the loom m shown in fig1 is equipped with a jacquard mechanism 2 which controls several harness strings 4 the lower end of which is associated with several cords 6 . the lower end 6 a of each cord 6 is connected to the upper end 8 a of a heddle 8 , each heddle 8 being provided with an eyelet 9 for passage of a warp yarn 10 and subject to the action of a restoring spring 12 fixed to the frame 14 of the loom through a stem 16 . the heddle 8 is formed from a threadlike element 81 which initially has the shape of a stainless steel wire with circular cross section . this thread is crushed to have a flattened transverse section . in its central part , the element 81 is separated into two branches 82 and 83 between which an opening 84 is defined for receiving the eyelet 9 . the eyelet 9 is obtained by cutting of a strip of metal , preferably a strip of carbon steel . it defines an orifice 91 for passage of the warp yarn 10 . the central axis of the orifice 91 , is referenced x 91 . this axis is perpendicular to the principal faces 92 and 93 of the eyelet 9 , that is its faces with the largest areas . the eyelet 9 has an oblong shape and its outer edge , which is overall oval or in the form of a flattened ellipse , is referenced 94 . the edge 94 is equipped with eight tabs 95 of which four , bearing the reference 95 a , have one of their sides flush with the surface 92 whereas the four other tabs , bearing the reference 95 b , have one of their sides flush with the surface 93 . the tabs 95 a and 95 b project relative to the edge 94 and are laid out in pairs along the edge 94 , each pair including a tab 95 a and a tab 95 b , these tabs being laterally offset from each other along the edge 94 . the median plane of the eyelet 9 , i . e a plane parallel to the faces 92 and 93 and equidistant from them , is denoted by p 9 . the tabs 95 a and 95 b are distributed on both sides of this plane . in particular , the tabs 95 a and 95 b of a single pair of tabs are offset on both sides of this plane along a direction d 9 parallel to the axis x 91 . looking at the section of the eyelet 9 shown in fig5 , it could be considered that the tabs 95 a and 95 b are placed in staggered rows on both sides of the plane p 9 . the tabs 95 a and 95 b from a single pair are offset along the edge 94 by a non - zero distance d , and parallel to the direction d 9 , by a distance d ′, taken between the centres of the tabs 95 a and 95 b , which is also non - zero . the succession of two tabs 95 a and 95 b from a single pair forms a volume v , shown in grey in fig6 with a width d ′, in which the edge 85 of the opening 84 can be partially introduced in order to firmly retain the eyelet 9 in position in this opening . in order to be able to be introduced in this grey volume v , the edge 85 is thinned as shown on fig7 to 10 . when the element 81 is shaped to make the heddle 8 , it is die - stamped along a length corresponding to the largest dimension of the opening 84 to form , from each of its largest dimensions or principal faces 86 and 87 , two housings 86 a and 87 a which each extend on two depths p 1 and p 2 where the larger depth p 2 corresponds to the central zone of each of the housings 86 a and 87 a . once the housings 86 a and 87 a have been formed by die - stamping of the element 81 , a slit 88 is created in their bottom part , as shown in fig9 . this slit joins the deepest parts of the housings 86 a and 87 a . by the formation of this slit 88 , branches 82 and 83 are created which can then be separated from each other , in the direction of the arrows f 2 in fig9 and 10 , to reach the position of fig1 where the branches 82 and 83 define between them the opening 84 with transverse dimensions greater than the dimensions of the eyelet 9 in the plane visible on fig4 . at the end of this operation , the edge 85 forms , on its entire length , a sized nose 85 a on both sides of which are arranged two shoulders 85 b of depth p i . the nose 85 a has a width l 85 measured parallel to the axis x 91 , less than the thickness e 81 of the element 81 and than the distance d ′. as shown in fig1 , it is then possible to place the eyelet 9 in the opening . 84 after having pulled away the branches 82 and 83 by elastic deformation , and then letting them come back towards each other in the direction of the arrows f 3 in this figure , which comes back to insert locally , meaning to engage , the nose 85 a of the edge 85 in the volumes v defined by the two tabs 95 a and 95 b of each pair of tabs . the eyelet 9 is then held , firmly and without play by the branches 82 and 83 . to ensure the durability of the attachment and fill the holes between the eyelet 9 and the element 81 , adhesive is applied in the holes 84 a which remain on both sides of the eyelet 9 . by capillarity the adhesive spreads in the area of at least part of the interface between the edge 85 and the eyelet 9 . this adhesive can be of any known type and , in particular , a single - component epoxy adhesive cured by ultraviolet radiation , or an anaerobic adhesive cured by ultraviolet radiation . the thickness of each of the tabs 95 is referenced e 95 . this thickness is slightly less than the depth p 1 of the housings 86 a and 87 a . further , the total thickness e 9 of the eyelet 9 is chosen roughly equal to the thickness e 81 . thus , when the eyelet 9 is pinched and bonded in the opening 84 as shown in fig3 , its faces 92 and 93 can be flush with the faces 86 and 87 of the element 81 , since the tabs 95 are received in the shoulders 85 b of both sides of the nose 85 a . the positioning of the tabs 95 a and 95 b , which are offset from each other along the edge 94 , makes it possible to make these tabs by die - stamping of the steel strip out of which the eyelet 9 is cut . as a variant , the eyelet can be made by cold forging . the fact of using die - stamping or forging for creating the tabs 95 avoids having to use machining operations which would be very costly and delicate to implement considering the size of the eyelet 9 whose length in practice is less than 20 mm , preferably less than 10 mm . in consideration of the manufacture method for the eyelets 9 by cutting , die - stamping and / or forging , it is not necessary to make use of a circular slug of the type of that used in fr - a - 2 267 403 or ep - a - 1 015 675 , which makes it possible to adapt the shape of the edge 94 to the final shape of the opening 84 . so , the holes 84 a that may need to be filled with adhesive can be of reduced size compared to the total surface of the opening 84 . the manufacture method for the eyelets 9 enables very high production rates because the various operations used can be done on a single machine with several work positions , and the shaping tools all have displacements perpendicular to the plane p 9 . the fact that the eyelet is bonded to the element 81 and not welded onto it allows this element 81 to be made of stainless steel . the use of a stainless steel element 81 makes it possible to dispense with conventional nickel plating operations on non - stainless steel elements , while these nickel plating operations are likely to generate the appearance of burrs or “ scratchings ” which can damage or cut the warp yarn . in the second embodiment of the invention shown in fig1 , the elements analogous to those from the first embodiment have identical references . this embodiment shows an inverted or “ mirror ” solution relative to the first embodiment in the sense that the tabs 95 a and 95 b are distributed on the edge 85 of the opening 84 arranged in the threadlike element 81 of the heddle 8 , whereas the outer edge 94 of the eyelet 9 is thinned and has a nose 94 a thinner than the eyelet and intended to be inserted in the volume defined by the two adjacent tabs 95 a and 95 b of a single pair of tabs 95 . as in the first embodiment , the tabs 95 a and 95 b are staggered , being offset from each other both parallel to the edge 85 , as shown by the distance d in fig1 , and perpendicularly to it along the direction of the axis x 91 of the orifice 91 defined by the eyelet 9 . the tabs 95 a and 95 b are flush to the lateral faces of the threadlike element 81 . as in the first embodiment , the eyelet 9 can be immobilized by a clamping force f 3 due to the branches 82 and 83 of the element 81 and by being bonded , in order to obtain additional anchoring . as shown in fig1 and 13 where the elements analogous to those from the first embodiment have the same references , the edge 94 of the eyelet 9 can be provided with two tabs 95 a and 95 b which form a pair of tabs 95 which are offset as in the first embodiment . the tab 95 a is flush with a principal face 92 of the eyelet 9 , whereas the tab 95 b is flush with the opposite principal face 93 . similarly , the edge 85 of the branch 82 of the threadlike element 81 is provided with two projecting tabs 95 ′, specifically one tab 95 ′ a flush with the principal face 86 of the branch 82 and one tab 95 ′ b flush with the opposite face 87 of this branch . the tabs 95 ′ are offset from each other along the edge 85 by a distance d identical to the offset distance d of the tabs 95 relative to each other along the edge 94 . the tabs 95 ′ are also offset from each other perpendicularly to the faces 86 and 87 by a distance d ′ between their respective centres , just like the tabs 95 are offset perpendicularly to the faces 92 and 93 by the same distance d ′. the direction of offset of the tabs 95 ′ perpendicularly to the faces 86 and 87 is the inverse of that of the tabs 95 . it is thereby possible during the placement of the eyelet 9 in the opening 84 to bring the tabs 95 a and 95 ′ b into a position overlapping one another whereas the tabs 95 ′ a and 95 b are brought into a position overlapping one another , as shown respectively in fig1 a and 12b . in the portions of the edges 94 and 85 free of tabs , these edges are straight and perpendicular to the principal faces 86 and 87 , and 92 and 93 of the elements 9 and 81 , as shown in fig1 c . as the fig1 a and 14b show , the tabs 95 a , 95 b , 95 ′ a and 95 ′ b can be chamfered , that is having a surface inclined at about 45 ° to the principal faces 86 , 87 , 92 and 93 of the elements 81 and 9 , while being offset perpendicularly to these faces by a distance d ′, along the edges 85 and 94 . as a variant , in the four embodiments described , as the blocking of the eyelet 9 in the opening 84 , obtained through the elasticity of the branches 82 and 83 , is very effective , the bonding of the eyelet in this opening can be eliminated . the invention was shown in the first two embodiments with an eyelet and an opening whose edge 94 or 85 is equipped with eight tabs 95 . in practice , the number of tabs 95 results from a design choice by a specialist who may decide to use only two of these tabs or an arbitrary number of them . this number can be less or more than eight . when more than two tabs are used , they are advantageously distributed along the length of the edge 94 or 85 , preferably in pairs . the invention was shown in its implementation for the manufacture of a heddle for a jacquard type loom . it also applies to the manufacture of a heddle intended to be mounted on a loom frame , this frame being driven by a weave mechanism , for example a dobby or basic weave mechanism .