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Combustor

Assembly

Reverse-flow annular combustion chamber. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.

Bill of materials for Combustor

3 top-level lines as of r178376
# Item / sub-assembly Part no. Qty/assy Ext. qty Parts Type
1 Combustor Liner turboprop-airliner-combustor-liner 1× 1 · part
2 Fuel Nozzle turboprop-airliner-fuel-nozzle 14× 14 · part
3 Igniter turboprop-airliner-igniter 2× 2 · part