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    • 12. 发明公开
    • On-board inert gas generation system
    • 车载惰性气体发生系统
    • EP1669290A1
    • 2006-06-14
    • EP05257507.3
    • 2005-12-05
    • Hamilton Sundstrand Corporation
    • Schwalm, Gregory
    • B64D37/32
    • B64D37/32B64D2013/0677Y02T50/44
    • An on-board inert gas generation system (10) provides first and second compressors (28, 36) in fluid communication with one another. The second compressor (36) includes an inlet and an outlet. The inlet is in fluid communication with the first compressor (28). The second compressor (36) is the final compressor stage of the system. An air separation module (40) is fluidly connected to the outlet of the second compressor (36) by a passageway (37). A vent passage (46) is arranged between the outlet and the air separation module (40) for venting fluid between the outlet and air separation module (40). The vent passage (46) enables the flow from the second compressor (36) to be increased thereby increasing compressor efficiency and increasing the inlet pressure to the air separation module (40), which enables use of a smaller air separation module.
    • 机载惰性气体发生系统(10)提供彼此流体连通的第一和第二压缩机(28,36)。 第二压缩机(36)包括入口和出口。 入口与第一压缩机(28)流体连通。 第二压缩机(36)是系统的最终压缩机级。 空气分离模块(40)通过通道(37)流体连接到第二压缩机(36)的出口。 在出口与空气分离模块(40)之间布置有排气通道(46),用于排放出口与空气分离模块(40)之间的流体。 排气通道46能够增加来自第二压缩机36的流量,由此增加压缩机效率并增加空气分离模块40的入口压力,这使得能够使用较小的空气分离模块。
    • 15. 发明公开
    • Low power nitrogen enriched air generation system
    • Energieeffiziente Versorgungseinrichtungfürstickstoffangereicherte Luft
    • EP1433704A1
    • 2004-06-30
    • EP03257942.7
    • 2003-12-17
    • Hamilton Sundstrand Corporation
    • Defrancesco, GregoryZywiak, ThomasHipsky, Harold W.
    • B64D37/32
    • A62B7/14B64D37/32B64D2013/0677Y02T50/44
    • An inerting system (10) provides air with reduced oxygen content by flowing and directing air through an air separation module (48). Optimal working pressure for the air separation module is obtained with two compressors. A first compressor (16) elevates air from the aircraft cabin (12) to a second pressure. The second pressure is at an intermediate level below the working pressure of the air separation module (48). A second compressor (30) elevates air from the second pressure to the working pressure. The second compressor (30) is driven by oxygen depleted air exhausted through a turbine (52). The pressure difference between air at the working pressure and air required by the fuel distribution system (54) is used to power the turbine (52) and drive the second compressor (30).
    • 惰化系统(10)通过流过并引导空气通过空气分离模块(48)来为空气提供降低的氧含量。 使用两台压缩机获得空气分离模块的最佳工作压力。 第一压缩机(16)将空气从飞机机舱(12)升高到第二压力。 第二压力处于低于空气分离模块(48)的工作压力的中间水平。 第二压缩机(30)将空气从第二压力升高到工作压力。 第二压缩机(30)由通过涡轮(52)排出的贫氧空气驱动。 使用燃料分配系统(54)所需的工作压力和空气之间的空气压力差来驱动涡轮机(52)并驱动第二压缩机(30)。
    • 16. 发明公开
    • Aircraft air conditioner
    • 飞机空调
    • EP1273515A3
    • 2004-05-12
    • EP02014467.1
    • 2002-06-28
    • Shimadzu Corporation
    • Mitani, HisashiSaito, Hidefumi
    • B64D13/06B64D13/08B01D53/04B01D53/26B64D37/32
    • B64D37/32B64D13/06B64D2013/0677B64D2013/0688Y02T50/44Y02T50/56
    • In an air conditioner, air extracted from engine (1) is fed through a main air flow path (90) into cabin (8) after being cooled by a cooling device. This extracted air is fed into the cabin (8) through an auxiliary air flow path (11, 92). The air within the cabin (8) flows out through an outflow air flow path (40). A plurality of adsorption sections (23, 24, 83) are constituted by an adsorption agent that adsorbs molecules contained in the air and releases adsorbed molecules by being raised in temperature to more than the temperature thereof on adsorption. By control of an air flow changeover mechanism (50) by a controller (25), each of the adsorption sections (23, 24, 83) is changed over between a condition connected with the auxiliary air flow path (11, 92) and a condition connected with the outflow air flow path (40).
    • 在空气调节器中,从发动机(1)抽取的空气在被冷却装置冷却之后通过主空气流动路径(90)供给到车厢(8)中。 该抽出的空气通过辅助空气流路(11,92)被供给到车室(8)内。 车厢(8)内的空气通过流出气流路径(40)流出。 多个吸附部(23,24,83)由吸附空气中所含分子的吸附剂构成,通过升温至比吸附温度高的温度来释放吸附分子。 通过由控制器(25)控制气流切换机构(50),各吸附部(23,24,83)在与辅助空气流路(11,92)连接的状态和 条件与流出气流路径(40)连接。
    • 17. 发明公开
    • A FUEL INERTING SYSTEM
    • 燃油加油系统
    • EP1250259A1
    • 2002-10-23
    • EP01901286.3
    • 2001-01-23
    • BAE SYSTEMS plc
    • PICOT, ChristineWARD, Michael, David
    • B64D37/32B01D19/00
    • B01D19/0005B64D37/32B64D2013/0677
    • A fuel inerting system, comprising a first supply means (2) to supply an inert gas to a fuel tank (8) to scrub the fuel therein when the ullage (16) of the fuel tank is inert, and a second supply means (4) to supply the inert gas to scrub the fuel (6) therein when the ullage of the fuel tank is not inert, the first and second supply means (2, 4) being individually operable by means of a valve arrangement (10), in such a manner that only one of the supply means is operable at any given time. The inert gas consist of nitrogen enriched air, produced by passing air from a pressurised area of the aircraft through a nitrogen separator located within, but removable from, the aircraft.
    • 一种燃料惰化系统,包括:第一供应装置(2),当燃料箱的空载(16)为惰性时,向燃料箱(8)供应惰性气体以擦洗其中的燃料;以及第二供应装置(4 ),当燃料箱的空间不是惰性时,第一和第二供应装置(2,4)通过阀装置(10)单独操作,以供应惰性气体以擦洗其中的燃料(6) 使得在任何给定时间只有一个供应装置可操作。 惰性气体由富氮空气构成,富氮空气是通过将来自飞机加压区域的空气通过位于飞机内但可从飞机上移除的氮气分离器产生的。