发明名称 TURBINE SNAP IN SPRING SEAL
摘要 Snap in annular spring seal (52) including continuous or split full 360 degree ring (79) having radially outer second seal end (55) spaced outwardly of a radially inner first end (53) of the ring (79) and axial biasing means urging first and second seal ends (55, 53) apart. Biasing means may include an axially aftwardly opening conical section (70) connecting first and second seal ends (55, 53) and second seal end (55) having outer aftwardly opening V shaped cross-sectional bend (66) or circular cross-sectional bend (67). Spring seal (52) may extend radially and circumferentially between and in sealing engagement with first and second annular turbine components (4, 6). First end (53) may be spring-loaded and removably secured in U-shaped or V-shaped slot (54) of turbine component. Slot (54) may include symmetrical inner U-shaped bent first seal end (83) including annular substantially parallel or non-parallel forward and aft legs (56, 58) connected by semi-circular cross-sectional bend (60). Seal (52) may include bowed section (80) connecting circular seal ends (55, 53).
申请公布号 CA2941835(A1) 申请公布日期 2017.03.24
申请号 CA20162941835 申请日期 2016.09.15
申请人 GENERAL ELECTRIC COMPANY 发明人 BROOMER, MARK;SEVINCER, EDIP;MARIN, ANTHONY CHRISTOPHER
分类号 F02C7/28;F01D9/02 主分类号 F02C7/28
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