开(公告)日：2012-11-20

申请号：US12534997

申请日：2009-08-04

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： B64D1/00

CPC分类号： B64C1/1453 ,  B64D1/16 ,  B64D37/26

摘要： The invention relates to a deflector for an aircraft, comprising a discharge pipe for leading a fluid to be drained from the aircraft by way of an outlet end to the environment of the aircraft; an actuator, coupled to the discharge pipe, for swinging out, when required, the discharge pipe to at least one activation position, wherein in the activation position the outlet end is arranged so as to be spaced apart from the exterior skin of the aircraft, and the deflector guides the fluid to be drained so that it exits outside a flow boundary layer that is present on the exterior skin. The deflector according to the invention is activated when required and is able to discharge structure-damaging fluids to the environment in such a way that the exterior structure of the aircraft does not become wet, and at the same time the deflector according to the invention, normally accommodated within the contour of the aircraft, does not result in any additional aerodynamic resistance.

摘要翻译： 本发明涉及一种用于飞机的偏转器，包括排出管，用于将通过出口端从飞机排出的流体引导到飞行器的环境; 联接到排放管的致动器，用于在需要时将排放管摆放到至少一个启动位置，其中在致动位置中，出口端被布置成与飞行器的外表面间隔开， 并且偏转器引导要排出的流体，使得其流出外部皮肤上存在的流动边界层的外部。 根据本发明的偏转器在需要时被激活，并且能够以使得飞行器的外部结构不变湿的方式将结构破坏性流体排放到环境中，并且同时根据本发明的偏转器， 通常容纳在飞行器的轮廓内，不会产生任何额外的空气阻力。

公开(公告)号：US09188374B2

公开(公告)日：2015-11-17

申请号：US13428050

申请日：2012-03-23

申请人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

发明人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

IPC分类号： F25B41/00 ,  F25B1/00 ,  F25B23/00

CPC分类号： F25B41/00 ,  F25B1/00 ,  F25B23/006 ,  F25B2600/13 ,  Y02B30/745

摘要： A cooling system for cooling food on board an aircraft includes a cooling circuit adapted to supply cooling energy to at least one cooling station, a refrigerant circulating in the cooling circuit selected such that it is convertible at least partially from the liquid to the gaseous state of aggregation on releasing its cooling energy to the at least one cooling station and subsequently convertible back at least partially to the liquid state of aggregation again by an appropriate pressure and temperature control in the cooling circuit, and a refrigerant container including a receiving space arranged in an interior space of the refrigerant container which receives the refrigerant circulating in the cooling circuit, the receiving space of the refrigerant container connected to the cooling circuit by a flow line for discharging the refrigerant from the receiving space and by a return line for returning the refrigerant into the receiving space.

摘要翻译： 一种用于冷却飞机上的食物的冷却系统，包括适于向至少一个冷却站供应冷却能量的冷却回路，选择冷却回路中循环的制冷剂，使其至少部分地从液体转变为气态 在至少一个冷却站释放其冷却能量并且随后通过冷却回路中的适当的压力和温度控制再次可转换回到聚集的液体状态的聚集;以及制冷剂容器，其包括布置在 接收在冷却回路中循环的制冷剂的制冷剂容器的内部空间，通过用于从制冷剂从容纳空间排出的流路的冷却回路连接的制冷剂容器的容纳空间和用于使制冷剂返回的返回管 接收空间。

公开(公告)号：US07992821B2

公开(公告)日：2011-08-09

申请号：US11946080

申请日：2007-11-28

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： B64C1/06

CPC分类号： B64C1/12 ,  B64C1/06

摘要： An arrangement (10) for installing a component (12) in an aircraft comprises a guide device (14) which is connectable to an aircraft structure or is formed integrally with the aircraft structure, as well as an elastically deformable damping element (16; 16a, 16b, 16c) which is adapted to enable the component (12) to be mounted in the guide device (14) in a self-supporting manner. A locking mechanism (26) is adapted to fasten the component (12) in a desired position in the guide device (14) in a releasable manner.

