DYNAMIC SEALING IN AN AIRCRAFT TURBINE ENGINE CONTROL VALVE

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United States of America Patent

APP PUB NO 20240167571A1
SERIAL NO

18552584

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Abstract

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A control valve, in particular for an aircraft turbine engine, includes a movable seal which is carried by a rod that passes through ports of a body of the valve. Sealing means are mounted in each of these ports. The sealing means include a tubular bellows mounted around the rod, a ring mounted around the rod and the tubular bellows and at least partially housed in one of the ports, and a washer mounted around the rod. The washer is inserted between the tubular bellows and one end of the ring which bears against the bottom of said port.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AEROSYSTEMS61 RUE PIERRE CURIE PLAISIR 78370

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
DOYEN, Emmanuel MOISSY-CRAMAYEL, FR 1 0

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges18823301 - 10010020030040050060070080090010001100120013001400150016001700180019002000

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