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    BURNER
    1.
    发明申请
    BURNER 有权

    公开(公告)号：US20220364726A1

    公开(公告)日：2022-11-17

    申请号：US17746521

    申请日：2022-05-17

    Applicant: BECKETT THERMAL SOLUTIONS S.R.L.

    Inventor： Luca BAROZZI

    IPC: F23N5/24 ,  F23D14/02 ,  F23D14/70

    Abstract: A burner includes a diffuser wall delimiting an inner space in flow communication with an inlet passageway and forming a diffuser perforation for the gas mixture to pass from the inner space to an outer side of the diffuser wall where combustion occurs. A pilot chamber is formed in the inner space and delimited by a pilot portion of the diffuser wall, forming a pilot perforation, and by a pilot wall extended into the inner space. The pilot chamber forms pilot inlet openings supplying air/gas-air pre-mixture into the pilot chamber. A pilot gas opening supplies non-premixed fuel gas into the pilot chamber. A main chamber formed in the inner space is delimited by a diffuser wall main portion, forming a main perforation, and by the pilot wall. The main chamber delimits a main inner volume and is in flow communication with the inlet passageway to supply air/gas-air pre-mixture.

    COMBUSTION MEMBRANE FOR A GAS BURNER
    2.
    发明申请
    COMBUSTION MEMBRANE FOR A GAS BURNER 有权

    公开(公告)号：US20220170631A1

    公开(公告)日：2022-06-02

    申请号：US17536770

    申请日：2021-11-29

    Applicant: BECKETT THERMAL SOLUTIONS S.R.L.

    Inventor： Luca SIGHINOLFI ,  Massimo GILIOLI ,  Gabriele GANGALE ,  Ettore ETENZI

    IPC: F23D14/14 ,  F23D14/70

    Abstract: A combustion membrane (14, 14′) for a gas burner (2) forms a multilayer panel (22) including a gas-permeable diffuser layer (24) of a porous or fibrous solid material other than metal sheet, the diffuser layer (24) forming a combustion surface (25) facing an outer side (17), a support layer (26) formed by a metal sheet (32), arranged on an inner side (23) with respect to the diffuser layer (24), opposite to the combustion surface (25), and connected to the diffuser layer. The metal sheet has a pattern (27) of passage openings (28), a local deviating layer (29), bordering the support layer (26). Diverter flaps (30) bent transversely out of the support layer (26) and delimited by cutting or tearing edges (42) of the support layer metal sheet (32), form guide surfaces (31) oblique to a direction (40) orthogonal to an extension plane (41) of the multilayer panel (22).

    COMBUSTION MEMBRANE FOR A GAS BURNER
    3.
    发明申请
    COMBUSTION MEMBRANE FOR A GAS BURNER 有权

    公开(公告)号：US20240410573A1

    公开(公告)日：2024-12-12

    申请号：US18700354

    申请日：2022-07-26

    Applicant: BECKETT THERMAL SOLUTIONS S.R.L.

    Inventor： Massimo GILIOLI ,  Alberto PEZZIN ,  Andrea CASONI

    IPC: F23D14/14 ,  D03D13/00 ,  D03D15/30 ,  D03D15/67 ,  F23D14/02 ,  F23D14/84

    Abstract: A combustion membrane for a gas burner including a fabric having two opposite fabric surfaces, which form a combustion surface exposed on the outer side and an inner surface facing towards an inner side respectively, where the fabric forms an interlacing of metal wires having warp threads and weft threads transverse to the warp threads, and where both fabric surfaces form ribs in high relief alternating with valleys in low relief and that both the ribs and the valleys have an extension, in at least one direction in the plane of the fabric, greater than the space occupied by at least three consecutive warp threads in the weft direction and greater than the space occupied by at least three consecutive weft threads in the warp direction.

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