Fuel flow control valve and fuel control system incorporating same
    1.
    发明公开
    Fuel flow control valve and fuel control system incorporating same 失效
    燃料控制阀和系统。

    公开(公告)号:EP0222524A2

    公开(公告)日:1987-05-20

    申请号:EP86308103.0

    申请日:1986-10-20

    IPC分类号: F02C7/232 F02C9/36 F02C7/26

    CPC分类号: F02C9/36 F02C7/26 F02C9/263

    摘要: A fuel flow control valve (10) is adapted to control the flow of fuel in a spill line (52) to control the amount of fuel usable in a two speed gas turbine (56). The valve includes fluid pressure operated valve means (16) controlled by two variable volume fluid pressure chambers (32, 34) to provide appropriate fuel flow for 'run' and 'idle' conditions, and positioning means (18, 24, 64) to automatically position the fluid pressure operated valve means (16) when the control valve (10) is at rest to provide a flow of fuel appropriate for'start-up' of the gas turbine (56) that is greater than the flow required in the 'idle' condition but less than that required in the 'run' condition. Operating fluid pressures connected to the chambers (32, 34) may comprise either gaseous fluid pressures tapped from a stage of the compressor (58) of the gas turbine or a combination of said gaseous pressure source and a liquid fluid pressure source preferably comprising a fuel pressure supply tapped from the fuel supply line (51) to the gas turbine.

    Aircraft aircrew life support apparatus
    4.
    发明公开
    Aircraft aircrew life support apparatus 失效
    飞机机组生命支持设备

    公开(公告)号:EP0448258A1

    公开(公告)日:1991-09-25

    申请号:EP91301937.8

    申请日:1991-03-08

    IPC分类号: B64D10/00 A62B9/02

    CPC分类号: A62B9/022 B64D10/00

    摘要: A breathing demand regulator for use in aircrew life support apparatus has an aneroid capsule 56 coacting with a valve head 50 to restrict outflow from a breathing pressure control chamber 32. The aneroid capsule expands to move the valve head in the event of aircraft cabin altitude rising above a predetermined level due to loss of cabin pressure. An end face 53 of a valve stem 51 supporting the valve head senses inflation pressure of an aircrew G-suit by way of a passageway 59 for movement of the valve head in the presence of G-load. This arrangement provides for increased control pressure and, hence, increased breathing gas pressure in a regulator outlet 13, in meeting the higher of requirements for positive pressure breathing to protect an aircrew member exposed to both G-load and high aircraft ambient altitude (say above 12000 metres).
    The regulator is disclosed in combination with an anti-G valve arrangement 90, 100 and a G-suit inflation control valve arrangement 60, 61, and 120, 121 that provides the higher of G-suit inflation pressure requirement for protecting the aircrew member when exposed to high aircraft ambient altitude in the presence of G-load.

    摘要翻译: 用于机组生命支持装置的呼吸需求调节器具有与瓣膜头50共同作用的液体小室56,以限制从呼吸压力控制室32流出。在飞机机舱高度升高的情况下,小型液体容器膨胀以移动瓣膜头 由于机舱压力的丧失而高于预定水平。 支撑阀头的阀杆51的端面53通过通道59检测机组G-套装的充气压力,以在存在G-负载的情况下移动阀头。 这种布置提供了增加的控制压力,并且因此增加了调节器出口13中的呼吸气体压力,满足正压呼吸的要求中的较高要求,以保护机组构件暴露于G-载荷和高飞机环境高度(例如以上 12000米)。 该调节器与抗G阀装置90,100和G套装充气控制阀装置60,61和120,121相结合公开,G装置充气控制阀装置60,61和120,121在保护机组件成员 在G负载的情况下暴露于高飞机环境高度。

    Aircraft undercarriage door latching assembly
    5.
    发明公开
    Aircraft undercarriage door latching assembly 有权
    锁定安排的飞机起落架的门

    公开(公告)号:EP0934874A3

    公开(公告)日:1999-10-27

    申请号:EP99102097.5

    申请日:1999-02-02

    IPC分类号: B64C25/26

    摘要: An assembly (10) for retaining a catch member (11) in a first condition and for releasing the catch member (11) for movement to a second condition, comprises a latch member (12) pivotable about a first pivotal axis (B) and having a formation (14) adapted to co-operate with the catch member (11) to retain the catch member (11) when the latch member (12) is in a latched position, and a rocker member (16) pivotable about a second pivotal axis (A), the latch member (12) and the rocker member (16) interacting to retain the latch member (12) in its latched position, the assembly (10) further comprising actuating means (25) to move the rocker member (16) about the second pivotal axis (A) to allow the latch member (12) to be pivoted about the first pivotal axis (B) to an unlatched position to release the catch member (11) characterised in that the latch member (12) and the rocker member (16) are interconnected by a resilient biasing means (18), the resilient biasing means (18) including first (26) and second (27) relatively movable parts with a spring (28) acting between them and there being a stop means (30, 31) which locks the first and second relatively movable parts (26, 27) upon a movement of the rocker member (16) about the second pivotal axis (A) beyond a threshold position.

    Aircraft undercarriage door latching assembly
    7.
    发明公开
    Aircraft undercarriage door latching assembly 有权
    飞机底盘门闩锁组件

    公开(公告)号:EP0934874A2

    公开(公告)日:1999-08-11

    申请号:EP99102097.5

    申请日:1999-02-02

    IPC分类号: B64C25/26

    摘要: An assembly (10) for retaining a catch member (11) in a first condition and for releasing the catch member (11) for movement to a second condition, comprises a latch member (12) pivotable about a first pivotal axis (B) and having a formation (14) adapted to co-operate with the catch member (11) to retain the catch member (11) when the latch member (12) is in a latched position, and a rocker member (16) pivotable about a second pivotal axis (A), the latch member (12) and the rocker member (16) interacting to retain the latch member (12) in its latched position, the assembly (10) further comprising actuating means (25) to move the rocker member (16) about the second pivotal axis (A) to allow the latch member (12) to be pivoted about the first pivotal axis (B) to an unlatched position to release the catch member (11) characterised in that the latch member (12) and the rocker member (16) are interconnected by a resilient biasing means (18), the resilient biasing means (18) including first (26) and second (27) relatively movable parts with a spring (28) acting between them and there being a stop means (30, 31) which locks the first and second relatively movable parts (26, 27) upon a movement of the rocker member (16) about the second pivotal axis (A) beyond a threshold position.

    摘要翻译: 一种用于在第一状态下保持锁扣件(11)并且用于释放锁扣件(11)以便移动到第二状态的组件(10)包括一个可围绕第一枢轴线(B)枢转的闩锁件(12)和 具有适于与锁扣构件(11)配合以在锁扣构件(12)处于锁扣位置时保持锁扣构件(11)的构造(14),以及可围绕第二锁定构件 (12)和闩锁构件(12)相互作用以将闩锁构件(12)保持在其闩锁位置中,组件(10)还包括致动装置(25)以使摇摆构件 (12)围绕所述第二枢转轴线(A)绕所述第一枢转轴线(B)枢转到解锁位置以释放所述锁扣构件(11),其特征在于,所述锁扣构件(12) )和摇杆构件(16)通过弹性偏置装置(18)相互连接,弹性偏置装置(18)包括第一 (26)和第二可相对运动部件(27),其中弹簧(28)作用在它们之间并且具有止动装置(30,31),所述止动装置在所述第一和第二相对可运动部件(26,27) 围绕第二枢转轴线(A)的摇摆构件(16)超出阈值位置。