REINFORCED BLADE
    1.
    发明申请

    公开(公告)号:US20220251958A1

    公开(公告)日:2022-08-11

    申请号:US17729159

    申请日:2022-04-26

    申请人: Ratier-Figeac SAS

    发明人: Pascal AMAT

    摘要: A propeller blade comprises a root, a tip distal from the root, a trailing edge extending from the root to the tip, a trailing edge, e.g. foam, insert, a shell forming an outer surface of the propeller blade and a plurality of stitches of yam extending through two parts of the shell adjacent the trailing edge, wherein the yarns do not extend through the trailing edge insert.

    BRAIDING
    2.
    发明申请
    BRAIDING 有权

    公开(公告)号:US20210206481A1

    公开(公告)日:2021-07-08

    申请号:US17142572

    申请日:2021-01-06

    申请人: Ratier-Figeac SAS

    IPC分类号: B64C27/473 D04C1/12 D04C3/48

    摘要: A method of applying a braided cover to a core comprises braiding a plurality of tows around the core from a plurality of bobbins. One or more properties of the tow on a respective bobbin vary along the length of the tow.

    PROPELLER BLADE
    5.
    发明公开
    PROPELLER BLADE 审中-公开

    公开(公告)号:US20240109645A1

    公开(公告)日:2024-04-04

    申请号:US18364188

    申请日:2023-08-02

    申请人: Ratier-Figeac SAS

    IPC分类号: B64C11/26 B29C59/16 B29C70/24

    摘要: A propeller blade comprising a composite member. The composite member comprises a stack of plies and a matrix in which the stack of plies is embedded. At least one ply comprises a plurality of first yarns aligned in a first direction defining a plane of the ply and a plurality of second yarns extending transverse to the plane of the ply. Each second yarn does not extend through more than one ply. Also provided is a propelling system comprising the propeller blade, a composite propeller blade prepreg, and a method of forming a propeller blade.

    REINFORCED BLADE AND SPAR
    7.
    发明申请

    公开(公告)号:US20180127088A1

    公开(公告)日:2018-05-10

    申请号:US15806502

    申请日:2017-11-08

    申请人: Ratier-Figeac SAS

    发明人: Pascal AMAT

    摘要: A spar for a propeller blade comprises central structural member extending from a root to a tip of the spar. A first portion of the central structural member extends from the root of the spar and a second portion extends from the tip and adjoins the first portion. The central structural member includes a first plurality of plies of composite material on a pressure side thereof and a second plurality of plies of composite material on a suction side thereof wherein the first plurality of plies are in contact with the second plurality of plies in the second portion from a leading edge to a trailing edge thereof. A plurality of yarns extends through the central structural member in at least the second portion.

    MULTI-LAYER BRAIDED ARTICLE
    8.
    发明公开

    公开(公告)号:US20240150009A1

    公开(公告)日:2024-05-09

    申请号:US18415987

    申请日:2024-01-18

    申请人: Ratier-Figeac SAS

    IPC分类号: B64C11/26 D04C1/06

    摘要: A multi-layer braided article and a method of making the multi-layer braided article. The multi-layer braided article includes a braid extending along a first axis, wherein the braid is folded over itself to form a first layer and a second layer; and a wrapper laid over the first layer of the braid and extending circumferentially around the first axis, wherein the wrapper defines an edge of the first layer about which the braid is folded. The multi-layer braided article may form part of a blade for an aircraft. A sleeve may be provided around a conical portion of the article to connect the article to something else, such as a propeller hub, where the multi-layer braided article is formed as part of a blade. The sleeve may provide a primary or secondary load path.

    MULTI-LAYER BRAIDED ARTICLE
    9.
    发明申请

    公开(公告)号:US20210403142A1

    公开(公告)日:2021-12-30

    申请号:US17307014

    申请日:2021-05-04

    申请人: Ratier-Figeac SAS

    IPC分类号: B64C11/26 D04C1/06

    摘要: A multi-layer braided article and a method of making the multi-layer braided article. The multi-layer braided article includes a braid extending along a first axis, wherein the braid is folded over itself to form a first layer and a second layer; and a wrapper laid over the first layer of the braid and extending circumferentially around the first axis, wherein the wrapper defines an edge of the first layer about which the braid is folded. The multi-layer braided article may form part of a blade for an aircraft. A sleeve may be provided around a conical portion of the article to connect the article to something else, such as a propeller hub, where the multi-layer braided article is formed as part of a blade. The sleeve may provide a primary or secondary load path.