Mechanical system for a turbine engine, turbine engine, and method for attaching a mechanical system within a turbine engine

Abstract

A mechanical system for a turbomachine includes a turbomachine part to be attached and a plurality of threaded attachment elements mounted on the turbomachine part in sequence along a line. The attachment elements fix the turbomachine part to the turbomachine. At least some of the attachment elements are arranged to be prevented from rotating by mutual cooperation about their corresponding thread axes, by a rotation prevention system provided on each of these attachment elements called self-locking elements. The self-locked elements cooperate in pairs, each pair including two directly consecutive self-locked elements along the line. At least one of the pairs has a distance between the thread axes of its two self-locked elements less than the distance between one of these two thread axes and the axis of either of the two attachment elements arranged along the line on each side of the at least one of the pairs.

Claims

1. A mechanical system for a turbomachine, comprising: a turbomachine part to be attached; and a plurality of threaded attachment elements mounted on the turbomachine part to be attached in sequence along a line, wherein the threaded attachment elements are adapted to fix the turbomachine part to be attached in the turbomachine and each of the threaded attachment elements having a thread axis, all of the threaded attachment elements, called self-locking threaded attachment elements, are arranged so as to be prevented from rotating by mutual cooperation about corresponding thread axes thereof, by means of a rotation prevention system provided on each of the self-locking threaded attachment elements, the self-locking threaded attachment elements cooperate in pairs, each pair including two directly consecutive self-locking threaded attachment elements along the line, and for each of the pairs, a distance between the thread axes of the two self-locking threaded attachment elements of the pair is less than distances between the thread axis of each of the two self-locking threaded attachment elements of the pair and the thread axes of the two attachment elements directly consecutive to the pair along the line, the distance between the thread axes of the two self-locking threaded attachment elements in a pair is approximately the same for each pair and is equal to a distance d1, and the distance between the thread axes of two consecutive self-locking threaded attachment elements in different pairs being equal to a distance d2 greater than the distance d1.

2. The mechanical system according to claim 1, wherein each self-locking threaded attachment element comprises a locking member forming locking means, the locking member of one of the self-locking threaded attachment element in a pair being complementary to the locking member of the other self-locking threaded attachment element in the same pair, the locking member also acting as a support means to limit translation displacements of the corresponding self-locking threaded attachment element along the thread axis of the self-locking threaded attachment element on the turbomachine part to be fixed.

3. The mechanical system according to claim 2, wherein each locking member has a stop portion bearing on a stop portion complementary to the locking member corresponding to the other self-locking threaded attachment element in the pair, the stop portions of the self-locking threaded attachment elements being approximately identical.

4. The mechanical system according to claim 1, wherein the line is approximately circular, the turbomachine part to be fixed being approximately in the form of a disk or approximately annular.

5. The mechanical system according to claim 1, wherein each of the attachment threaded elements is a threaded attachment element among the group comprising bolts, studs and nuts, the turbomachine part to be fixed being a turbomachine flange.

6. A turbomachine, comprising: the mechanical system according to claim 1.

7. A turbomachine fabrication method, the method comprising: providing the mechanical system according to claim 1; and fixing a turbomachine part by means of the attachment elements.

8. The mechanical system according to claim 1, wherein the ratio of d2 to d1 is greater than or equal to 1.3.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) This invention will be better understood after reading the description of example embodiments given purely for guidance and in no way limitative, with reference to the appended drawings in which:

(2) FIG. 1 shows an example of a mechanical system according to the invention,

(3) FIG. 2 shows two portions of casings fixed to each other by means of a mechanical system of the same type as that shown in FIG. 1,

(4) FIG. 3 shows a close-up perspective view of the mechanical system shown in FIG. 1,

(5) FIG. 4 shows a first variant of an attachment element in which the attachment element is a bolt,

(6) FIG. 5 shows a second variant of an attachment element in which the attachment element is a nut.

(7) Identical, similar or equivalent parts of the different figures have the same numeric references to facilitate the comparison between one figure and the others.

(8) The different possibilities (variants and embodiments) must be understood as not being mutually exclusive and they can be combined with each other.

