Oil filler tube assembly for aircraft engine
AssigneePratt & Whitney Canada Corp.
InventorsAhmad Cheikhzen, Victor Sa Melo, Michel Labbe, Penny Nicolaidis, Daniel Alecu
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AssigneePratt & Whitney Canada Corp.
InventorsAhmad Cheikhzen, Victor Sa Melo, Michel Labbe, Penny Nicolaidis, Daniel Alecu
Estimating the term…
An oil filler assembly for an aircraft engine, has: a filler tube extending from a bottom end to a top end; a valve having a tube side fluidly connected to the filler tube and a tank side; a cap removably secured to the top end; a dipstick secured to the cap and extending into the filler tube; and a piston secured to the dipstick, the piston having: a sealing configuration in which the piston sealingly engages the filler tube to fluidly disconnect the top end from the valve, the piston being in the sealing configuration when the cap is secured to the top end of the filler tube; and a venting configuration in which the piston permits fluid communication between the top end and the valve, the piston being in the venting configuration when the cap is moved away from the top end of the filler tube.
An oil filler assembly for an aircraft engine, comprising:
An aircraft engine, comprising:
A method for mitigating detrimental effects of air in a filler tube, the filler tube fluidly connected to an oil tank via a valve, the filler tube closable with a cap secured to a dipstick, the filler tube fluidly disconnectable from an environment with a piston secured to the dipstick, the method comprising:
Dependencies are inferred from the claim text.