Combustor liner support assembly

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60 3932, 60752, 60753, F02C 720

Patent

active

052917320

ABSTRACT:
A support assembly for a gas turbine engine combustor includes an annular frame having a plurality of circumferentially spaced apart tenons, and an annular combustor liner disposed coaxially with the frame and including a plurality of circumferentially spaced apart tenons circumferentially adjoining respective ones of the frame tenons for radially and tangentially supporting the liner to the frame while allowing unrestrained differential thermal radial movement therebetween.

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Jones, "Advanced Technology for Reducing Aircraft Engine Pollution," Nov. 1974, Transactions of the ASME, Serie B: Journal of Engineering for Industry, pp. 1354-1360.

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