SHUT-OFF VALVE
    1.
    发明公开
    SHUT-OFF VALVE 审中-公开

    公开(公告)号:EP4194719A1

    公开(公告)日:2023-06-14

    申请号:EP21213197.3

    申请日:2021-12-08

    IPC分类号: F16H61/4069

    摘要: A valve (200) for controlling the flow of hydraulic fluid to a hydraulic motor (214) is disclosed. The valve (200) includes a sleeve (209) and a spool (212). The sleeve (209) includes a first fluid flow port (201) for receiving hydraulic fluid from the supply line (223); a second fluid flow port (202) for supplying hydraulic fluid to a second valve (213); a third fluid flow port (203) for receiving hydraulic fluid from a first control line (220a); a fourth fluid flow port (204) for receiving hydraulic fluid from a second control line (220b); and a fifth fluid flow port (205) in fluid communication with the return line (224). The valve (200) is arranged to be actuated to move the spool (212) between a first position and a second position. When the spool (212) is in the second position, the fifth fluid flow port (205) is in fluid communication with the second, third and fourth fluid flow ports (202, 203, 204) and the first fluid flow port (201) is closed by the spool (212).

    PRESSURE RELIEF VALVE
    2.
    发明公开

    公开(公告)号:EP3745011A1

    公开(公告)日:2020-12-02

    申请号:EP19191539.6

    申请日:2019-08-13

    IPC分类号: F16K31/365 G05D16/06

    摘要: A pressure relief valve (200) comprising:
    a first port (210) configured to receive a first gas at an input pressure;
    a second port (212) configured to receive a second gas at a regulating pressure;
    a third (214) port in fluid communication with the first port via an orifice (220) and configured to output the first gas at an output pressure;
    a diaphragm (230) configured to flex in a direction along an axis (A) and configured to control the passage of the first gas through the orifice between the first port and the third port, such that the output pressure of the gas is dependent on the flex of the diaphragm; and
    a resilient member (240) configured to bias the diaphragm,
    wherein the valve comprises a chamber (280) at least partly defined by the diaphragm and in fluid communication with the second port, such that the force exerted by the second gas within the chamber on the diaphragm acts against the action of the resilient member.

    HYDRAULIC NO-BACK DEVICE
    3.
    发明公开

    公开(公告)号:EP3505775A1

    公开(公告)日:2019-07-03

    申请号:EP17211099.1

    申请日:2017-12-29

    摘要: A hydraulic no-back device is described herein. In particular, a system (10) for moving a hydraulic actuator (12) is described herein that uses the new type of hydraulic no-back device. In some examples, the system comprises: a hydraulic power module (14) for pumping hydraulic fluid through the system (10) to the actuator (12), a reservoir (16) for receiving said fluid back from said system and said actuator (12), first and second check valves (20a, 20b); a conduit or conduits for fluidly connecting said power module (14) to said check valves (20a, 20b) and said reservoir (16); and wherein said conduit or conduits are connected so as to allow said hydraulic fluid to flow from the hydraulic power module (14) to said first check valve (20a), and from said first check valve (20b) into said hydraulic actuator (12), and from said hydraulic actuator (12) to said second check valve (20b) and from said second check valve (20b) to said reservoir (16).

    STABILITY CONTROL AUGMENTATION SYSTEM AND METHOD

    公开(公告)号:EP4371874A3

    公开(公告)日:2024-07-31

    申请号:EP24163360.1

    申请日:2021-09-27

    IPC分类号: B64C13/40

    CPC分类号: B64C13/40

    摘要: A stability control augmentation system and method for a flight control surface of an aircraft. The system comprises an actuator 200 operable for actuating the flight control surface, and a control valve 100 comprising a spool 140 and an integrated augmentation mechanism 130, 150. The spool 140 and the actuation mechanism 130, 150 are both moveable to open and close a fluid flow path through the control valve 100 to control the actuator 200.

    STABILITY CONTROL AUGMENTATION SYSTEM AND METHOD

    公开(公告)号:EP4371874A2

    公开(公告)日:2024-05-22

    申请号:EP24163360.1

    申请日:2021-09-27

    IPC分类号: B64C13/40

    CPC分类号: B64C13/40

    摘要: A stability control augmentation system and method for a flight control surface of an aircraft. The system comprises an actuator 200 operable for actuating the flight control surface, and a control valve 100 comprising a spool 140 and an integrated augmentation mechanism 130, 150. The spool 140 and the actuation mechanism 130, 150 are both moveable to open and close a fluid flow path through the control valve 100 to control the actuator 200.

