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1. 发明申请

US20050035119A1 Liner for an insulated container 审中-公开
标题翻译：隔热容器的衬里
公开(公告)号：US20050035119A1
公开(公告)日：2005-02-17
申请号：US10639993
申请日：2003-08-13
申请人： Kenneth Hull , Sean O'Brien , Fred Reber , David Sander , Thomas Scherer , Stephanie Schneider
发明人： Kenneth Hull , Sean O'Brien , Fred Reber , David Sander , Thomas Scherer , Stephanie Schneider
IPC分类号： B65D81/38 , B65D21/02
CPC分类号： B65D81/3825
摘要： A removable container liner for a rigid insulating container includes a bottom portion and a wall portion formed as a single unitary body. The body may be composed of a stain resistant and odor resistant plastic. The liner may be configured to be used within an insulated container such as a cooler or water jug.
摘要翻译：用于刚性绝缘容器的可移除的容器衬里包括底部和形成为单个整体的壁部。身体可以由抗污渍和抗气味塑料组成。衬里可以被配置成在诸如冷却器或水壶之类的绝热容器内使用。

2. 发明申请

US20050035120A1 Freezable container for a cooler 审中-公开
标题翻译：可冷却容器
公开(公告)号：US20050035120A1
公开(公告)日：2005-02-17
申请号：US10639994
申请日：2003-08-13
申请人： Kenneth Hull , Sean O'Brien , Fred Reber , David Sander , Thomas Scherer , Stephanie Schneider
发明人： Kenneth Hull , Sean O'Brien , Fred Reber , David Sander , Thomas Scherer , Stephanie Schneider
IPC分类号： A45C11/20 , B65D81/38 , F25D3/06 , B65D21/02
CPC分类号： B65D81/3825 , A45C11/20 , A45C2013/026 , B65D81/382 , F25D3/06 , F25D2303/082 , F25D2303/0832 , F25D2331/804
摘要： A freezable container includes a base portion and may include a lid. The base portion may include a cold-retaining medium layer and be configured to be freezable to maintain a chilled environment for stored content. The freezable container may be configured to fit inside an insulated container such as a cooler.
摘要翻译：可冷冻容器包括基部并且可以包括盖。基部可以包括冷保持介质层，并且被配置为可冷冻保持用于存储的内容物的冷冻环境。可冷冻容器可以被配置成装在诸如冷却器的绝热容器内。

3. 发明申请

US20050189360A1 Laundry basket with hip hugging feature 审中-公开
标题翻译：具有臀部拥抱功能的洗衣篮
公开(公告)号：US20050189360A1
公开(公告)日：2005-09-01
申请号：US11009722
申请日：2004-12-10
申请人： Brandi Loucks , Thomas Scherer , Fred Reber
发明人： Brandi Loucks , Thomas Scherer , Fred Reber
IPC分类号： D06F29/00 , D06F95/00
CPC分类号： D06F95/002
摘要： A laundry basket has a bottom panel with a perimeter. A contiguous side wall extends generally upward from the perimeter of the bottom panel and terminates at an upper end. A basket interior is defined above the bottom panel and bounded by the side wall. A curved wall section of the side wall is curved concavely inward toward the basket interior. The bottom panel and the contiguous side wall, including the curved wall section, are formed of a primary material. A cushion pad is positioned generally at the upper end of the curved wall section and is formed from a secondary material that is softer than the primary material of the curved wall portion.
摘要翻译：洗衣篮具有带有周边的底板。连续的侧壁从底板的周边大致向上延伸并终止于上端。篮子内部被限定在底板上方并且由侧壁限定。侧壁的弯曲壁部分朝向篮内部凹入地向内弯曲。包括弯曲壁部分的底板和相邻侧壁由主要材料形成。缓冲垫通常位于弯曲壁部分的上端，并且由比弯曲壁部分的主要材料软的次级材料形成。