摘要翻译： 用于在飞行器中安装部件（12）的装置（10）包括可连接到飞行器结构或与飞机结构一体形成的引导装置（14），以及可弹性变形的阻尼元件（16; 16a ，16b，16c），其适于使得部件（12）以自支撑的方式安装在引导装置（14）中。 锁定机构（26）适于以可释放的方式将部件（12）紧固在引导装置（14）中的期望位置。

公开(公告)号：US20100300661A1

公开(公告)日：2010-12-02

申请号：US12809896

申请日：2008-11-24

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： F28B9/10

CPC分类号： B01F5/0471 ,  B01F5/0413 ,  B01F5/049 ,  B64D41/00 ,  B64D2033/045 ,  B64D2041/002 ,  Y02T50/44

摘要： The invention relates to a device for cooling hot gas to be discharged from an aircraft, having a duct for leading the hot gas from a hot gas source which is connectable to the device to an outlet point, and having a frame which surrounds the duct and serves for mounting the duct, the duct being formed from one or more pipe sections and having one or more cooling air inlet points which is connectable to one in or more cooling air sources in order to mix the hot gas with cooling air.

摘要翻译： 本发明涉及一种用于冷却从飞行器排出的热气体的装置，具有用于将热气体从可连接到该装置的热气体引导到出口点的管道，并且具有围绕导管的框架， 用于安装管道，该管道由一个或多个管道部分形成，并且具有一个或多个冷却空气入口点，冷却空气入口点可连接到一个或多个冷却空气源中，以便将热气体与冷却空气混合。

公开(公告)号：US20100032525A1

公开(公告)日：2010-02-11

申请号：US12534997

申请日：2009-08-04

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： B64D1/16

CPC分类号： B64C1/1453 ,  B64D1/16 ,  B64D37/26

摘要： The invention relates to a deflector for an aircraft, comprising a discharge pipe for leading a fluid to be drained from the aircraft by way of an outlet end to the environment of the aircraft; an actuator, coupled to the discharge pipe, for swinging out, when required, the discharge pipe to at least one activation position, wherein in the activation position the outlet end is arranged so as to be spaced apart from the exterior skin of the aircraft, and the deflector guides the fluid to be drained so that it exits outside a flow boundary layer that is present on the exterior skin. The deflector according to the invention is activated when required and is able to discharge structure-damaging fluids to the environment in such a way that the exterior structure of the aircraft does not become wet, and at the same time the deflector according to the invention, normally accommodated within the contour of the aircraft, does not result in any additional aerodynamic resistance.

摘要翻译： 本发明涉及一种用于飞机的偏转器，包括排出管，用于将通过出口端从飞机排出的流体引导到飞行器的环境; 联接到排放管的致动器，用于在需要时将排放管摆放到至少一个启动位置，其中在致动位置中，出口端被布置成与飞行器的外表面间隔开， 并且偏转器引导要排出的流体，使得其流出外部皮肤上存在的流动边界层的外部。 根据本发明的偏转器在需要时被激活，并且能够以使得飞行器的外部结构不变湿的方式将结构破坏性流体排放到环境中，并且同时根据本发明的偏转器， 通常容纳在飞行器的轮廓内，不会产生任何额外的空气阻力。

公开(公告)号：US20080135683A1

公开(公告)日：2008-06-12

申请号：US11951859

申请日：2007-12-06

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： B64C1/00 ,  B32B3/10

CPC分类号： F16L59/07 ,  Y10T428/24273

摘要： A thermal insulating element (10′; 10′″) comprises a first plate (24) forming at least a part of an outer face of the insulating element (10′; 10′″) and a second plate (26) forming a further part of the outer face of the insulating element (10′; 10′″). The first and the second plate (24, 26) are connected to each other via a frame structure (12) which establishes a geometry of the insulating element (10′; 10′″). The first and the second plate (24, 26) and the frame structure (12) define a cavity filled with air, wherein at least one vent opening (28) is formed in the first and/or the second plate (24, 26) and/or the frame structure (12). A projecting edge portion (34, 36) is formed along an edge of a portion of the insulating element (10′; 10′″) which is provided with the at least one vent opening (28), the projecting edge portion (34, 36) being adapted to at least partially cover a gap between two insulating elements (10′; 10′″) disposed side by side.

