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公开(公告)号：US5295999A
公开(公告)日：1994-03-22
申请号：US6590
申请日：1993-01-21
申请人： Rolf Hinrichs , Peter Wild
发明人： Rolf Hinrichs , Peter Wild
CPC分类号： C09B67/0051 , D21H21/28
摘要： The dyestuff mixtures comprising the dyestuff of the formula (I) ##STR1## and a dyestuff of the formula ##STR2## wherein R.sub.1 and R.sub.2 independently of one another represent alkyl, cycloalkyl or aryl,and/or tautomeric forms of the dyestuffs of the formulae (I) and/or (II), are particularly suitable for the preparation of concentrated, storage-stable dyestuff solutions which, apart from a small amount of alkanolamines, comprise no further water-soluble organic solubilising agents.
摘要翻译： 包含式（I）染料的染料混合物和式（II）的染料，其中R 1和R 2彼此独立地表示烷基，环烷基或芳基，和/或互变异构体 的式（I）和/或（II）的染料特别适用于制备浓缩的储存稳定的染料溶液，除了少量的链烷醇胺之外，还不包含另外的水溶性有机增溶剂。
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公开(公告)号：US5233027A
公开(公告)日：1993-08-03
申请号：US704747
申请日：1991-05-23
申请人： Rolf Hinrichs , Klaus Kunde
发明人： Rolf Hinrichs , Klaus Kunde
摘要： The new disazo dyestuffs of the formula (I) ##STR1## in which the substituents and indices have the meaning given in the description, and salts thereof are outstandingly suitable for dyeing cellulose-containing materials and leather in blue shades having good wet- and light-fastnesses.
摘要翻译： 其中取代基和指数具有说明书中给出的含义的式（I）的新的二重氮染料及其盐显着适用于以蓝色色调染色含纤维素的材料和皮革 具有良好的耐湿和耐光性。
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公开(公告)号：US20090260449A1
公开(公告)日：2009-10-22
申请号：US12427099
申请日：2009-04-21
IPC分类号： G01M5/00
CPC分类号： G01M5/0075 , G01M5/0041
摘要： The present invention provides a device for test loading a fuselage barrel, in particular in the aviation and aerospace industry. The device comprises a first and a second pressure bulkhead for sealing the fuselage barrel at the end faces thereof in a pressure-tight manner. The device further comprises a support device which may be coupled to the first pressure bulkhead, on the one hand, and to the second pressure bulkhead, on the other hand, extending through the fuselage barrel. Moreover, the device comprises a loading device which may be coupled to the support device, on the one hand, and to a portion of the fuselage barrel, on the other hand, for introducing loads into the fuselage barrel. The resulting advantage is that gravitational force and/or acceleration forces acting on the masses arranged in the fuselage barrel, for example cargo, in particular during the flight phase may be simulated by means of components which are exclusively arranged within the fuselage barrel, which is pressurised during the test. Thus a provision of through-holes in the fuselage skin for passing through hydraulic cylinders and the sealing of said holes relative to the fuselage skin, as in the device known to the applicant, are avoided.
