the present invention concerns a method for producing a part comprising a hollow body , such as a rod , from a composite material using preforms . in the case in point , the present invention is illustrated by a part made from two dry preforms 11 , 12 cut out from a pattern for producing said part and initially prepared flat . each preform therefore has an adapted shape , a specific geometry , a number of fibrous layers able to fill the final volume to be molded after forming , etc . . . each preform 11 , 12 has at least one layer 111 , 121 of transverse fibers extending from one lateral end 112 , 113 , 122 , 123 to the other with a sufficient length . of course , it may be considered to prepare some or all of the preforms 11 , 12 by light forming . moreover , the method according to the invention is not limited to a given number of preforms . although the method is intended to facilitate the use of dry preforms , it is , however , possible to consider using some preimpregnated preforms . a supporting element 1 is diagrammatically illustrated in fig1 . it will be noted that the supporting element 1 is made up of several elements , shown in fig1 in four pieces 21 , 22 , 23 , and 24 , the assembly of which constitutes a shape close to the molding geometry , and at least one element of which is able to move , in order to be able to vary the winding perimeter and contribute to later compacting operations , and also to be able to remove the supporting element after the forming operations . an inner mechanical device ( not shown ) makes it possible to slightly expand or contract the pieces 21 , 22 , 23 , 24 to slightly increase or reduce the perimeter of the supporting element 1 . the first step of the method according to the invention is diagrammatically illustrated in fig2 and is composed of winding , on the supporting element 1 , the first preform 11 , the winding and forming of the preform 11 being controlled by the movements of rigid outer shapes ( not shown ), stretched flexible shapes ( not shown ), or by traction on the longest transverse fibers 111 , 121 , or by a combination of these forms , or by a succession of steps ending with at least one of the above operations , and that can be preceded by a forming operation between the supporting element 1 or another supporting element with a close shape and flexible vessel in vacuum , or pressed rigid counterpart . the ends 112 , 113 , 122 , 123 of the longest and continuous transverse fibers 111 , 121 from one lateral edge to the other of the preform 11 , 12 are then flanged on the supporting element 1 by one or several retention means . after this , the forming system can be dismissed . it will be noted that the preform 11 on the supporting element 1 has beveled ends 112 , 113 . these ends 112 , 113 can result from the winding of the preform 11 . in fact , if the inner and outer fibers 111 have substantially the same length , the corresponding angular section will be more significant for the inner fibers 111 , wound around a smaller radius . beveled ends 112 , 113 result therefrom . however , this normal formation of beveled ends 112 , 113 rarely yields long enough ends . it is therefore possible to provide preforms 11 , 12 having flat , beveled edges , this bevel length being accentuated by the winding . these beveled ends 112 , 113 are intended to form a coupling edge intended to be covered by a corresponding coupling edge of the second preform 12 , formed by a beveled end 122 , 123 thereof . once the first preform 11 is wound around the supporting element 1 , it is kept in place using retention means , by flanging , or even tensioning of circumferential fibers . various retention means can be considered . in the case in point , fig3 presents a retention means comprising positioning , on the first preform , a fibrous membrane 201 gripping it . the fibrous membrane 201 has lateral ends 201 a , 201 b that are then fastened in the supporting element 1 using any adapted means , preferably by clipping inside a slot formed in the supporting element 1 . the fibers making up the retention ends 201 a , 201 b can , in another alternative , be circumferential fibers that are part of the preform 11 whereof the ends will be retained in the device . the fact that the circumferential fibers , of the preform 11 or the fibrous membrane 201 , are flanged relative to the supporting element makes it possible for any preform portion defined in said fibers to be contained in a maximum perimeter and thus to keep a compacting level between the layers close to that generated by the forming system , making it possible to manage the thickness by layer in the dry state . the clipping may be done between two pieces 21 , 22 , 23 , 24 of the supporting element 1 , which makes it possible to open the clip by simple expansion of the pieces of the supporting element 1 . thus with the first preform 11 retained and stretched , the second preform 12 is wound on the supporting element 1 using the same forming principles , possibly using the same forming devices used for the first preform 11 if the geometry allows it . this second preform 12 covers the rest of the supporting element 1 and has beveled ends 122 , 123 covering the beveled ends 112 , 113 of the first preform 11 at a coupling area . the ends 122 , 123 of the second preform 12 are then also flanged and kept in place using the retention device , in particular by clipping . as for the first preform 11 , fig5 shows the retention of the second preform using a second fibrous membrane 202 , which is stretched and clipped in order to keep the outer perimeter described by the preform 12 . the retention means are adjusted and the preforms 11 , 12 stretched so as to obtain an outer perimeter close to the final molding outer perimeter in order to obtain correct alignments of the circumferential fibers during molding . the fibrous membranes 