Interface for a valve for a cryogenic fluid duct

Patent metadata

Field	Value
Publication number	US-10371309-B2
Application number	US-201515128843-A
Country	US
Kind code	B2
Filing date	Mar 18, 2015
Priority date	Mar 27, 2014
Publication date	Aug 6, 2019
Grant date	Aug 6, 2019

Abstract

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 ).

First claim

The invention claimed is:

1. An assembly comprising a duct for passing a flow of cryogenic fluid and a valve adapted to shut said duct selectively;
the assembly being characterized in that the duct includes an interface for inserting the valve, the interface forming an internal abutment inside the duct and an external abutment outside the duct;
the valve being configured so as to be removably inserted into said insertion interface by sliding, the valve comprising a valve body presenting a first end and a second end, the valve body being adapted to be removably bolted in said insertion interface so that the first end and the second end come into abutment respectively against the internal abutment and against the external abutment of the duct, the assembly including an internal sealing element arranged between the internal abutment of the duct and the first end of the valve body, and an external sealing element arranged between the external abutment of the duct and the second end of the valve body; and
wherein the valve body and/or the duct include(s) an index suitable for orienting the valve body while it is being inserted in the duct, and
wherein said duct includes a first portion and a second portion relative to the valve, said first and second portions:
not being in alignment with each other;
not being perpendicular with each other; and
forming a deflection in the flow of fluid in the duct,

wherein the insertion interface is arranged in line with one of the first and second portions so that the valve is inserted in the duct in alignment with said first portion or said second portion.

2. An assembly according to claim 1 , wherein the internal abutment and the external abutment of the duct are formed by two parallel surfaces, and wherein the internal sealing element is more flexible than the external sealing element.

3. An assembly according to claim 1 , wherein said valve further includes an actuator assembled on said valve body, outside the duct.

4. An assembly according to claim 1 , wherein the valve is of the type having a valve member, a cylindrical plug, or a tube.

5. An assembly according to claim 1 , wherein the flow of fluid in the duct is configured so that the first portion is a portion that is upstream relative to the valve, and the second portion is a portion that is downstream relative to the valve.

6. An assembly according to claim 1 , wherein the flow of fluid in the duct is configured so that the first portion is a portion that is downstream relative to the valve, and the second portion is a portion that is upstream relative to the valve.

7. A space vehicle engine including an assembly according to claim 1 , wherein the second portion and the first portion of the duct are assembled to the engine by welding.

8. An assembly according to claim 2 , wherein said valve further includes an actuator assembled on said valve body, outside the duct.

Assignees

• Safran Aircraft Engines

Inventors

• Gazave Robert
• Millon Frédérick

Classifications

• F16L59/141 Primary

  in which the temperature of the medium is below that of the ambient temperature · CPC title

• F16K27/02 Primary

  of lift valves (for reducing the flow resistance of screw-spindle lift-valves F16K1/06) · CPC title

• F16L59/161

  Housings for valves, tee pieces, or the like · CPC title