摘要翻译： 绝热元件（10'; 10“）包括形成绝缘元件（10'，10”）的外表面的至少一部分的第一板（24）和形成 绝缘元件（10'; 10“）的外表面的另一部分。 第一和第二板（24,26）经由构成绝缘元件（10'; 10“）的几何形状的框架结构（12）彼此连接。 第一和第二板（24,26）和框架结构（12）限定了填充有空气的空腔，其中在第一和/或第二板（24,26）中形成至少一个通气口（28） 和/或框架结构（12）。 沿着绝缘元件（10'; 10“）的一部分的边缘形成突出边缘部分（34,36），所述绝缘元件设置有至少一个通气开口（28），所述突出边缘部分（34） ，36）适于至少部分地覆盖并排布置的两个绝缘元件（10'，10“）之间的间隙。

公开(公告)号：US20130074530A1

公开(公告)日：2013-03-28

申请号：US13428050

申请日：2012-03-23

申请人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

发明人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

IPC分类号： F25B41/00 ,  F25B1/00

CPC分类号： F25B41/00 ,  F25B1/00 ,  F25B23/006 ,  F25B2600/13 ,  Y02B30/745

摘要： A cooling system for cooling food on board an aircraft includes a cooling circuit adapted to supply cooling energy to at least one cooling station, a refrigerant circulating in the cooling circuit selected such that it is convertible at least partially from the liquid to the gaseous state of aggregation on releasing its cooling energy to the at least one cooling station and subsequently convertible back at least partially to the liquid state of aggregation again by an appropriate pressure and temperature control in the cooling circuit, and a refrigerant container including a receiving space arranged in an interior space of the refrigerant container which receives the refrigerant circulating in the cooling circuit, the receiving space of the refrigerant container connected to the cooling circuit by a flow line for discharging the refrigerant from the receiving space and by a return line for returning the refrigerant into the receiving space.

摘要翻译： 一种用于冷却飞机上的食物的冷却系统，包括适于向至少一个冷却站供应冷却能量的冷却回路，选择冷却回路中循环的制冷剂，使其至少部分地从液体转变为气态 在至少一个冷却站释放其冷却能量并且随后通过冷却回路中的适当的压力和温度控制再次可转换回到聚集的液体状态的聚集;以及制冷剂容器，其包括布置在 接收在冷却回路中循环的制冷剂的制冷剂容器的内部空间，通过用于从制冷剂从容纳空间排出的流路的冷却回路连接的制冷剂容器的容纳空间和用于使制冷剂返回的返回管 接收空间。

公开(公告)号：US08371522B2

公开(公告)日：2013-02-12

申请号：US12809896

申请日：2008-11-24

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： A01K1/10

CPC分类号： B01F5/0471 ,  B01F5/0413 ,  B01F5/049 ,  B64D41/00 ,  B64D2033/045 ,  B64D2041/002 ,  Y02T50/44

摘要： A device for cooling hot gas to be discharged from an aircraft includes a duct for leading the hot gas from a hot gas source which is connectable to the device to an outlet point, and a frame which surrounds the duct and serves for mounting the duct. The duct is formed from one or more pipe sections and has one or more cooling air inlet points which is connectable to one or more cooling air sources in order to mix the hot gas with cooling air. An outlet pipe section of the duct extends outwards beyond the aircraft outer skin to lead hot gas through and out of a flow boundary layer on the outer skin.

