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1. 发明授权

US06168112A Double pane window for an aircraft cabin 有权
标题翻译：飞机机舱的双窗格窗口
公开(公告)号：US06168112A
公开(公告)日：2001-01-02
申请号：US09249460
申请日：1999-02-12
申请人： Rainer Mueller , Sven Uhlemann , Thomas Scherer , Heiko Luetjens
发明人： Rainer Mueller , Sven Uhlemann , Thomas Scherer , Heiko Luetjens
IPC分类号： B64C114
CPC分类号： B64C1/1492
摘要： A double pane window for an aircraft cabin has a passive air dehumidifying channel (5, 5A) that is in heat exchange contact with a window metal frame (1) which is in turn in heat exchange contact with the atmosphere outside the aircraft. The air dehumidifying channel (5, 5A) communicates through a first air flow port (6) with the cabin space and through a second air flow port (7) with a space enclosed between the double panes.
摘要翻译：用于飞机机舱的双窗格窗口具有与窗口金属框架（1）进行热交换接触的被动空气除湿通道（5,5A），所述窗金属框架（1）又与飞机外部的大气进行热交换接触。空气除湿通道（5,5A）通过第一气流端口（6）与客舱空间连通，并通过第二空气流通口（7）连通，空间包围在双层玻璃板之间。

2. 发明授权

US5884865A Non-fogging aircraft window arrangement 失效
标题翻译：不起雾的飞机窗口布置
公开(公告)号：US5884865A
公开(公告)日：1999-03-23
申请号：US984605
申请日：1997-12-03
申请人： Thomas Scherer , Rainer Mueller , Sven Uhlemann
发明人： Thomas Scherer , Rainer Mueller , Sven Uhlemann
IPC分类号： B64C1/14
CPC分类号： B64C1/1492
摘要： A double-pane aircraft cabin window arrangement avoids fogging, frosting, or icing of the window without using any active pressure regulating system or other active components. An inner pane and an outer pane are held in a window seal that is mounted in a frame connected to the aircraft fuselage. An interspace is formed between the two panes and sealed by the window seal. A condensation inducing tube is connected by a hose to an adapter tube, which passes through the window seal into the window interspace. The condensation inducing tube is connected in a direct thermally conducting manner to the outer fuselage skin of the aircraft. An open end of the condensation inducing tube is arranged to receive pressurized air from the aircraft cabin interior. As the air flows through the condensation inducing tube, any condensable moisture in the air condenses out on the interior walls of the tube, so that only dry air flows into the window interspace.
摘要翻译：双层飞机机舱窗口布置避免了窗户的雾化，结霜或结冰，而不使用任何主动调压系统或其他有源部件。内部窗格和外部窗格保持在安装在与飞机机身连接的框架中的窗口密封件中。在两个窗格之间形成一个间隙，并被窗户密封件密封。冷凝诱导管通过软管连接到适配器管，适配器管通过窗口密封件进入窗口间隙。冷凝诱导管以直接导热的方式连接到飞行器的机身外部皮肤。冷凝诱导管的开口端布置成从飞机机舱内部接收加压空气。当空气流过冷凝诱导管时，空气中的任何可冷凝水分在管的内壁上冷凝，使得只有干燥空气流入窗口间隙。

3. 发明授权

US08490365B2 Aircraft side fairing 有权
公开(公告)号：US08490365B2
公开(公告)日：2013-07-23
申请号：US12308926
申请日：2007-06-22
申请人： Rainer Mueller , Georg Muehlthaler
发明人： Rainer Mueller , Georg Muehlthaler
IPC分类号： E04C2/54
CPC分类号： B64C1/40 , B32B3/12 , B32B3/26 , B64C1/066 , F16L59/065 , Y02T50/46 , Y10T428/231
摘要： The invention relates to an aircraft side fairing, with a component (9) in the form of individual hollow chambers (12, 13, 14) which are arranged essentially in a preferably curved plane and are arranged between two cover layers (1, 2), wherein a gastight film which completely encases the component (9) with the hollow chambers (12, 13, 14) is provided and, after application of a vacuum to evacuate the hollow chambers (12, 13, 14), surrounds the component (9) with the hollow chambers in a gastight manner.

