A gas turbine engine includes a fan shaft and a support which supports the fan shaft. A channel is formed between the source region and the drain region. The inner part adapted to receive a portion of a finish of the bottle.
Algorithmically generated prior art
A gas turbine engine includes a fan shaft and a support which supports the fan shaft. A channel is formed between the source region and the drain region. The inner part adapted to receive a portion of a finish of the bottle.