摘要翻译： 本发明提供了一种用于特别在航空航天工业中对机身筒进行试验加载的装置。 该装置包括第一和第二压力舱壁，用于在其端面处以密封的方式密封机身筒体。 该装置还包括支撑装置，另一方面，支撑装置可以连接到第一压力舱壁，另一方面延伸穿过机身筒。 此外，该装置还包括一个装载装置，一方面可以耦合到支撑装置，另一方面则耦合到机身筒体的一部分，用于将负载引入机身筒体。 所产生的优点是，可以通过专门设置在机身筒内的部件来模拟作用在设置在机身筒体（例如货物）中的质量的重力和/或加速力，特别是在飞行阶段期间的重力和/或加速力， 在测试期间加压。 因此，如本申请人已知的装置那样，避免了在机身皮肤中提供穿过液压缸的通孔和相对于机身皮肤密封所述孔。
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公开(公告)号：US08024981B2
公开(公告)日：2011-09-27
申请号：US12427099
申请日：2009-04-21
IPC分类号： G01M5/00
CPC分类号： G01M5/0075 , G01M5/0041
摘要： The present invention provides a device for test loading a fuselage barrel, in particular in the aviation and aerospace industry. The device comprises a first and a second pressure bulkhead for sealing the fuselage barrel at the end faces thereof in a pressure-tight manner. The device further comprises a support device which may be coupled to the first pressure bulkhead, on the one hand, and to the second pressure bulkhead, on the other hand, extending through the fuselage barrel. Moreover, the device comprises a loading device which may be coupled to the support device, on the one hand, and to a portion of the fuselage barrel, on the other hand, for introducing loads into the fuselage barrel. The resulting advantage is that gravitational force and/or acceleration forces acting on the masses arranged in the fuselage barrel, for example cargo, in particular during the flight phase may be simulated by means of components which are exclusively arranged within the fuselage barrel, which is pressurized during the test. Thus a provision of through-holes in the fuselage skin for passing through hydraulic cylinders and the sealing of said holes relative to the fuselage skin, as in the device known to the applicant, are avoided.
摘要翻译： 本发明提供了一种用于特别在航空航天工业中对机身筒进行试验加载的装置。 该装置包括第一和第二压力舱壁，用于在其端面处以密封的方式密封机身筒体。 该装置还包括支撑装置，另一方面，支撑装置可以连接到第一压力舱壁，另一方面延伸穿过机身筒。 此外，该装置还包括一个装载装置，一方面可以耦合到支撑装置，另一方面则耦合到机身筒体的一部分，用于将负载引入机身筒体。 所产生的优点是，可以通过专门设置在机身筒内的部件来模拟作用在设置在机身筒体（例如货物）中的质量的重力和/或加速力，特别是在飞行阶段期间的重力和/或加速力， 在测试期间加压。 因此，如本申请人已知的装置那样，避免了在机身皮肤中提供穿过液压缸的通孔和相对于机身皮肤密封所述孔。
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公开(公告)号：US08833700B2
公开(公告)日：2014-09-16
申请号：US13652069
申请日：2012-10-15
申请人： Andrej Klaas , Michael Stohl , Rolf Hinrichs
发明人： Andrej Klaas , Michael Stohl , Rolf Hinrichs
IPC分类号： B64C1/14
CPC分类号： B64C1/1407
摘要： The present invention provides a cover plate for covering at least portions of a door gap formed between a door covering and a fuselage cell of an aircraft or spacecraft, comprising: a fastening portion by which the cover plate can be mounted on an outer surface of the door covering; a contact portion which rests in a contacting manner against an outer skin of the fuselage cell when the door covering is closed; at least one corner portion associated with a corner of the door covering; and a side portion associated with a side of the door covering, the at least one corner portion and the side portion being configured to press the contact portion with a constant contact pressure against the outer skin of the fuselage cell when the door covering is closed. The present invention further provides a door covering for an access opening in a fuselage cell of an aircraft or spacecraft having a cover plate of this type as well as an aircraft or spacecraft having a cover plate of this type and/or having a door covering of this type.
摘要翻译： 本发明提供了一种用于覆盖形成在飞机或航天器的门罩和机身单元之间的门间隙的至少一部分的盖板，包括：紧固部分，盖板可以通过该紧固部分安装在 门盖; 接触部分，当所述门盖关闭时，所述接触部分以接触方式抵靠所述机身单元的外皮; 与所述门罩的角部相关联的至少一个角部; 以及与所述门罩的侧面相关联的侧部，所述至少一个拐角部分和所述侧部构造成当所述门盖关闭时，使接触部分以一定的接触压力抵靠在机身单元的外皮上。 本发明还提供了一种用于具有这种盖板的飞机或航天器的机身单元中的进入开口的门盖以及具有这种类型的盖板的飞机或航天器和/或具有这种盖板的门盖 这个类型。
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