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    METHOD FOR MAKING HEAT BARRIER COATINGS, COATINGS AND STRUCTURE OBTAINED THEREBY AS WELL AS COMPONENTS COATED THEREWITH
    1.
    发明申请
    METHOD FOR MAKING HEAT BARRIER COATINGS, COATINGS AND STRUCTURE OBTAINED THEREBY AS WELL AS COMPONENTS COATED THEREWITH 审中-公开
    制造热障涂层的方法，涂层和结构，以及作为组分的组分

    公开(公告)号：WO2008040678A1

    公开(公告)日：2008-04-10

    申请号：PCT/EP2007/060287

    申请日：2007-09-28

    Applicant: TURBOCOATING S.P.A. ,  ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  RIZZI, Gabriele

    Inventor： ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  RIZZI, Gabriele

    IPC: B05D1/02 ,  B05D7/00 ,  C23C4/08 ,  C23C4/12

    CPC classification number: C23C4/02 ,  C23C4/11 ,  C23C4/12

    Abstract: A method for making a thermal barrier coating (11), such as for gas turbine components (5) and mainly heat shields, combustion chambers or turbine wall covering panels, said thermal barrier coating (11 ) resulting from successive deposition of various numbers of layers (13, 15) which join together to form the coating (11 ), which coating (11 ) is obtained by any Thermal Spray process, including the steps of laying at least three coating layers (13), each of said layers being deposited at a different angle (τ, β, α) of the spray torch (33); said angles (τ, β, α) being defined relative to the surface to be sprayed and covering a range from 30° to 150° with respect to the tangent to the surface (3) of the component (5) to be coated. Protection also extends to the component so coated and the covering structure.

    Abstract translation: 一种用于制造隔热涂层（11）的方法，例如用于燃气涡轮机部件（5）和主要是隔热罩，燃烧室或涡轮机壁覆盖板的所述热障涂层（11），所述热障涂层（11）由连续沉积各种层数 （13,15），其连接在一起以形成涂层（11），所述涂层（11）通过任何热喷涂方法获得，包括以下步骤：铺设至少三个涂层（13），每个所述层被沉积在 喷枪（33）的不同角度（t，ß，a）; 所述角度（t，β，a）相对于待喷涂的表面被限定，相对于待涂覆的组分（5）的表面（3）的切线覆盖30°至150°的范围。 保护也延伸到如此涂层和覆盖结构的部件。

    METHOD AND EQUIPMENT FOR REMOVAL OF CERAMIC COATINGS BY SOLID CO2 BLASTING
    2.
    发明申请
    METHOD AND EQUIPMENT FOR REMOVAL OF CERAMIC COATINGS BY SOLID CO2 BLASTING 审中-公开
    通过固体CO2喷砂去除陶瓷涂层的方法和设备

    公开(公告)号：WO2011135526A1

    公开(公告)日：2011-11-03

    申请号：PCT/IB2011/051839

    申请日：2011-04-27

    Applicant: TURBOCOATING S.P.A. ,  A & G CHEMICAL PRODUCTION S.R.L. ,  SCRIVANI, Andrea ,  GIOLLI, Carlo ,  ALLEGRINI, Bruno, Antonio

    Inventor： SCRIVANI, Andrea ,  GIOLLI, Carlo ,  ALLEGRINI, Bruno, Antonio

    IPC: B24C1/00 ,  B24C1/08

    CPC classification number: B24C1/003 ,  B24C1/08

    Abstract: A method for removing ceramic coatings using a special equipment without modifying the characteristics of the substrate such as roughness and thickness and able to prepare the substrate to be recoated with a new ceramic layer, is provided. The removing of the ceramic coating without damaging the substrate characteristics is obtained by a combination of coating/substrate preheating by irradiation during or immediately before the stripping and improved solid CO 2 blasting equipment and parameters.

    Abstract translation: 提供了一种使用特殊设备去除陶瓷涂层的方法，而不改变基板的特性，例如粗糙度和厚度，并且能够制备用新的陶瓷层重新涂覆的基板。 通过在剥离期间或之前通过照射预先涂覆的涂层/基板和改进的固体二氧化碳喷砂设备和参数的组合来获得陶瓷涂层的去除而不损害基板特性。

    TORCH FOR THERMAL SPRAYING OF SURFACE COATINGS, AND COATINGS OBTAINED THEREBY
    4.
    发明申请
    TORCH FOR THERMAL SPRAYING OF SURFACE COATINGS, AND COATINGS OBTAINED THEREBY 审中-公开
    用于表面涂层的热喷涂的TORCH和由其获得的涂料

