CPC F04D 29/601 (2013.01) [F04D 29/441 (2013.01)] | 8 Claims |
1. An alignment tool for aligning a plurality of diffuser pipes of a centrifugal compressor relative to a casing of an aircraft engine, the alignment tool comprising:
a body defining a center axis and having at least one tool datum configured for abutting against the casing; and
a plurality of alignment members fixed to the body and extending radially from the body relative to the center axis, each alignment member of the plurality of alignment members having a respective fixed position relative to the at least one tool datum, the plurality of alignment members configured to abut the plurality of diffuser pipes.
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