Slotted exhaust liner

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

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Details

60752, F23R 360, F02C 728

Patent

active

055355854

ABSTRACT:
A gas turbine exhaust liner contains air holes and a transverse slot to relieve thermally induced stresses on the liner, which is a catenary. The slot is covered by a seal, also a catenary, having two pieces that are joined in a way that allows them the expand with the liner so that the seal does not place thermal stresses across the liner.

REFERENCES:
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patent: 3031844 (1962-05-01), Tomolonius
patent: 4800718 (1989-01-01), Zimmerman
patent: 4854122 (1989-08-01), Belling
patent: 4887663 (1989-12-01), Auxier et al.
patent: 5069034 (1991-12-01), Jourdain et al.
patent: 5333443 (1994-08-01), Halila
patent: 5337583 (1994-08-01), Giles et al.
patent: 5363643 (1994-11-01), Halila

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