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    • 4. 发明公开
    • MODULAR CANISTER MODULES FOR AIR SEPARATION SYSTEMS
    • MODULARE KANISTERMODULEFÜRLUFTTRENNUNGSSYSTEME
    • EP3040279A1
    • 2016-07-06
    • EP15203241.3
    • 2015-12-31
    • Hamilton Sundstrand Corporation
    • PEACOS III, FrederickCRAWFORD, Kenneth
    • B64D37/32B01D63/02
    • B64D37/32B01D2053/221B01D2256/12B01D2257/102B01D2257/106B01D2258/06B01D2259/4575B64D13/06B64D37/005B64D2013/0651B64D2013/0677B64D2013/0681
    • An air separation system is provided that includes at least one air separation module (202a, 202b, 202c) having a first end (206) and a second end (210) and at least one mounting assembly (204, 208) removably connected the at least one air separation module (202a, 202b, 202c) and configured to mount the at least one air separation module (202a, 202b, 202c) in an aircraft. The at least one mounting assembly (204, 208) includes a first end cap (212a, 212b, 212c) removably connected to the first end (206) of the at least one air separation module (202a, 202b, 202c), a second end cap removably connected to the second end (208) of the at least one air separation module (202a, 202b, 202c), and at least one bracket (218) configured to removably connect one of the first end cap and the second end cap (212a, 212b, 212c) to an aircraft.
    • 提供了一种空气分离系统,其包括具有第一端(206)和第二端(210)的至少一个空气分离模块(202a,202b,202c)和至少一个安装组件(204,208),其可移除地连接在 至少一个空气分离模块(202a,202b,202c)并被配置成将至少一个空气分离模块(202a,202b,202c)安装在飞行器中。 所述至少一个安装组件(204,208)包括可移除地连接到所述至少一个空气分离模块(202a,202b,202c)的第一端(206)的第一端盖(212a,212b,212c) 可拆卸地连接到所述至少一个空气分离模块(202a,202b,202c)的第二端(208)的端盖,以及至少一个支架(218),其构造成可移除地连接所述第一端盖和所述第二端盖 (212a,212b,212c)到飞行器。
    • 8. 发明公开
    • Oxygen breathing device for an aircraft
    • Sauerstoffatemgerätfürein Flugzeug
    • EP2143636A1
    • 2010-01-13
    • EP08012585.9
    • 2008-07-11
    • Intertechnique SA
    • Ritttner, WolfgangMeckes, RüdigerNiedostatek, Mark
    • B64D10/00A62B7/14
    • B64D10/00A62B7/02A62B7/10A62B7/14B64D2013/0677
    • The invention relates to an oxygen breathing device for an aircraft, in particular for oxygen supply to crew member in a cockpit of an aircraft, comprising a filter unit (9) having an inflow port and an outflow port, the filter unit (9) being adapted to extract nitrogen from an air flow flowing from the inflow port to the outflow port through the filter unit (9), wherein the filter unit (9) is adapted to receive compressed air, preferably, bleed air from a precompressor stage of a turbine driving the aircraft, or directly by a separate electrically driven compressor, via a bleed air supply line (3) connected to the inflow port, a first pressure regulator (5) in the bleed air supply line (3), a first water separator (1a) which is arranged in the bleed air supply line (3) in flow direction of the bleed air before the first pressure regulator (5) and a connection port which can be brought in fluid communication with said outflow port of the filter unit (9) and which is adapted to be coupled to at least one oxygen supply mask (13) via an oxygen supply line (21). According to the invention, a chemical oxygen generator (18) comprising at least one substance adapted to produce oxygen in a chemical reaction and to provide said oxygen to an outflow port of said oxygen generator (18) is provided. The outflow port of said chemical oxygen generator (18) is connected to an auxiliary oxygen supply line (23) and a control unit (16) is adapted to selectively provide oxygen from the filter unit (9) or the chemical oxygen generator (18) to an oxygen supply mask (13) coupled to the connection port.
    • 本发明涉及一种用于飞行器的氧气呼吸装置,特别是用于飞机驾驶舱中的乘员的氧气供应,其包括具有入口和流出口的过滤器单元(9),所述过滤单元(9) 适于从通过过滤器单元(9)从流入口流到流出口的空气流中提取氮气,其中过滤器单元(9)适于接收压缩空气,优选地从涡轮机的预压缩器级排出空气 通过连接到流入口的排气供应管线(3)直接驱动飞机,或直接由单独的电动压缩机驱动,排气供应管线(3)中的第一压力调节器(5),第一水分离器 1a),其在第一压力调节器(5)之前在排气的流动方向上布置在排气供应管线(3)中,并且连接端口可以与过滤器单元(9)的所述流出端口流体连通 ),并且适合于联动 经由供氧管线(21)经由至少一个氧气供给掩模(13)。 根据本发明,提供一种化学氧气发生器(18),其包括适于在化学反应中产生氧并将氧气提供给所述氧气发生器(18)的流出口的至少一种物质。 所述化学氧气发生器(18)的流出口连接到辅助氧气供应管线(23),并且控制单元(16)适于从过滤器单元(9)或化学氧气发生器(18)选择性地提供氧气, 耦合到连接端口的氧供应掩模(13)。