    公开(公告)号：WO2007116036A1

    公开(公告)日：2007-10-18

    申请号：PCT/EP2007/053426

    申请日：2007-04-06

    Applicant: TURBOCOATING S.P.A. ,  ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  SCARTAZZA, Michele ,  RIZZI, Gabriele

    Inventor： ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  SCARTAZZA, Michele ,  RIZZI, Gabriele

    IPC: B05B7/22

    CPC classification number: B05B15/62 ,  B05B7/201 ,  B05B7/222

    Abstract: A torch (1) for thermal spraying of surface coatings, of the type that comprises a head (3) and a bracket (2) for the head (3), in which the head (3) pivots relative to the bracket (2). The invention also relates to the coatings obtained using the torch, whether of polymer, metal or ceramic materials, on any substrate coated thereby, whether of polymer, metal or ceramic or composite materials. The invention is applicable to different types of thermal spray torches, using plasma spray, combustion spray, High Velocity Oxygen Fuel (HVOF), or Low Velocity processes.

    Abstract translation: 一种用于热喷涂表面涂层的火炬（1），其包括用于头部（3）的头部（3）和支架（2）的类型，头部（3）相对于支架（2）枢转， 。 本发明还涉及使用手电筒（无论是聚合物，金属或陶瓷材料）在由其涂覆的任何基材上获得的涂层，无论是聚合物，金属还是陶瓷或复合材料。 本发明适用于不同类型的热喷枪，使用等离子喷涂，燃烧喷雾，高速氧燃料（HVOF）或低速工艺。

    METHOD FOR MAKING HEAT BARRIER COATINGS
    6.
    发明授权
    METHOD FOR MAKING HEAT BARRIER COATINGS 有权
    工艺用于产生热能LAYERS

    公开(公告)号：EP2069080B1

    公开(公告)日：2010-11-03

    申请号：EP07820675.2

    申请日：2007-09-28

    Applicant: Turbocoating S.P.A.

    Inventor： ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  RIZZI, Gabriele

    IPC: C23C4/02 ,  C23C4/10 ,  C23C4/12

    CPC classification number: C23C4/02 ,  C23C4/11 ,  C23C4/12

    Abstract: A method for making a thermal barrier coating (11), such as for gas turbine components (5) and mainly heat shields, combustion chambers or turbine wall covering panels, said thermal barrier coating (11 ) resulting from successive deposition of various numbers of layers (13, 15) which join together to form the coating (11 ), which coating (11 ) is obtained by any Thermal Spray process, including the steps of laying at least three coating layers (13), each of said layers being deposited at a different angle (τ, β, α) of the spray torch (33); said angles (τ, β, α) being defined relative to the surface to be sprayed and covering a range from 30° to 150° with respect to the tangent to the surface (3) of the component (5) to be coated. Protection also extends to the component so coated and the covering structure.

    METHOD FOR MAKING HEAT BARRIER COATINGS, COATINGS AND STRUCTURE OBTAINED THEREBY AS WELL AS COMPONENTS COATED THEREWITH
    9.
    发明公开
    METHOD FOR MAKING HEAT BARRIER COATINGS, COATINGS AND STRUCTURE OBTAINED THEREBY AS WELL AS COMPONENTS COATED THEREWITH 有权
    工艺用于产生热能LAYERS

    公开(公告)号：EP2069080A1

    公开(公告)日：2009-06-17

    申请号：EP07820675.2

    申请日：2007-09-28

    Applicant: Turbocoating S.P.A.

    Inventor： ANTOLOTTI, Nelso ,  SCRIVANI, Andrea ,  RIZZI, Gabriele

    IPC: B05D1/02 ,  B05D7/00 ,  C23C4/08 ,  C23C4/12

    CPC classification number: C23C4/02 ,  C23C4/11 ,  C23C4/12

    Abstract: A method for making a thermal barrier coating (11), such as for gas turbine components (5) and mainly heat shields, combustion chambers or turbine wall covering panels, said thermal barrier coating (11 ) resulting from successive deposition of various numbers of layers (13, 15) which join together to form the coating (11 ), which coating (11 ) is obtained by any Thermal Spray process, including the steps of laying at least three coating layers (13), each of said layers being deposited at a different angle (τ, β, α) of the spray torch (33); said angles (τ, β, α) being defined relative to the surface to be sprayed and covering a range from 30° to 150° with respect to the tangent to the surface (3) of the component (5) to be coated. Protection also extends to the component so coated and the covering structure.

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