4. 发明授权

US08403264B2 Air inlet valve for an airplane and manufacturing method for an air inlet valve 有权
标题翻译：用于飞机的进气阀和进气阀的制造方法
公开(公告)号：US08403264B2
公开(公告)日：2013-03-26
申请号：US12948877
申请日：2010-11-18
申请人： Thorsten Schiek , Markus Petrac , Thomas Scherer
发明人： Thorsten Schiek , Markus Petrac , Thomas Scherer
IPC分类号： B64C1/14 , F02K1/12 , F02K1/38
CPC分类号： B64D13/00 , B64D2241/00 , Y02T50/44 , Y02T50/56 , Y10T29/49412 , Y10T137/0536 , Y10T137/0645
摘要： The present invention provides an air intake valve for an aircraft and a method for the production of an air intake valve. The air intake valve has an opening region for letting ambient air through into a fuselage inner region of the aircraft and a flap for opening and closing the opening region, the opening region and the flap each having a shape which is capable of forming air vortices on edges of the opening region when ambient air flows through the air intake valve.
摘要翻译：本发明提供一种用于飞行器的进气阀和用于制造进气阀的方法。进气阀具有用于使周围空气进入飞行器的机身内部区域的开口区域和用于打开和关闭开口区域的开口区域，开口区域和翼片，每个具有能够形成空气涡流的形状当环境空气流过进气阀时，开口区域的边缘。

5. 发明申请

US20110309784A1 COUNTER ELECTRO-MOTORIC FORCE BASED FUNCTIONAL STATUS DETECTION OF AN ELECTRO-MOTOR 有权
标题翻译：基于电动力学的基于电动机的功能状态检测
公开(公告)号：US20110309784A1
公开(公告)日：2011-12-22
申请号：US13097440
申请日：2011-04-29
申请人： Jürgen Kelnhofer , Thomas Scherer , Steffen Kalsow , Alvy Biccum , John Maljanian , David Leenhouts , Walter S. Hojnowski
发明人： Jürgen Kelnhofer , Thomas Scherer , Steffen Kalsow , Alvy Biccum , John Maljanian , David Leenhouts , Walter S. Hojnowski
IPC分类号： H02P8/34
CPC分类号： H02P6/182
摘要： The present invention relates to a circuit for detecting a functional status of an electro-motor. Typical electro-motors need additional components to identify the functional status of the motor. This means additional weight for such motors determining the functional status. According to the present invention a circuit is provided using a part of a motor as a sensor for detecting the functional status of the electro-motor.
摘要翻译：本发明涉及一种用于检测电动机的功能状态的电路。典型的电动马达需要额外的部件来识别电机的功能状态。这意味着这种电机的额外重量决定了功能状态。根据本发明，使用电动机的一部分作为用于检测电动机的功能状态的传感器来提供电路。

6. 发明授权

US08061154B2 Cooling system for the cooling of heat-producing devices in an aircraft 有权
标题翻译：用于冷却飞机中的制热装置的冷却系统
公开(公告)号：US08061154B2
公开(公告)日：2011-11-22
申请号：US10584779
申请日：2004-12-30
申请人： Thomas Scherer , Matthias Witschke , Carsten Colberg
发明人： Thomas Scherer , Matthias Witschke , Carsten Colberg
IPC分类号： B60H1/32
CPC分类号： F25D17/02 , B64D11/04 , B64D13/06 , B64D2013/0629 , Y02T50/56
摘要： A cooling system for the cooling of heat producing devices in an aircraft is designed with a central cold producing device, at least one cold consumer and a cold conveyance system which connects the cold producing device and the cold consumer. With this cooling system, the cold conveyance system has at least one cooling circuit which supplies a cooled cold carrier medium from the cold producing device to at least one cold consumer and brings the cold carrier medium back to the cold producing device, so that at least one cold consumer is supplied with the cold produced in the cold producing device.
摘要翻译：用于冷却飞机中的发热装置的冷却系统设计有中央冷产生装置，至少一个冷消费者和连接冷产生装置和冷消费者的冷输送系统。通过该冷却系统，冷传送系统具有至少一个冷却回路，该冷却回路将冷却的冷载体介质从冷产生装置提供给至少一个冷消耗装置，并使冷载体介质回到冷产生装置，使得至少一个冷的消费者被供应在冷产生装置中产生的冷。