DETAILED PRESENTATION OF PARTICULAR EMBODIMENTS

(9) FIG. 1 shows a mechanical system 100 designed to be installed on a turbomachine.

(10) The mechanical system 100 shown is a flange, such as a connecting flange 200 used to connect two portions 20, 30 of combustion gas exhaust casings as shown in FIG. 2.

(11) Such a mechanical system 100 comprises: a first flange 200 that will be used with a second flange 32 shown only in FIG. 2 to connect two portions of casings 20, 30, and a plurality of bolts 310, 330 that is intended to attach the first flange 200 onto the second flange when the first and second flange 200 make the connection between two casings, each of the bolts 310, 330 having a threaded bolt body 311 as shown in FIG. 3, defining a thread axis 320 and a bolt head 315 acting as means of preventing rotation.

(12) The flange 200 has a plane annular shape, the central opening 210 of the ring being adapted for the passage of a rotor and centred onto an axis 205 corresponding to the longitudinal axis of the turbomachine.

(13) The flange 200 comprises a plurality of through holes not shown, for bolts distributed along a line 250. The line 250, as shown in dashed lines in FIG. 1, is approximately circular. The line 250 follows a circumference of the flange 200, like a conventional through hole, preferably with a small clearance.

(14) The through holes are adapted for the passage of bolts 310, 330. Each through hole is preferably smooth to facilitate assembly of bolts 310, 330 on the flange 200.

(15) The through holes are arranged approximately uniformly in pairs.

(16) The through holes on the flange 200 are arranged such that when the bolts 310, 330 are mounted on the first flange 200, the distance between the thread axes 320 of the two bolts 310, 330 corresponding to one pair 300 is approximately equal to d1 and such that the distance between the axes of the two bolts 310, 330 adjacent to each other along the line 250 and belonging to two different pairs is equal to approximately d2.

(17) The distances d1 and d2 are defined taking account of two parameters, namely the mechanical stresses necessary to obtain a high quality connection between the two casings and the dimensions and therefore the weight of the bolt heads 315 of the bolts 310, 330.

(18) Thus, the first parameter is used to determine d2, that will be chosen such that compression forces of the first flange and the second flange are distributed uniformly around their periphery.

(19) The second parameter is used to determine d1, that defines the dimensions of bolt heads 315 for high quality prevention of bolt rotation without the bolts being excessively heavy.

(20) The ratio d2 to d1 may be greater than 1.3.

(21) FIG. 4 shows one of the bolts.

(22) The body of bolt 311 is axially symmetric about the thread axis 320. The body of bolt 311 comprises a threaded part 311a for assembly of a nut and a smooth part 311b for assembly in the corresponding through hole of the first flange 200 and of the second flange.

(23) The smooth part 311b comprises a groove 311c around its periphery adapted to hold a stop ring (not shown) and a part 311d adjusted to the through hole corresponding to the first flange 200 so as to fix the bolt to the first flange 200 before assembly on the second flange.

(24) The bolt head 315 is approximately plane in shape with a bearing face 316 bearing in contact with the first flange 200 when the bolt 310, 330 is installed on the first flange 200. The bolt head 315 is arranged at the end of the adjusted part 311d of the smooth part, the body of bolt 311 extending approximately perpendicular to the bearing face 316. The body of bolt 311 is connected to the centre of the bearing face 316 so that connection loads can be satisfactorily distributed.

(25) The bearing face 316 forms a bearing means appropriate to bear on the first flange 200 when the bolt 310, 330 is installed in the first flange 200, and thus limit translation displacements of the bolt 310, 330 along its thread axis 320 relative to the first flange 200.

(26) The bolt head 315 comprises a stop portion 317 adapted to bear in contact with the portion of the stop 317 of a second bolt 330 that is matched to it when it is installed on the first flange 200.

(27) The stop portion 317 is an approximately plane portion of the bolt head 315 parallel to the thread axis 320 of the bolt 310. The distance between the plane delimited by the stop portion 317 and the centre of the bearing face 316 at the intersection with the thread axis 320 is equal to half d1 minus half the separation distance between bolts 310, 330, this spacing being much less than d1.

(28) For example, the separation distance between bolts 310, 330 may be equal to 0.5 mm.

