The present invention relates to a pipe assembly provided with a drainage system.
Conventionally, the pipe assembly comprises two pipes, and a joining device configured to connect the two pipes together.
Although not exclusively, the present invention relates more particularly to the transfer of fuel on an aircraft, in particular on a transport plane, for example in order to send fuel from a wing of the aircraft to an underwing engine attachment pylon, in order to supply the engine with fuel.
It is known that, in order to monitor possible leaks, such a pipe assembly comprising a connection of fuel transfer pipes (or lines) must be drained in specific zones.
Generally, drained connections comprise a complex and relatively bulky assembly of elements and seals.
The object of the present invention is to provide an efficient and more compact drainage system.
It relates to a pipe assembly comprising two pipes and a joining device configured to connect the two pipes together, said pipe assembly being provided with a drainage system.
According to the invention, the drainage system comprises:
Thus, by virtue of the invention, the pipe assembly comprises a drainage system by means of which it is possible to drain the joining device joining the two pipes, this drainage system being more compact and being particularly effective, as set out hereinbelow, being installed where the pipes meet (and are therefore weaker).
The pipe assembly may have at least some of the following special features, considered individually or in combination:
In one particular embodiment, the joining device has a general shape which is longitudinal with respect to the longitudinal axis of at least one section of each of the two pipes, and the two annular seals have one and the same diameter and they are arranged parallel to one another, coaxial with the longitudinal axis, being spaced apart longitudinally from one another.
In this particular embodiment, advantageously:
Furthermore, the present invention also relates to an aircraft, in particular a transport plane, which comprises at least one pipe assembly such as that mentioned above.
The attached figures will make it easy to understand how the invention may be embodied. In these figures identical references denote elements that are similar.
The pipe assembly 1 shown in
In a preferred application, the pipe assembly may be designed more particularly to send fuel from a wing of an aircraft to an underwing engine attachment pylon, in order to supply the engine with fuel. The pipe assembly may then be located between the primary structure of the attachment pylon and the wing, and it may provide the connection between a fuel line (or conduit) of the wing and a fuel line (or conduit) of the pylon.
As shown in
According to the invention, the drainage system 5 comprises:
The drainage element 9 is configured to send fluid present in the drainage slot 6 from its first end 10 to its other end (not shown), as indicated by a respective arrow F in
Thus, by virtue of the invention, the pipe assembly 1 comprises a particularly effective drainage system 5, which is installed on the joining device 4, that is to say where the two pipes 2 and 3 meet (and are therefore weaker). This drainage system 5 makes it possible to drain the device 4 joining the two pipes and to identify (and locate) leaks.
In one preferred embodiment, the joining device 4 is made of the same material as pipes 2 and 3 (generally entirely made of metal).
In addition, preferably, said annular seals 7 and 8 are O-rings.
Moreover, the drainage element 9 is provided with a hollow cylinder 11. A first end of the hollow cylinder 11 enters the drainage slot 6 and the second end is connected to a flexible line 12. Moreover, a rigid line 13 may be connected to this flexible line 12 so as to evacuate the drained fluid in the direction indicated by the arrow F. This rigid line 13 may in particular be attached by means of one or more attachment plates 14 to a pipe 3.
In the embodiment shown in
The two annular seals 7 and 8 have the same diameter and they are arranged parallel to one another, coaxial with the longitudinal axis L, being spaced apart longitudinally from one another and being provided on either side of the drainage slot 6.
In this embodiment:
The drainage slot 6, as well as grooves 19 and 20 for accommodating the annular seals 7 and 8, are created in the outer periphery 24 of said end section 23, in the form of annular grooves which are coaxial with the longitudinal axis L.
The pipe assembly further comprises a conventional retaining ring 25, which attaches the section 22 to the section 23. The drainage element 9 comprises, also, a connection element 26 to which is connected the flexible line 12, and which is attached to the section 22.
This embodiment, in which the joining device 4 is arranged longitudinally and comprises a covering for pipe end sections, is more compact as it is not necessary to attach together portions around the pipes. This embodiment may thus be easily mounted in any area, in particular of an aircraft, in which space is reduced, and may in particular be designed for the abovementioned application between a wing and a pylon, to supply an engine with fuel.
The drainage system 5 uses a double-wall system, formed by two annular seals 7 and 8, in order to guide the liquid in the drainage slot 6 to the drainage element 9. The two walls are created by the annular seals 7 and 8, which are preferably O-rings and which are arranged over the entire perimeter of the pipe, while the drainage element 9 is in one location.
Thus, whatever the weaker region in question, the first annular seal 7 prevents the drained liquid entering the pipes, and the second annular seal 8 prevents liquid present in the drainage slot 6 from reaching the outside of the pipes.
It is to be noted that, in the pipe assembly 1, it is not necessary for the two joints 7 and 8 to be arranged in the same plane, and preferably downstream of the drainage slot 6, since the joining device 4 is arranged longitudinally, in the axis L of the pipe assembly 1.
Number | Date | Country | Kind |
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FR1462883 | Dec 2014 | FR | national |