4. 外观设计

USD670636S1 Wheel or wheel cover 有权
公开(公告)号：USD670636S1
公开(公告)日：2012-11-13
申请号：US29417654
申请日：2012-04-06
申请人： Dirk Juergens , Rainer Mueller
设计人： Dirk Juergens , Rainer Mueller

5. 外观设计

USD655657S1 Wheel or wheel cover 有权
公开(公告)号：USD655657S1
公开(公告)日：2012-03-13
申请号：US29371355
申请日：2011-01-14
申请人： Dirk Juergens , Rainer Mueller
设计人： Dirk Juergens , Rainer Mueller

6. 发明申请

US20110256589A1 T7 RNA POLYMERASE VARIANTS WITH ENHANCED THERMOSTABILITY 有权
标题翻译：具有增强热稳定性的T7 RNA聚合酶变体
公开(公告)号：US20110256589A1
公开(公告)日：2011-10-20
申请号：US13069514
申请日：2011-03-23
申请人： Harald Sobek , Johann-Peter Thalhofer , Rainer Mueller , Manfred Schmidt , Michael Greif , Armin Ruf , Christian Rudolph
发明人： Harald Sobek , Johann-Peter Thalhofer , Rainer Mueller , Manfred Schmidt , Michael Greif , Armin Ruf , Christian Rudolph
IPC分类号： C12P19/34 , C12N5/10 , C12N15/63 , C12N9/10 , C07H21/00
CPC分类号： C12N9/1247 , C12P19/34 , C12Y207/07006
摘要： The present invention provides improved variants of T7 RNA polymerase by introducing novel mutations which lead to improved thermostability of the enzyme. According to the invention, amino acid substitutions at the positions Val426, Ser633, Val650, Thr654, Ala702, Val795, and combinations thereof are advantageous.
摘要翻译：本发明通过引入导致酶的热稳定性的新突变来提供T7RNA聚合酶的改进变体。根据本发明，位置Val426，Ser633，Val650，Thr654，Ala702，Val795及其组合的氨基酸取代是有利的。

7. 外观设计

USD625236S1 Wheel or wheel cover 有权
公开(公告)号：USD625236S1
公开(公告)日：2010-10-12
申请号：US29357596
申请日：2010-03-15
申请人： Gert Hildebrand , Henning Holstein , Dirk Juergens , Rainer Mueller
设计人： Gert Hildebrand , Henning Holstein , Dirk Juergens , Rainer Mueller

8. 外观设计

USD620872S1 Wheel or wheel cover 有权
公开(公告)号：USD620872S1
公开(公告)日：2010-08-03
申请号：US29347275
申请日：2009-11-19
申请人： Dirk Juergens , Rainer Mueller
设计人： Dirk Juergens , Rainer Mueller

9. 外观设计

USD612787S1 Wheel or wheel cover 有权
公开(公告)号：USD612787S1
公开(公告)日：2010-03-30
申请号：US29347010
申请日：2009-08-24
申请人： Dirk Juergens , Rainer Mueller
设计人： Dirk Juergens , Rainer Mueller

10. 发明申请

US20090304979A1 Aircraft side fairing 有权
标题翻译：飞机侧整流罩
公开(公告)号：US20090304979A1
公开(公告)日：2009-12-10
申请号：US12308926
申请日：2007-06-22
申请人： Rainer Mueller , Georg Muehlthaler
发明人： Rainer Mueller , Georg Muehlthaler
IPC分类号： B32B3/12 , B32B37/02
CPC分类号： B64C1/40 , B32B3/12 , B32B3/26 , B64C1/066 , F16L59/065 , Y02T50/46 , Y10T428/231
摘要： The invention relates to an aircraft side fairing, with a component (9) in the form of individual hollow chambers (12, 13, 14) which are arranged essentially in a preferably curved plane and are arranged between two cover layers (1, 2), wherein a gastight film which completely encases the component (9) with the hollow chambers (12, 13, 14) is provided and, after application of a vacuum to evacuate the hollow chambers (12, 13, 14), surrounds the component (9) with the hollow chambers in a gastight manner.
摘要翻译：本发明涉及一种飞机侧整流罩，其具有基本上位于优选弯曲平面中并且布置在两个覆盖层（1,2）之间的单个中空室（12,13,14）形式的部件（9）其特征在于，提供将所述部件（9）完全包住所述中空室（12,13,14）的气密膜，并且在施加真空以抽空所述中空室（12,13,14）之后，围绕所述部件 9）以气密的方式与中空室。

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