201 , 202 will be made up of fibers of the same nature or of different natures from the fibers of the preforms 11 , 12 . as for the first preform 11 , the ends 202 a , 202 b , 202 a and 202 b can be formed by circumferential fiber margins of the second preform 12 . fig6 then shows a compacting step of the preforms 11 , 12 . through expansion or separation devices of the pieces 21 , 22 , 23 , 24 of the supporting element 1 , it is then possible to increase the perimeter described by the inner transverse fibers , obtaining a compacting of the coupling areas at the same time , which contributes to aligning the circumferential fibers of inner layers . it is preferable to keep the outer forming devices in place around the assembly , to confine the outer perimeter by limiting the tension on the retention means of the second preform 12 , however the flanging systems of the only preform 11 will have to be released during this operation to allow the expansion sliding of the inner perimeter . as for the first preform 11 , the ends 202 a , 202 b can be made up of margins of circumferential fibers of the second preform 12 . as shown in fig7 , the preforms 11 , 12 are then made integral at their coupling areas in a sewing step . this operation can be done using known methods of sewing ( stitching , blind stitching ), tufting , or z - pinning . preferably , a fiber 300 will be chosen of the same nature as the fibers making up the preforms 11 , 12 but with a low enough count to be able to stitch it . in the case of z - pinning , the fiber 300 may be pultruded , i . e . coated with resin and polymerized , before insertion into the assembly of preforms 11 - 12 . a stitching pitch will be chosen procuring sufficient cohesion for the assembly while preserving a slight possibility of sliding of the layers in relation to each other . it will be noted that the preforms 11 , 12 are generally formed by fibers woven in three dimensions . in the case where a preform 11 , 12 is made having beveled ends , these areas generally cannot be made in three dimensions and rather include a superposition of layers woven in two dimensions . the sewing step makes it possible to restore this three - dimensional weaving locally , which provides better strength and resistance of the assembly . for the sewing operation , the outer forming devices can be removed if the flanging systems of the circumferential fibers 202 are sufficient , in a contrary case , i . e . if the mastery of the outer perimeter requires the maintenance of outer compacting shapes , these outer shapes will be made in pieces making it possible to expose , over time , an access window for accessing the outer surface to perform the insertion of the coupling fibers . the outer retention means as well as the forming device can then be disassembled after the sewing operation or during it when the sewing already allows sufficient resistance . the non - connected ends of the coupling areas , ends that were then clipped , can be cut or left free . the supporting element 1 is retracted or disassembled into pieces 21 , 22 , 23 , 24 ( of course , the number of pieces making up the supporting element 1 is not limited ) to remove the complete preform thus formed . it will also be noted that , for better effectiveness , the sewing can be done on the entire thickness of the complete preform . the supporting element 1 will then have martyr areas located at coupling areas for the passage emerging from the sewing needle . this area may be either made of a soft penetrable material ( cellular foam , for example ) or a dry fibrous structure of substantially the same type as the preform , or a perforated structure , such as a honeycomb substructure , or a slotted tool , if it is possible to precisely master the through positions of the needles . in the case where more than two preforms are used , it may of course be possible to carry out sewing steps according to the described method so as to come back to cases of two preforms . it will also be noted that it is not mandatory for both ends of each preform to have the same covering order with the other preforms . in the illustrated case , it is therefore not required that the ends 112 and 113 both be covered by the ends 122 and 123 . it is of course completely possible for the end 112 to be covered by the end 122 , but for the end 113 to cover the end 123 , or vice versa . the described method makes it possible to achieve , after the compacting and sewing step , fiber volume rates very close to those that will be obtained during molding and an overall cohesion of the orientations of the fibers facilitating the manipulation of the complete preform . the following step therefore comprises an rtm / lri molding step according to a known method . to do this , a mold core is introduced inside the preform in one or several pieces depending on the geometry of the part . also known are cores in vessel form , inflated inside the preform . however , the core will generally be made in several elements having slopes such that they produce radial relative movements when they are put in contact with the complete preform so as to keep the fibers suitably aligned and thus contribute to aligning the circumferential fibers . the core and preform assembly is inserted into the mold device generally comprising at least two matrices . a final compacting is done by closing the outer matrices . it is also possible to add a final expansion of the core thereto . the consolidation of the fibrous structure is ensured by injecting a liquid resin according to an rtm / lri method as well as through a polymerization of said resin following a suitable mechanical - thermal cycle . of course , the invention is not limited only to the embodiments of this rod described above as an example , but on the contrary encompasses all alternatives of structures comprising hollow bodies .