This application claims priority from French Application No. 08/06526, filed Nov. 20, 2008, which is hereby incorporated herein in its entirety by reference.
The present invention provides a fluid transport device, in particular for transporting fuel in an aviation application.
Airplane wings are usually made in the form of a structure of composite material that is not electrically insulating together with stiffening elements that are electrically conductive and generally made of aluminum.
The fuel pipes situated inside airplane wings need to be capable firstly of discharging electrostatic charge, and secondly of avoiding short-circuiting the structure in the event of a lightning strike.
It is known to design tubes having a central section made of a material having high resistivity together with two end sections made of conductive material that are connected by conductive wires to conductive endpieces each of which is secured to a stiffener element.
The material constituting the central section is an epoxy resin filled with fiberglass and carbon black, thus implying relatively high weight.
An object of the present invention is thus to provide the looked-for function while reducing the weight and possibly also the cost of the tube.
To this end, the invention provides a fluid transport device for incorporating in a structure that is not electrically insulating, in particular being made of a composite and including an electrically resistive tube, with conductive endpieces including means for fastening to said structure, wherein the tube comprises:
at least one conductive element electrically connecting a conductive endpiece and an end section having a said effective resistance lying in the range 100 kΩ to 500 kΩ, said effective resistance being defined as the value of the resistance of the end section between the central section and the conductive element.
In a first variant, the device presents two end sections presenting an effective resistance lying in the range 100 kΩ to 500 kΩ and two said conductive elements each connecting one end section to the corresponding conductive endpiece.
At least one end section may include an extension of the central section, which extension is surrounded in succession by a conductive sleeve and an end coupling.
At least one conductive element may be a conductive wire or a conductive gasket.
In a first embodiment of a second variant, the device presents two end sections presenting respective effective resistances lying in the range 100 kΩ to 500 kΩ and at least one said conductive element disposed on a single end section and connecting it to the corresponding conductive endpiece.
In a second embodiment of the second variant, the device presents a first end section presenting resistance lying in the range 100 kΩ to 500 kΩ and a second end section presenting effective resistance less than said value, and at least one said conductive element disposed on the second end section and connecting it to the corresponding conductive endpiece.
The central section may be made of a thermoplastic, thermosetting, or elastomer material with conductive fillers, which act both to provide mechanical reinforcement and to adjust conductivity.
At least one end section may be made of a material filled with fiberglass and conductive particles.
At least one end coupling may be made of a thermoplastic or thermosetting material with optional conductive fillers.
The invention can be better understood on reading the following description with reference to the drawings, in which:
a and 1b are diagrams illustrating an airplane wing structure, and
c is an equivalent electrical circuit diagram for a fuel pipe;
a and 3b show two embodiments of a first variant of the invention;
a is a diagrammatic section view of a portion of an airplane wing 1 that comprises a structure 2 made of composite material presenting resistance per unit length of 103 ohms per meter (Ω/m), and stiffener elements 3 of conductive material such as aluminum. One or more tubes 5 for conveying fuel (
An electrical circuit diagram is given in
The tube 5 for performing this function needs to have resistance that is much higher than that value, e.g. R2=105 Ω/m.
The tube shown in
The first variant of the invention is shown in
For example, the end sections 62 and 63 are made of a material, e.g. a polyamide, that is filled with fiberglass, and with conductive fillers, e.g. carbon black.
b shows another embodiment that differs from
Because the central segment 61 has low resistance, it is possible to decrease its weight, and there is no need to add fiberglass (carbon fibers suffice), thereby enabling its thickness to be reduced while still providing the required mechanical properties, thus achieving a saving in weight, e.g. of 20% to 30%. Because the end segments 62 and 63 are not made of metal, a weight saving is obtained that is generally greater than 15%.
The central segment 61 may comprise long carbon fibers in a thermoplastic material, carbon fibers in a thermosetting material, e.g. an epoxy resin, or indeed a filled thermoplastic material or a filled conductive rubber having as its conductive filler carbon fibers that are short (length<1 millimeter (mm)), for example.
The fact that the central segment 61 presents lower resistance than in the prior art is favorable to evacuating charge, whereas in the event of a lightning strike, since the tube 6 presents electrical resistance significantly higher than that of the structure 2, it avoids establishing a short circuit.
In the variant of
Under such circumstances, it is possible for the end segment 63 to be made of a material that is more conductive than that of the other end segment 61, e.g. to be made of the same material as the central segment 62.
In this configuration, electrostatic charge is evacuated via the electrical connection 14 and/or 14′ and insulation against lightning is provided by the fact that the impedance between the couplings 11 and 12 is infinite since the gasket 15 is electrically insulating.
Contact is made by the wire 13, 14 (or by the conductive gasket) via the end coupling 64′ or 65′. When the coupling is resistive, the value of its resistance needs to be taken into account when calculating the effective resistance.
Number | Date | Country | Kind |
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08 06526 | Nov 2008 | FR | national |
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10 2005 013981 | Sep 2006 | DE |
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2 211 266 | Jun 1989 | GB |
Entry |
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International Search Report from French Application No. 08 06526, filed Nov. 20, 2008. |
Number | Date | Country | |
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20100122749 A1 | May 2010 | US |