The present invention relates to a double wall duct system, in particular to be used in the aeronautical field, and to a method of manufacturing such a double wall duct system.
Double wall ducts are typically used in the aeronautical field in areas where a potential leakage may jeopardize the continuity of a safe flight, therefore causing possible injuries to the related personnel due to vapors hazards.
In the case of double wall ducts used in the aeronautical field, comprising an internal duct and an external duct, the internal duct is used for bearing fuel pressures, while the external duct is used to convey potential leakages to a specific drain system outside the risk area, this constituting a situation of a special risk in the aeronautical field.
There exist known methods of fabricating double wall ducts, like for example the one described in document U.S. Pat. No. 4,332,073, where a method for manufacturing a double wall duct made of composite material is disclosed. The outer duct is expanded by heating, whereas the inner duct is contracted by cooling, therefore being the two ducts introduced one inside the other. After this, the clearance between the two ducts disappears and they are brought to the same dimension. No bending in the duct is disclosed in this document, and no clearance is kept between the two ducts. The problem raised by the method of this document is that it is expensive and not valid for fabricating bends. Moreover, as there is no clearance kept between the two ducts, potential leakages are therefore not controlled.
Document U.S. Pat. No. 5,189,790 discloses a method of manufacturing a double walled duct elbow by the use of seal plugs to be used in car exhaust gas manifolds. The main problem raised in this method is that its fabricating costs are quite high, as the diameter of both ducts has to be the same and this diameter must also be of a very specific dimension. Moreover, the material of the ducts is very expensive, as the fabricating method comprises the step of blowing by pressure, the material needing therefore to bear such high pressures. In the junctions, the double wall duct of this document does not have any clearance between the two ducts: the double wall duct is then not valid for controlling or detecting potential leakages.
Document U.S. Pat. No. 5,054,185 discloses a method for fabricating a double wall duct comprising an inner and an outer duct, also comprising an intermediate layer with a material for attenuating vibrations, to be particularly used in automobile exhaust systems. The material for attenuating vibrations of this invention means weight and is therefore something to be considered as highly negative in the aeronautical field. Also, the method of this invention does not maintain a clearance between the ducts, necessary for the detection and control of leakages. The problem solved by this invention is that of noise in a double wall duct. This invention does not solve, on the other hand, the problem of structural integrity in double wall ducts caused by vibrations.
Document U.S. Pat. No. 3,201,861 discloses a method for forming a tubular double wall exhaust duct element, comprising an outer duct element and an inner duct element comprising orifices spaced along its length, for acoustic reasons, such that there exists a gap between the outer and the inner duct, all along the length of the duct except at the ends. These orifices would produce uncontrolled leakages when used for conveying fluids; moreover, the costs of this method are high.
Document U.S. Pat. No. 5,497,809, upon which the preamble of claim 1 is based, discloses a coaxial tubing system comprising bending sleeves of an insoluble, compression resistant material with cold flow characteristics, longitudinal fluid passageways being provided between the tubes. Conductive spacers are also provided for maintaining annular tube spacing, particularly at tube ends. The main problem of this invention is that the compression resistant material increases the system weight, which is of particular relevance in the aeronautical field.
The main problem and difficulty when using the double wall duct manufacturing processes as described above comes where low weight and small area is available to route such ducting systems, as it happens when used in the aeronautical field, therefore being these processes non-viable.
The present invention is oriented to the solution of these drawbacks.
The invention is intended to provide a double wall duct system and a method for such a double wall duct system manufacturing, the double wall duct system preferably been made of a metallic material and comprising an external duct used to convey potential leakages and an internal duct used for bearing fuel pressures. The method according to the invention comprises bending both the internal and the external ducts together, and welding afterwards said internal and external duct to a fitting devoted to support the double wall duct system and/or to connect said double wall duct system to other similar duct systems.
The objective of the present invention is therefore to provide a double wall duct system, particularly metallic, to be used preferably in those areas of an aircraft where special precautions are needed (fuselage, areas adjacent to fire zones, etc.) and to provide a method for manufacturing such double wall duct system.
The manufacturing method of the present invention allows bending the inner duct and the outer duct of a double wall duct together, therefore eliminating the need for additional outer shell welding and keeping a clearance or gap in between the inner duct and the outer duct to avoid fretting that may cause non-detectable damages.
