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    • 6. 发明公开
    • AIRCRAFT COMPONENTS WITH POROUS PORTION
    • FLUGZEUGKOMPONENTEN MITPORÖSEMTEIL
    • EP2930310A1
    • 2015-10-14
    • EP15156998.5
    • 2015-02-27
    • Pratt & Whitney Canada Corp.
    • Scalzo, OrlandoCompomanes, MarcBouthillier, Alain
    • F01D9/04F01D5/18F01D25/12B22F5/00B22F7/00
    • A component (20) including a porous portion (50a) which may be permeable or impermeable to air. The component is a cooled wall segment for a gas turbine engine, including a body defining a contact surface (24) configured to be in contact with circulating hot gas and an outer surface (32) configured to be in contact with cooling air. The body includes a first portion (52a) with at least one retention element, and a porous second portion (50a) made of a porous material permeable to air, containing a plurality of interconnected pores, and having a porosity greater than that of the first portion (52a). The second portion (50a) is engaged to the first portion (52a), defines at least part of the contact surface (24), and defines at least part of a fluid communication between the outer surface (32) and the contact surface (24) through the interconnected pores. The wall segment may be for example a heat shield or shroud segment.
    • 一种包括多孔部分(50a)的部件(20),所述多孔部分可透气或不透气。 该部件是用于燃气涡轮发动机的冷却壁段,包括限定构造成与循​​环热气接触的接触表面(24)的主体和构造成与冷却空气接触的外表面(32)。 本体包括具有至少一个保持元件的第一部分(52a)和由可渗透空气的多孔材料制成的多孔第二部分(50a),其包含多个相互连通的孔,并且具有大于第一部分 部分(52a)。 第二部分(50a)接合到第一部分(52a),限定接触表面(24)的至少一部分,并且限定外表面(32)和接触表面(24)之间的流体连通的至少一部分 )通过互连孔。 壁段可以是例如隔热罩或护罩区段。
    • 10. 发明公开
    • METHOD OF FORMING A COOLED WALL SEGMENT OF A GAS TURBINE ENGINE
    • ETELENHETELLUNGSVERFAHREN GASTURBINEWANDSEGMENT
    • EP2930309A1
    • 2015-10-14
    • EP15156994.4
    • 2015-02-27
    • Pratt & Whitney Canada Corp.
    • Scalzo, OrlandoCompomanes, MarcBouthillier, Alain
    • F01D9/04F01D5/18F01D25/12B22F5/00B22F7/00
    • F02C7/18B22F5/009B22F7/004F01D5/183F01D9/04F01D25/005F01D25/12F05D2230/21F05D2230/22F05D2260/203Y02T50/671Y02T50/6765
    • A method of forming a component (20) including a porous portion (50a) which may be permeable or impermeable to air. The component is a cooled wall segment for a gas turbine engine, including a body defining a contact surface (24) configured to be in contact with circulating hot gas and an outer surface (32) configured to be in contact with cooling air. The body includes a first portion (52a) with at least one retention element, and a porous second portion (50a) made of a porous material permeable to air, containing a plurality of interconnected pores, and having a porosity greater than that of the first portion (52a). The second portion (50a) is engaged to the first portion (52a), defines at least part of the contact surface (24), and defines at least part of a fluid communication between the outer surface (32) and the contact surface (24) through the interconnected pores. The wall segment may be for example a heat shield or shroud segment.
    • 一种形成包括多孔部分(50a)的部件(20)的方法,所述多孔部分可以是空气渗透的或不透气的。 该部件是用于燃气涡轮发动机的冷却壁段,包括限定构造成与循​​环热气接触的接触表面(24)的主体和构造成与冷却空气接触的外表面(32)。 本体包括具有至少一个保持元件的第一部分(52a)和由可渗透空气的多孔材料制成的多孔第二部分(50a),其包含多个相互连通的孔,并且具有大于第一部分 部分(52a)。 第二部分(50a)接合到第一部分(52a),限定接触表面(24)的至少一部分,并且限定外表面(32)和接触表面(24)之间的流体连通的至少一部分 )通过互连孔。 壁段可以是例如隔热罩或护罩区段。