摘要翻译： 用于冷却从飞行器排出的热气体的装置包括用于将来自可连接到装置的热气体源的热气体引导到出口点的管道，以及围绕管道并用于安装管道的框架。 管道由一个或多个管道部分形成，并且具有一个或多个冷却空气入口点，其可连接到一个或多个冷却空气源，以便将热气体与冷却空气混合。 管道的出口管部分向外延伸超出飞行器外皮，引导热气体通过和流出外皮上的流动边界层。

公开(公告)号：US08079194B2

公开(公告)日：2011-12-20

申请号：US11951859

申请日：2007-12-06

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： E04D1/00

CPC分类号： F16L59/07 ,  Y10T428/24273

摘要： A thermal insulating element (10′; 10′″) comprises a first plate (24) forming at least a part of an outer face of the insulating element (10′; 10′″) and a second plate (26) forming a further part of the outer face of the insulating element (10′; 10′″). The first and the second plate (24, 26) are connected to each other via a frame structure (12) which establishes a geometry of the insulating element (10′; 10′″). The first and the second plate (24, 26) and the frame structure (12) define a cavity filled with air, wherein at least one vent opening (28) is formed in the first and/or the second plate (24, 26) and/or the frame structure (12). A projecting edge portion (34, 36) is formed along an edge of a portion of the insulating element (10′; 10′″) which is provided with the at least one vent opening (28), the projecting edge portion (34, 36) being adapted to at least partially cover a gap between two insulating elements (10′; 10′″) disposed side by side.

摘要翻译： 绝热元件（10'; 10“）包括形成绝缘元件（10'; 10”）的外表面的至少一部分的第一板（24）和形成另外的绝缘元件 绝缘元件（10'; 10“）的外表面的一部分。 第一和第二板（24,26）经由构成绝缘元件（10'; 10“）的几何形状的框架结构（12）彼此连接。 第一和第二板（24,26）和框架结构（12）限定了填充有空气的空腔，其中在第一和/或第二板（24,26）中形成至少一个通气口（28） 和/或框架结构（12）。 沿着绝缘元件（10'; 10“）的一部分的边缘形成突出边缘部分（34,36），该边缘设置有至少一个通气开口（28），所述突出边缘部分（34） 36）适于至少部分地覆盖并排设置的两个绝缘元件（10'; 10“）之间的间隙。

公开(公告)号：US20100269328A1

公开(公告)日：2010-10-28

申请号：US12809910

申请日：2008-11-10

申请人： Markus Piesker

发明人： Markus Piesker

IPC分类号： B23P19/00

CPC分类号： B64D41/00 ,  B64D2033/045 ,  B64D2041/002 ,  F01D25/30 ,  F01N13/1816 ,  F02K1/04 ,  F02K1/80 ,  F05D2220/50 ,  F16L27/111 ,  F16L59/21 ,  Y02T50/671 ,  Y10T29/53

摘要： Device for mechanically decoupled retention of components perfused by hot gas in an aircraft, with a coupling member for coupling to a component emitting hot gas and to a component accepting hot gas, with a holder, with a flange, and with a bellows, the holder being fittable to a housing or frame connected to the component emitting hot gas, the bellows being fastened by one end to the flange and by the other end to the holder, and the coupling member being fastened to the flange. By virtue of the device, both an angular misalignment and radial and axial positional misalignment can be equalised.

摘要翻译： 用于机械地分离保留在飞行器中被热气体灌注的部件的装置，具有用于与发射热气体的部件耦合的耦合部件和接收热气体的部件，具有凸缘的保持器和波纹管，所述保持器 适用于与发出热气体的部件连接的外壳或框架，波纹管由一端固定在凸缘上，另一端固定在支架上，连接件固定在凸缘上。 通过该装置，可以均衡角度偏差和径向和轴向位置偏移。