The manufacturing method of the invention comprises the following steps:
Once the bending procedure as described above is finished, the double wall duct system is then welded to a fitting devoted to its support by welding the inner duct and then the outer duct, using a bushing according to the invention and designed to fit the double wall duct system to the required fitting in particular, this bushing having previously been inserted surrounding the external duct of the double wall duct system. The bushing can either be straight or conic, depending on the fitting size to which the double wall duct system is to be connected.
Other features and advantages of the present invention will be disclosed in the following detailed description of an illustrative embodiment of its object in relation to the attached figures.
The features, objects and advantages of the invention will become apparent by reading this description in conjunction with the accompanying drawings, in which:
a, 3b and 3c show details of the fittings to which the double wall duct system according to the invention is connected,
a, 4b and 4c show details of sliding bushings used for the welding procedure of a double wall duct system according to the invention,
a, 5b and 5c show details of the assembly of both inner and outer ducts together with a conical stopper for the manufacturing of a double wall duct system according to the invention.
a, 8b and 8c show details of the steps of the welding operation for a double wall duct system according to the invention.
a, 9b and 9c show details of the steps of the welding operation at the other end of the assembly of a double wall duct system according to the invention.
The invention is therefore intended to provide a double wall duct system 1, preferably being made of a metallic material, and a method for such a double wall duct system 1 manufacturing. The double wall duct system 1 comprises an external duct 2, used to convey potential leakages, and an internal duct 3, used for bearing fuel pressures. It is to be noted that these two ducts, 2 and 3, are of standard commercial dimensions: this represents another advantage of the invention, as no additional cost are to be added because of ducts of special diameters. The double wall duct system of the invention and its method of manufacturing keeps a clearance between the two ducts, 2 and 3, therefore being the manufacturing costs maintained. The method according to the invention comprises bending both the internal duct 3 and the external duct 2 together, and welding afterwards said internal 3 and external duct 2 to a fitting 6, 7 devoted to support the double wall duct system 1 and/or to connect said double wall duct system 1 to other duct systems that can also be similar to system 1. As schematically illustrated in
The inner duct 3 and the outer duct 2 conforming the double wall duct system 1 are preferably made of a metallic material, such as Stainless Steel, preferably AISI 321, although the invention is also applicable to a variety of metallic materials.
The manufacturing method of the present invention allows bending the inner duct 3 and the outer duct 2 of a double wall duct system 1 together, therefore eliminating the need for additional outer shell welding and keeping a clearance or gap 8 in between the inner duct 3 and the outer duct 2 to avoid fretting that may cause non-detectable damages.
The process for the manufacturing of a metallic double wall duct system 1 of
The manufacturing of the machined fittings, 6 and 7, is performed following a standard known procedure. The manufacturing of the sliding bushings 4 and 5, which are preferably made of a metal which is compatible as to welding with the double wall duct system 1 and with the fittings 6 and 7, is also performed following a standard known procedure. The bushings 4 and 5 can either be conical, straight or of any appropriate shape to fit the system 1 to the other systems.
Both fittings, 6 and 7, are machined preferably from steel material, for example of the type CRES 321. The bushings 4 and 5 are also preferably made of steel material of the type CRES 321.
The welding operation for a double wall duct system 1 comprises, as can be seen in
The welding operation at the other end of the double wall duct system 1 comprises, as can be seen in
The method according to the invention comprises welding first the inner duct 3, then sliding the bushing 4 or 5, which has previously been introduced in the double wall duct system 1, and one the bushing is displaced, it is welded in two parts to the system 1.
One of the main advantages of the present invention is to provide a double wall duct system 1 connected to other systems by fittings 6 and 7 with at least one bending, such that the system 1 is formed in a single process, and is not formed by different parts, each one of the parts being formed in different processes, therefore having the advantages of maintaining a low weight where a small area is available to route the ducting systems, as it happens in the aeronautical field of the present invention.
The bushings, 6 or 7, can also comprise a drain port, as the one showed in bushing 4 of
In
The bushings 4, 5 provide a closed structural integrity of the system 1, therefore allowing a potential leakage in the double wall system 1 to be detected and evacuated in a controlled manner.
Although the present invention has been fully described in connection with preferred embodiments, it is evident that modifications may be introduced within the scope thereof, not considering this as limited by these embodiments, but by the contents of the following claims.
Number | Date | Country | Kind |
---|---|---|---|
200801199 | Apr 2008 | ES | national |