AIRCRAFT FLUID CONDUIT COMPRISING THERMOPLASTIC PIPING AND CONNECTOR
20230364853 · 2023-11-16
Assignee
Inventors
Cpc classification
F16L37/084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C57/005
PERFORMING OPERATIONS; TRANSPORTING
F16L47/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A fluid conduit for aircraft, the conduit having a pipe made from thermoplastic material having a connection end which extends along a pipe axis and a connector which is intended to be mounted in the connection end by a translational movement along the pipe axis in a downstream direction, the connector having a joining portion which extends longitudinally along the connector axis and which is configured to extend into the connection end, the joining portion having a free longitudinal end which is chamfered, the free longitudinal end being configured to be radially deformed after the connector is mounted in the connection end, which has been thermally expanded beforehand, so that the conduit has an internal surface which has an internal radius which is substantially constant at the interface between the connector and the pipe.
Claims
1-11. (canceled)
12. An aircraft fluid conduit, the conduit comprising a piping of thermoplastic material comprising a connection end extending along a piping axis and a connector to be mounted in the connection end by a translational movement along the piping axis from upstream to downstream, the connection end defining a piping internal surface configured to be in contact with a fluid and a piping external surface, opposite to the piping internal surface, the connector extending along a connector axis and comprising a connecting portion, extending longitudinally along the connector axis configured to extend into the connection end, the connecting portion defining a connector internal surface, to be in contact with the fluid, and a connector external surface, opposite to the connector internal surface and configured to be in contact with the piping internal surface of the connection end, the connecting portion having a free longitudinal end that is beveled, the free longitudinal end of the connector is configured to be radially deformed following mounting the connector into the connector end, previously thermally expanded, so that the conduit has an internal surface having a substantially constant internal radius at the interface between the connector and the piping.
13. The conduit according to claim 12, wherein, in a longitudinal half cross-section plane with respect to the connector axis, the free longitudinal end comprises a tilted wall, with respect to the connector axis, formed on the connector internal surface.
14. The conduit according to claim 13, wherein the tilted wall forms with the connector axis a tilt angle of between 5 and 10°.
15. The conduit according to claim 13, wherein the connector internal surface comprises a longitudinal wall, with a constant internal radius, and a tilted wall.
16. The conduit according to claim 12, wherein the longitudinal length of the projection of the tilted wall onto the connector axis is between 3 and 6 mm.
17. The conduit according to claim 12, wherein the longitudinal length of the longitudinal wall is between 9 and 25 mm.
18. The conduit according to claim 12, wherein, in a longitudinal half cross-section plane with respect to the connector axis, the free longitudinal end comprises at least one curvilinear wall formed on the connector external surface.
19. The conduit according to claim 12, wherein the connector external surface comprises at least one hooking member radially protrudingly extending.
20. The fluid conduit according to claim 12, wherein the connector is assembled in the connection end of the piping by a translational movement along the piping axis from upstream to downstream, the free longitudinal end being radially deformed following assembling of the connector into the connection end, previously thermally expanded, the conduit having an internal surface having a substantially constant internal radius at the interface between the connector and the piping.
21. A fluid circuit comprising at least two conduits according to claim 20, the connectors of the conduits being connected by a connecting linkage.
22. A method for assembling the conduit according to claim 12, the method comprising: a step of hot preforming the connection end of the piping so as to expand it radially, a step of inserting the connecting portion of the connector into the connection end of the piping, a step of radially deforming, when cooling the connection end of the piping, the free longitudinal end so that the conduit has an internal surface having a substantially constant internal radius at the interface between the connector and the piping.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0030] The invention will be better understood upon reading the following description, given as an example, and referring to the following figures, given as non-limiting examples, in which identical references are given to similar objects.
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[0046] It should be noted that the figures set out the invention in detail to implement the invention, wherein said figures can of course be used to better define the invention if necessary.
DETAILED DESCRIPTION
[0047] The invention relates to an aircraft fluid conduit CA, the conduit CA comprising a piping 1 of thermoplastic material comprising a connection end 11 extending along a piping axis X and a connector 2 to be mounted in the connection end 11 by a translational movement along the piping axis X from upstream to downstream. Such conduits CA can be connected to form a fluid circuit, for example a waste water circuit mounted in an aircraft. Each conduit CA preferably has a circular cross-section.
