Method and system for the disassembly of an annular combustor

Details Method and system for the disassembly of an annular combustor Method and system for the disassembly of an annular combustor

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/42 (2006.01) F01D 25/28 (2006.01) F23R 3/50 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2056587

13DV-10389 ABSTRACT OF THE DISCLOSURE An apparatus and method for effecting the disassembly of an annular combustor for the maintenance of very large power generation gas generators such as those used in military aircraft engines, commercial aircraft engines, and smaller power generation turbines. The apparatus utilizes rollers which are attachable to a lower half outer casing. An inversion ring located radially inward from the lower half outer casing is supported by the rollers. By disconnecting a removable upper half outer casing, the combustor segments of a first section of the combustor can be removed. Supports connected to the first section of the combustor are secured by pins to a tool ring which is in turn secured to the inversion ring so as to create a closed path. By removing pins which secure the inversion ring and lower half outer casing to supports connected to a second section of combustor segments, the combustor can be rotated so that the second section of formerly inaccessible segments can be easily removed.

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