| CPC F16N 23/00 (2013.01) [B01D 19/00 (2013.01); F05D 2260/602 (2013.01); F05D 2260/609 (2013.01); F16N 2210/08 (2013.01)] | 20 Claims |

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1. A blowdown valve for an aircraft engine lubrication system, the blowdown valve comprising:
a valve body defining:
a chamber;
an inlet for receiving a mixture of air and lubricating fluid into the chamber;
a first outlet for releasing a first portion of the mixture out of the chamber; and
a second outlet for releasing a second portion of the mixture out of the chamber, the second outlet being disposed downstream of the first outlet relative to the inlet; and
a valve member disposed inside the chamber of the valve body, the valve member being translatable along an axis between:
a valve-closed position where the valve member hinders fluid flow through the inlet; and
a valve-open position corresponding to a downstream translation limit of the valve member where:
fluid flow is permitted through the inlet;
fluid flow is permitted from the inlet to the first outlet and through the first outlet;
fluid flow is permitted from the inlet to the second outlet and through the second outlet by flowing radially outwardly around and past the valve member; and
the valve member is disposed between the inlet and the second outlet.
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