Interface for a valve for a cryogenic fluid duct
AssigneeSafran Aircraft Engines
InventorsRobert Gazave, Frédérick Millon
Life of this patent
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AssigneeSafran Aircraft Engines
InventorsRobert Gazave, Frédérick Millon
Estimating the term…
An assembly comprising a duct (1) for passing a flow of cryogenic fluid, and a valve (2); the assembly being characterized in that the duct (1) includes an interface for inserting the valve, the interface forming an internal abutment (51) and an external abutment (52); the valve (2) being configured in such a manner as to be inserted into said insertion interface by sliding, the valve (2) comprising a valve body (3) presenting a first end (31) and a second end (32), the valve body (3) being adapted to be bolted in said insertion interface in such a manner that the first end (31) and the second end (32) come into abutment respectively against the internal abutment (51) and against the external abutment (52), the assembly including an internal sealing element (61) arranged between the internal abutment (51) and the first end (31), and an external sealing element (62) arranged between the external abutment (52) and the second end (32).
An assembly comprising a duct for passing a flow of cryogenic fluid and a valve adapted to shut said duct selectively;
Dependencies are inferred from the claim text.