[0048] As represented in [
[0049] The piping 1 is made of thermoplastic material. Preferably, the piping 1 is made of a PEEK (meaning polyetheretherketone) polymeric material, allowing the use of a semi-rigid, light and robust piping 1 (hence easier to handle and install).
[0050] In this example, the piping 1 has a thickness of less than 2 mm, so as to reduce its mass. Preferably, the thickness of the piping 1 is between 0.5 and 2 mm. The connection end 11 has an internal radius RI which depends on the dimension of the piping 1 and which is preferably between 10 and 60 mm. The internal radius R1 corresponds to the radius of the piping 1 in the rest state, that is when the piping 1 is cold and is not subjected to any force.
[0051] With reference to
[0052] The connector 2 extends along a connector axis V. As represented in [
[0053] Preferably, connector 2 is made of a thermoplastic material. Further preferably, the connector 2 is made of a PEEK polymeric material allowing the use of a semi-rigid, thus easy to handle, light and robust connector 2. The assembly of a piping 1 and a connector 2 formed from thermoplastic materials ensures optimum connection. The connector 2 is obtained by machining or molding, in particular, by injection.
[0054] With reference to
[0055] Preferably, the linking portion 22 is to be positioned facing the linking portion 22 of another connector 2 of an adjacent piping 1, with a view to connecting them to form a fluid circuit.
[0056] As represented in [
[0057] Still with reference to [
[0058] The connecting portion 21 of the connector 2 has an external radius R3 ([
[0059] The connector internal surface SI2 is to be in contact with the fluid, when the conduit CA is assembled.
[0060] With reference to [
[0061] The longitudinal wall 4 extends parallel to the connector axis V and has a length L4 of between 9 and 25 mm. The connecting portion 21 is thus long enough to hold the connector 2 in position in the connection end 11 of the piping 1.
[0062] With reference to [
[0063] Preferably, the projection of the tilted wall 5 onto the connector axis V determines a length L5 (represented in [
[0064] The external connecting surface SE2 of connector 2 is configured to be in contact with the piping internal surface SI1 of the connection end 11.
[0065] With reference to [
[0066] With reference to [
[0067] Preferably, the tilted portion 33 and the longitudinal portion 32, as well as the longitudinal portion 32 and the radial stop portion 31, are connected through a rounded chamfer (not represented) making it possible to limit wear or damage to the piping 1 when inserting the connector 2 into the connection end 11. Such rounding makes it easier to slide one piece in relation to the other.
[0068] In one preferred embodiment, with reference to [
[0069] The insertion tip 6 preferably has a rounded profile so as to limit the risk of damaging the piping 1 when inserting the connector 2. Preferably, the rounded insertion tip 6 has a radius of curvature r6 of between 0.2 and 0.4 mm. The curvilinear wall 8 forms, on the external connecting surface SE2, a toric portion, which facilitates insertion of the connector 2 into the connection end 11 of the piping 1, without damaging the piping 1. The curvilinear wall 8 preferably has a radius of curvature r8 of between 1.5 and 3 mm.
[0070] A method for assembling a piping 1 and a connector 2, according to one embodiment of the invention, will henceforth be described, with reference to [
[0071] The assembly method first comprises a step E1 of hot preforming the connection end 11 of the piping 1. For this, with reference to [
[0072] As the piping 1 is still hot, the operator then inserts, in a second insertion step E2, the linking portion 21 of the connector 2 into the connection end 11 of the piping 1 as illustrated in [
[0073] With reference to [
[0074] When cooling the connection end 11 of the first piping 1, the bevel-shaped free longitudinal end 21a is gradually deformed radially inwardly of the connector 2 as represented in
[0075] As illustrated in [
[0076] When the piping 1 is cooled, the free longitudinal end 21a of the connector 2 does not form any internal protrusion or discontinuity that may lead to the trapping of fluids. The risk of defect is dramatically reduced. By virtue of the assembly method according to the invention, the conduit CA obtained is tight and robust, even with a thin-walled PEEK polymer piping.
[0077] Assembly of a connector 2 at a connection end 11 of a piping 1 has been set forth. The assembly method can advantageously be repeated for each connection end 11 of a piping 1 in order to obtain fluid conduits CA that can be attached to the structure of an aircraft. Referring to [