    STABILITY AND CONTROL AUGMENTATION SYSTEM
    6.
    发明公开

    公开(公告)号:EP4194334A1

    公开(公告)日:2023-06-14

    申请号:EP21213218.7

    申请日:2021-12-08

    摘要: A Stability and Control Augmentation System ("SCAS") module includes a SCAS actuator (610). The SCAS actuator (610) has a substantially cylindrical hydraulic chamber having a first and second regions (620, 625). A piston (630) is arranged for linear motion in first and second directions along an axis of the hydraulic chamber. The SCAS module (600) also includes a valve system (635) for controlling a flow of a hydraulic fluid into the hydraulic chamber. The valve system (635) has: at least one supply line (672) arranged to provide a first fluid flow path to the first region (620) of the hydraulic chamber and/or a second fluid flow path to the second region (625) of the hydraulic chamber, and a moveable valve member (660) arranged to have a position between a first and second positions.

    STABILITY CONTROL AUGMENTATION SYSTEM AND METHOD

    公开(公告)号:EP4155196A1

    公开(公告)日:2023-03-29

    申请号:EP21199251.6

    申请日:2021-09-27

    IPC分类号: B64C13/40

    摘要: A stability control augmentation system and method for a flight control surface of an aircraft. The system comprises an actuator 200 operable for actuating the flight control surface, and a control valve 100 comprising a spool 140 and an integrated augmentation mechanism 130, 150. The spool 140 and the actuation mechanism 130, 150 are both moveable to open and close a fluid flow path through the control valve 100 to control the actuator 200.

    VALVE ASSEMBLY
    8.
    发明公开
    VALVE ASSEMBLY 审中-公开

    公开(公告)号:EP4067711A1

    公开(公告)日:2022-10-05

    申请号:EP21166019.6

    申请日:2021-03-30

    摘要: A valve assembly 100 for an anti-ice system of an aircraft. The valve assembly 100 comprises: a valve body 110; a first piston 120; and a regulating piston 140. The valve body 110 defines a valve inlet 112, a valve outlet 114, a fluid passage between the valve inlet 112 and the valve outlet 114, and a core portion 116 defining a first chamber 112 by cooperation with the first piston 120 and a regulating chamber 142 by cooperation with the regulating piston 140. The first piston 120 is moveable between a first position and a second position, and the regulating piston 140 is movable between a first position and a second position. The first piston 120 overlaps the regulating piston 140 when the first piston 120 is its first position and the regulating piston 140 is in its second position.

    PRESSURE RELIEF VALVE
    9.
    发明公开

    公开(公告)号:EP3745007A1

    公开(公告)日:2020-12-02

    申请号:EP19177394.4

    申请日:2019-05-29

    摘要: A pressure relief valve comprising:
    a first port configured to receive a first gas at an input pressure;
    a second port configured to receive a second gas at a regulating pressure;
    a third port in fluid communication with the first port via an orifice and configured to output the first gas at an output pressure;
    a piston movable along an axis and configured to control the passage of the first gas through the orifice between the first port and the second port, such that the output pressure of the first gas is dependent on the axial position of the piston; and
    a resilient member configured to bias the piston,
    wherein the valve comprises a chamber at least partly defined by the piston and in fluid communication with the second port, such that the force exerted by the second gas within the chamber on the piston acts against the action of the resilient member.

    REGULATING DEVICE FOR TORQUE LIMITER
    10.
    发明公开

    公开(公告)号:EP3699448A1

    公开(公告)日:2020-08-26

    申请号:EP19159100.7

    申请日:2019-02-25

    IPC分类号: F16D7/04 F16D43/202

    摘要: An apparatus (100) for regulating a torque limiter, comprising a resilient member (130) configured to exert a force on one or more components of the torque limiter, wherein the force exerted by the resilient member (130) adjusts a torque limit of the torque limiter in use, a movable abutment (180) configured to contact the resilient member (130) and translatable in an axial direction to vary the force exerted by the resilient member (130), a nut (170) rotatable about the axis and configured to contact the movable abutment (180) such that a given rotational position of the nut (170) corresponds to a given axial position of the movable abutment (180), and an anti-rotation member (160) configured to move between first and second positions. In the first position the anti-rotation member (160) prevents rotational movement of the nut (170) and, in turn, prevents axial movement of the movable abutment (180), and in the second position the anti-rotation member (160) does not prevent rotational movement of the nut (170) and permits rotation of the nut (170) and, in turn, axial movement of the movable abutment (180) to vary the force exerted by the resilient member (130).