Braking system for an aircraft wheel

    公开(公告)号:US11274716B2

    公开(公告)日:2022-03-15

    申请号:US16711188

    申请日:2019-12-11

    Abstract: A braking system (4) for an aircraft wheel (2) comprises first and second brake rotor discs (20a, 20b) axially spaced along an axis (A) and rotationally coupled to the wheel (2), a stator disc (24) arranged axially between the first and second rotor discs (20a, 20b), and a heat shield (34) mounted to at least one of the first and second rotor discs (20a, 20b). Radially outer portions (30) of the first and second rotor discs (20a, 20b) extend radially outwardly of the stator disc (24) to define a gap (32) between the radially outer portions (30) of the first and second rotor discs (20a, 20b). The heat shield (34) extends at least partially over or into the gap (32).

    PISTON ENGAGING MEMBER
    3.
    发明申请

    公开(公告)号:US20220033070A1

    公开(公告)日:2022-02-03

    申请号:US17386007

    申请日:2021-07-27

    Abstract: A piston engaging member of a piston assembly for engaging a pressure plate of an aircraft brake system, the engaging member comprising a body having a first side configured to selectably engage with the pressure plate, and a mount on a second side of the body configured to mount the piston engaging member with a piston of the piston assembly wherein the body comprises a cellular structure between the first and second sides.

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