Patent ID: 8201389

Claim:
A gas turbine engine lubrication system comprising at least first and second bearing compartments of a gas turbine engine, said first bearing compartment housing multiple bearing components; the system further comprising a main oil supply; and an oil distributing unit having a central body mounted in said first bearing compartment and having one inlet port connected in flow communication with the main oil supply, the central body defining a central conduit connected to said inlet port, the oil distributing unit having at least one outlet transfer port branching off from said central conduit and connected to a transfer tube extending into said second bearing compartment for supplying oil to a bearing component housed in the second bearing compartment, the oil distributing unit further having multiple nozzles branching off from the central conduit of the central body and pointing to different bearing components in the first bearing compartment for lubricating the multiple bearing components housed in the first bearing compartment from said central body.