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    • 2. 发明公开
    • ACTIVE CLEARANCE CONTROL WITH INTEGRAL DOUBLE WALL HEAT SHIELDING
    • 积分双壁热屏蔽主动间隙控制
    • EP3159493A1
    • 2017-04-26
    • EP16194079.6
    • 2016-10-17
    • General Electric Company
    • SABO, Nicolas, KristopherSCHIMMELS, Scott, AlanSHIVANATHAN, SivarubanPENDURTI, Srinivas
    • F01D11/24
    • F01D25/145F01D11/24F02C3/04F05D2220/32F05D2260/201F05D2300/175Y02T50/671Y02T50/676
    • A gas turbine engine thermal control double-wall apparatus 312 for active clearance control and a method of using the apparatus are provided herein. The apparatus 312 has a thermal air distribution manifold 350 encircling an axially extending portion of an engine outer casing 466. The manifold 350 has a plurality of header assemblies 357 with an annular supply tube 354 and a plurality of annular spray rails 460 in fluid supply communication with at least one of the plurality of supply plenums 356. The annular spray rails 460 define spray holes 462 that are oriented to impinge thermal control air 336 onto the outer casing 466 having at least one thermal control ring 484 attached thereto before being exhausted from circumferentially extending exhaust passages 526. All of the thermal control apparatus 312 surfaces in direct contact with the thermal control air 336 are constructed of an integrated double wall heat shield 610 defining a hermetically sealed cavity 612 between the walls therein.
    • 本文提供了用于主动间隙控制的燃气涡轮发动机热控制双壁装置312以及使用该装置的方法。 设备312具有围绕发动机外壳466的轴向延伸部分的热空气分配歧管350.歧管350具有多个联管箱组件357,联管箱组件357具有环形供应管354和多个流体供应通信的环形喷雾轨道460 与多个供应增压室356中的至少一个相关联。环形喷射轨道460限定喷射孔462,所述喷射孔462定向成将热控制空气336撞击到外壳466上,所述外壳466具有至少一个附接到其上的热控制环484,然后从圆周 延伸的排气通道526.与热控制空气336直接接触的所有热控制设备312表面由在其中的壁之间限定密封的空腔612的集成双壁热屏蔽610构成。