Linear compressor
    13.
    发明授权

    公开(公告)号:US11603834B2

    公开(公告)日:2023-03-14

    申请号:US17065958

    申请日:2020-10-08

    Abstract: A compressor is disclosed. A compressor according to the present discloser includes a piston structure which has a guide member reciprocating inside a cylinder in an axial direction, and a magnet frame which supports a mover moving together with the piston structure, in which the piston structure includes the guide member, a mount member connected to the magnet frame, and an elastic member provided between the guide member and the mount member and capable of elastic deformation.

    Linear compressor
    17.
    发明授权

    公开(公告)号:US09890772B2

    公开(公告)日:2018-02-13

    申请号:US14804425

    申请日:2015-07-21

    Abstract: A linear compressor is provided that may include a shell in which a discharge port is provided, a cylinder disposed in the shell to define a compression space for a refrigerant, a piston disposed to be reciprocated in an axial direction within the cylinder, a discharge valve disposed on or at one side of the cylinder to selectively discharge the refrigerant compressed in the compression space, the discharge valve including an insertion protrusion, and a valve spring coupled to the discharge valve to provide a restoring force to the discharge valve. The valve spring may include a spring body having a central portion defined at a portion corresponding to a center of the cylinder, and an insertion hole defined in the spring body. The insertion hole may be coupled to the insertion protrusion of the discharge valve. The central portion of the spring body may be spaced apart from a central portion of the insertion hole.

    LINEAR COMPRESSOR
    18.
    发明申请
    LINEAR COMPRESSOR 审中-公开

    公开(公告)号:US20170321672A1

    公开(公告)日:2017-11-09

    申请号:US15584334

    申请日:2017-05-02

    Abstract: A linear compressor is provided. The linear compressor may include a suction valve with a plurality of wings. Each of the plurality of wings may include two first edge portions that extend in an outer direction of a fixing portion, and a second edge portion forming an outer circumferential portion of the wing. A distance between a first edge portion of a first wing among the plurality of wings and a second edge portion of a second wing among the plurality of wings gradually increases toward the outer direction of the suction valve.

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