7. 发明授权

US07980928B2 Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft 有权
标题翻译：利用废气热量加热飞机舱底的布置和方法
公开(公告)号：US07980928B2
公开(公告)日：2011-07-19
申请号：US11311535
申请日：2005-12-19
申请人： Michael Markwart , Thomas Scherer , Oliver Schaumann
发明人： Michael Markwart , Thomas Scherer , Oliver Schaumann
IPC分类号： B64D13/00 , B64D11/00 , B60H1/00
CPC分类号： B64D13/06 , B64D2013/0648 , Y02T50/56
摘要： The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer unit via a first air supply pipe, through which a bilge air flow drawn in from the bilge area flows into the heat transfer unit, wherein the heat transfer unit comprises a second air supply pipe, through which a waste air heat flow to be cooled that is created at another location in the aircraft flows into the heat transfer unit in order to heat the drawn-in bilge air flow, wherein the heat transfer unit comprises a first air discharge pipe, through which the cooled waste air heat flow is discharged, and a second air discharge pipe with a bilge inlet section, and wherein at least a portion of the heated bilge flow is returned to the bilge area via the air discharge pipe and the bilge inlet section.
摘要翻译：本申请描述了一种用于利用废气的热量来加热飞机舱底区域的布置和方法，其中舱底区域经由第一空气供应管连接到传热单元，通过该第一空气供应管，从舱底区域流入传热单元，其中传热单元包括第二空气供应管，通过该第二空气供应管，在飞机中的另一位置处产生的待冷却的废气热流按顺序流入传热单元加热吸入舱底空气流，其中传热单元包括排出冷却的废气热流的第一排气管和具有舱底入口段的第二排气管，并且其中至少一个加热的舱底流的一部分经由排气管和舱底入口部返回到舱底区域。

8. 发明授权

US07922118B2 System for producing process air 有权
标题翻译：生产工艺空气的系统
公开(公告)号：US07922118B2
公开(公告)日：2011-04-12
申请号：US11573531
申请日：2005-08-10
申请人： Juergen Kelnhofer , Thomas Scherer
发明人： Juergen Kelnhofer , Thomas Scherer
IPC分类号： B64D11/00
CPC分类号： B64D13/02 , B64D13/06 , B64D2013/0677 , F28D2021/0021 , Y02T50/44
摘要： A system for the provision of process air comprises a first cooling system (2) with a first heat exchanger, which is arranged in a channel (3) that serves as a cooling sink, and a cooling system (8), integrated in the first cooling system (2), wherein said cooling system (8) comprises a heat exchanger (9) which is integrated in the channel (3) either upstream or downstream of the first heat exchanger.
摘要翻译：一种用于提供处理空气的系统包括具有第一热交换器的第一冷却系统（2），其布置在用作冷却槽的通道（3）中，以及冷却系统（8），其集成在第一冷却系统（2），其中所述冷却系统（8）包括在第一热交换器的上游或下游集成在通道（3）中的热交换器（9）。

9. 发明申请

US20100267323A1 Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft 有权
标题翻译：用于控制进入客机客舱区域的进料空气温度的方法
公开(公告)号：US20100267323A1
公开(公告)日：2010-10-21
申请号：US12824898
申请日：2010-06-28
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： B64D13/08 , B64D13/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

10. 发明授权

US07775447B2 Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权
标题翻译：用于控制喷射到客机的客舱区域中的进料空气的温度的方法
公开(公告)号：US07775447B2
公开(公告)日：2010-08-17
申请号：US10582595
申请日：2004-12-30
申请人： Thomas Scherer , Michael Markwart , Torsten Schwan
发明人： Thomas Scherer , Michael Markwart , Torsten Schwan
IPC分类号： F24F11/00 , B60H1/00 , F24F3/00
CPC分类号： B64D13/00 , B64D13/08 , B64D2013/0655 , Y10S62/05
摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.
摘要翻译：使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

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