This application is a § 371 application from PCT/EP2016/055742 filed Mar. 16, 2016, which claims priority from French Patent Application No. 15 52080 filed Mar. 16, 2015, each of which is incorporated herein by reference in its entirety.
The invention relates to a method and device for fireproofing a part in composite material. The invention is more particularly but not exclusively intended for the field of aeronautics, for fireproofing a structural part made of composite material with fiber reinforcement in a thermoplastic or thermosetting polymer matrix.
Structural aircraft parts located in areas that are potentially exposed to flames need to be fire resistant under a regulatory obligation. The standards require minimum resistance for 15 minutes from a part exposed to a flame at 1100° C. combined with vertical vibration with 0.4 mm amplitude and 50 Hz frequency. “Fire resistance” qualification is defined by the achievement of different performance levels, which correspond to standards or the internal requirements of the aircraft manufacturer, namely:
To that end, different protection techniques are used. The document EP 0167533 provides a view of the protection techniques of the prior art.
These different protection techniques of the prior art have the drawbacks of making a significant addition of mass, as the specific gravity of the protective means is greater than that of the structural part, and of not following the shape of the part. Further, the coverings used to protect the parts according to the methods of the prior art have the drawback of being sensitive to perforation and tearing, and such degradation of said covering leads to a loss of efficiency of the covering in respect of fire protection. In order to remedy that drawback, a solution of the prior art consists in protecting the thermal insulation with metal shells. Beyond the significant addition of mass resulting from this solution, the metal shell tends to deform and dilate thermally in a different way from the structure, which makes it difficult to fix it to said structure and results in significant mechanical constraints in the structure when the metal shell is exposed to a flame, or even during temperature variations that occur in service. 0.08 mm thick sheets of stainless steel are commonly used for that purpose. The mass added by these sheets is about 1.270 kg*m−2, while the fine thickness of said sheets only offers moderate mechanical protection to the underlying protective covering and is sensitive to perforation. Thus, when the underlying protective covering has a surface density of about 1 kg*m−2, the mass added by that protective solution of the prior art is about 2.270 kg*m−2.
The invention aims to remedy the drawbacks of the prior art and therefore relates to a device for fireproofing a section of a structural part made of composite material, characterized in that it comprises:
Thus, the skin is suitable to be formed using conventional techniques for working with composite materials with polymer matrices, and can be adapted precisely to the shape of the section of the part to protect. It protects the thermal insulation, that is to say the needled felt, from mechanical attacks and the addition of mass remains moderate. Said skin is sufficiently flexible in relation to the rigidity of the structure to enable it to follow the deformations of the structure and its thermal dilatation is of the same amplitude as that of the structure protected in that way.
The invention can be implemented advantageously in the embodiments described below which may be considered individually or in any technically operative combination.
Advantageously, the mineral felt is about 10 mm thick. That thickness, combined with the protection granted by the composite skin, is sufficient to offer thermal protection to the structural part with a moderate addition of mass.
In one embodiment, the fastening means comprise rivets.
In another embodiment, compatible with the previous one, the fastening means comprise gluing between the skin and the structural part.
Advantageously, the fastening means combine gluing with glue that withstands temperature above or equal to 200° C. and riveting. Thus, gluing offers sealed protection to the structural part at the degassing temperatures, and the rivets hold the thermal protection on the structure at higher temperatures.
Advantageously, the skin comprises a ply made of glass fabric on its inner surface. Said glass fabric protects the felt from the flame.
The invention also relates to a method for protecting a structural part using a device according to the invention, which method comprises the steps of:
Thus, application by laying up, curing and consolidating the skin makes it possible to adapt the shape of the skin to the part to protect.
Advantageously, step (iv) of fixing the skin of the method according to the invention comprises a riveting operation and the method comprises a step of:
Thus, the rivet heads are protected from the temperature and the rivets do not transmit the flame inside the skin.
The invention is described below in its preferred embodiments, which are not imitative in any way, and by reference to
In
Thermal insulation (120) is placed between the inner surface of the skin (110) and the part (100). In an exemplary embodiment, said insulation is made of needled quartz fibers with a thickness of 10 mm. In this configuration, the surface density of the thermal insulation is about 1 kg*m−2.
In an exemplary embodiment, the skin is attached to the part by gluing, using silicone glue (130) that resists temperature of at least 200° C., and using rivets (140). To that end, the skin (110) comprises fastening portions (111) provided in the laying up tool. The flexibility of the skin enables it to adapt to the shape of the part and ensures close contact between said part and the assembly portions (111) so that the volume enclosed by the skin is sealed. The rivet heads are protected by thermal protection covering (150) of the ablative or intumescent type, for example ablative covering distributed under the trademark FASTBLOCK® 800 by Esterline. The combination of gluing and riveting makes it possible to secure the skin as close to the contour of the part as possible, including in the connecting radius zones, where rivets cannot be installed. In this exemplary embodiment, the overall mass added is 1.7 kg*m−2, that is to say 25% less than the solution of the prior art using metal protective sheets.
In
Thus, the device according to the invention provides thermal protection compatible with applicable aerospace standards, with an added mass that is 25% less than the known solutions of the prior art.
The device and method according to the invention are more particularly advantageous for making thermal protection for a structural part made of composite material with a polymer matrix. However, the device and method according to the invention are also adapted for making thermal protection for a structural part made of other material.
Number | Date | Country | Kind |
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15 52080 | Mar 2015 | FR | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2016/055742 | 3/16/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2016/146716 | 9/22/2016 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4767656 | Chee | Aug 1988 | A |
4952440 | Sanmartin | Aug 1990 | A |
20120227370 | Mickelsen | Sep 2012 | A1 |
Number | Date | Country |
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0167533 | Feb 1990 | EP |
2 640 738 | Jun 1990 | FR |
2 690 106 | Oct 1993 | FR |
Number | Date | Country | |
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20180043983 A1 | Feb 2018 | US |