公开(公告)号：US20030136879A1

公开(公告)日：2003-07-24

申请号：US10282333

申请日：2002-10-28

发明人： Thomas Grabow ,  Alexander Scheidt ,  Konstantin Kallergis

IPC分类号： B64D045/00

CPC分类号： A62C99/0009 ,  A62C3/08 ,  A62C99/0018

摘要： A system for extinguishing and suppressing a fire in an enclosed space includes a Halon storage container and a nitrogen generator that are both connected by a duct system to extinguishing nozzles arranged in the enclosed space. Halon is supplied as a first extinguishing agent from the container to achieve a rapid initial extinguishing of the fire. Nitrogen enriched air is supplied as a second extinguishing agent from the nitrogen generator to achieve a continuous long-term fire suppression, commencing simultaneously with or after the introduction of the Halon. The nitrogen generator may include a molecular sieve to continuously generate the nitrogen enriched air from an inlet flow of environmental air.

摘要翻译： 用于灭火和灭火的封闭空间的火灾系统包括哈龙存储容器和氮气发生器，它们都通过管道系统连接到设置在封闭空间中的灭火喷嘴。 哈龙作为第一个灭火剂从容器中提供，以实现火灾的快速初始灭火。 富氮空气作为第二种灭火剂从氮气发生器中提供，以实现连续的长期灭火，其与哈龙引入同时或之后开始。 氮气发生器可以包括从环境空气的入口流中连续产生富氮空气的分子筛。

公开(公告)号：US20020125372A1

公开(公告)日：2002-09-12

申请号：US09793551

申请日：2001-02-27

发明人： Henry Shooflar

IPC分类号： B64D045/00 ,  A62C003/07

CPC分类号： A62C3/08

摘要： A mechanically operable actuating device for opening a circular entry in the fuselage wall of an Aircraft. This device moves a plug attached to the shaft of a pneumatic piston inwards to expose an opening which allows smoke from a fire in any area of the plane to be expelled outside through a network of flexible tubing and computer directed shut off valves and nozzles that route the smoke outside by the nearest mechanism automatically. The smoke expulsion is achieved by the huge pressure differentially inside the plane and the outside forcing the mixture of smoke and pressurized air outside. When a plane on fire lands at an Airport the Firefighters attach hoses with an interlocking Storz receiving adapter that permits interior water spraying on the burning passengers by the same tubing network. The Flight Deck Computer controls all operations but the Pilot may alter any move. A back up Computer is located in the cabin.

摘要翻译： 一种用于打开飞机的机身壁中的圆形入口的机械操作的致动装置。 该装置将附接到气动活塞的轴的塞子向内移动以露出开口，该开口允许通过柔性管道和计算机定向的截止阀和喷嘴的路线将在平面的任何区域的火焰中的烟气排出到外部 烟雾外面由最近的机构自动。 烟雾排出是由平面内部巨大的压力差异引起的，而外面的烟雾和加压空气混合在一起。 当一架飞机着陆在机场时，消防队员用一个互锁的Storz接收适配器连接软管，允许通过同一管道网络对燃烧的乘客进行内部喷水。 飞行计算机控制所有操作，但飞行员可能会改变任何动作。 备用电脑位于机舱内。

公开(公告)号：US20030010867A1

公开(公告)日：2003-01-16

申请号：US10180484

申请日：2002-06-27

申请人： Eurocopter Deutschland GmbH

发明人： Klaus Wojatschek ,  Mark Drewe

IPC分类号： B64D045/00

CPC分类号： B64C1/1492

摘要： A connecting device for joining a windshield with a fuselage side frame of a viewing port of an aircraft, especially a cockpit frame of a helicopter. The connecting device includes a fastening element which is fixed into position on a section of a peripheral region of the windshield through a bore hole and into a congruent bore hole of the fuselage side frame and in a fastening part with a spring device. A peripheral slit filled with a sealant is arranged in a peripheral region between the fuselage side frame and windshield. The fastening part includes a retaining nut and a spring device which can be moved and guided within a seating element and connected with the fuselage side frame. The spring device is arranged between the retaining nut and the frame.

摘要翻译： 一种用于将挡风玻璃与飞机的观察端口的机身侧框架连接的连接装置，特别是直升机的驾驶舱框架。 连接装置包括紧固元件，该紧固元件通过孔眼固定在挡风玻璃的周边区域的一部分上并进入机身侧框架的一体钻孔中以及具有弹簧装置的紧固部件中。 填充有密封剂的周边狭缝布置在机身侧框架和挡风玻璃之间的周边区域中。 紧固部件包括固定螺母和弹簧装置，该弹簧装置可在座位元件内移动和引导并与机身侧框架连接。 弹簧装置设置在固定螺母和框架之间。

公开(公告)号：US20030144769A1

公开(公告)日：2003-07-31

申请号：US10298477

申请日：2002-11-14

发明人： Dieter Meier

IPC分类号： B64D045/00

CPC分类号： B64D45/0015 ,  B64D45/0031 ,  G05D1/0061

摘要： A security system for preventing the hijacking of aircraft, which are provided with an autopilot with stored flight routes, wherein an emergency switch-over device for actuating the autopilot, when actuated, prevents the autopilot being switched off again in the cockpit.

摘要翻译： 一种用于防止劫持飞行器的安全系统，其中设置有具有存储的飞行路线的自动驾驶仪，其中用于致动自动驾驶仪的紧急切换装置在被致动时防止在驾驶舱中再次关闭自动驾驶仪。

公开(公告)号：US20020158167A1

公开(公告)日：2002-10-31

申请号：US10128297

申请日：2002-04-24

发明人： Nicolas Schmutz ,  Olivier Vandroux

IPC分类号： B64D045/00

CPC分类号： A62C99/0018 ,  A62C3/06 ,  A62C3/08 ,  B64D37/32 ,  Y02T50/44

摘要： There is produced (at 2) air enriched in inert gas, from a source (9) of compressed air internal to the aircraft, and this enriched air is admitted (via 10) into the fuel tank (12). During the cruising phase of the aircraft, there is produced a first fraction of air having a first inert gas content, and this first fraction is admitted into the fuel tank (12) at a first flow rate. Moreover, during the descent phase, there is produced a second fraction of enriched air having a second inert gas content substantially less than the first content, and the second fraction is admitted to the reservoir (12) at a second flow rate substantially greater than the first flow rate.

摘要翻译： 从空气内部产生（2）富含惰性气体的空气，这种富集的空气通过10进入燃料箱（12）。 在飞行器的巡航阶段期间，产生具有第一惰性气体含量的第一部分空气，并且该第一部分以第一流速进入燃料箱（12）。 此外，在下降阶段期间，产生富含空气的第二部分，其具有基本上小于第一含量的第二惰性气体含量，并且第二馏分以基本上大于第一含量的第二流量允许进入储存器（12） 第一流量。