(29) The bolt head 315, due to its bearing portion 317, is a bolt stop member and forms a rotation prevention means when the bolt 310 is installed on the flange 200 and cooperates with a bolt 330 matched to it.

(30) Each of the bolts 310, 330 forms an attachment element that is also a self-locked element due to the presence of the stop portion 317.

(31) The first flange 200 and the plurality of bolts 310, 330 associated with it form a mechanical system for a turbomachine when the bolts 310, 330 are installed in the corresponding through holes.

(32) Such a mechanical system 100 is suitable for fabrication of a turbomachine.

(33) The second flange has a shape similar to the first flange with through holes corresponding to those in the first flange 200 such that when the first flange 200 is fixed onto the second flange, each of the through holes in the first flange 200 is facing the corresponding through hole in the second flange.

(34) Thus, a turbomachine comprising such a mechanical system 100 may be fabricated using a method including particularly steps consisting of: provide the first casing fitted with the first flange 200, provide the plurality of bolts 310, 330, install the bolts 310, 330 each in the corresponding through hole of the first flange 200, the bolts 310, 330 being matched in pairs 300 with their bearing face 316 bearing on the first flange 200 and the stop portion 317 facing the stop portion 317 of the bolt 330 matched to it, install a stop ring in the groove 311c of each bolt 310, 330 in order to fix them with the first flange. provide the second casing fitted with the second flange, insert the threaded parts 311a of the bolts 310, 330 into the corresponding bolt through holes in the second flange so as to attach the casings together with communication between them, the two flanges 200 squeezing the two casings in contact with each other, provide nuts, not shown, with dimensions compatible with the dimensions of the bolts 310, 330, screw the nuts on the bolts 310, 330 so as to make the junction between the two casings fixed and relatively leaktight.

(35) Thus, when these steps are implemented using a mechanical system 100 as disclosed above, the technician performing these implementations does not need to prevent rotation of the bolts 310, 330, since they are locked in rotation by bearing of their stop portion 317 on the stop portion 317 of the bolt 330 matched to them.

(36) FIG. 5 shows a variant of the mechanical system 100 according to which the attachment elements are bolts 310′.

(37) Such a mechanical system is different from the mechanical system 100 described above in that each of the through holes is a through hole for a bolt, not shown, of the second flange that will be screwed into the corresponding nut 310′ in the mechanical system 100, and in that the nut 310′ comprises a nut body 311′, this nut body 311′ having the stop portion 317′.

(38) A nut 310′ according to this variant comprises a threaded hole 313′ formed in the nut body 311′ and that will hold the threaded part of a bolt, not shown, during attachment of the first flange 200 onto the second flange. The nut 310′ also comprises a central assembly part 312′ in which the threaded hole is also formed.

(39) This central part 312′ may also comprise a self-locked or equivalent zone adapted to prevent accidental loosening of the bolt during operation, particularly in the presence of strong vibrations.

(40) The central part 312′ projecting from the nut body 311′ will be installed in the corresponding through hole in the first flange 200 to enable assembly of the nut 310′ on the first flange 200.

(41) The central part 312′ is adapted so that it can be locked in the through hole of the first flange when it is inserted into the hole. Such an adaptation of the central part may be in the form of a taper of this central part that will cooperate with a larger or conical reaming formed in the first flange 200 on the face opposite the face on which the surface 316′ of the nut will bear in contact.

(42) A turbomachine comprising a mechanical system 100 according to this variant may be fabricated using a method particularly including steps to: provide the first casing fitted with the first flange 200, provide the plurality of nuts 310′, install each of the nuts 310′ in the corresponding through hole in the first flange 200, the nuts 310′ being associated in pairs 300 with their bearing face 316′ bearing on the first flange 200 and the stop portion 317′ bearing on the stop portion of the nut matched with it, the central part 312′ being installed in the corresponding through hole, provide the second casing fitted with the second flange, position the second flange so as to join the casings with a communication between them, the two flanges 200 squeezing the casings in contact with each other, this positioning being arranged such that the through holes of the second flange are coincident with the through holes in the first flange 200, provide bolts with dimensions compatible with the dimensions of nuts 310′, insert the bolts in the through holes in the second flange and screw the bolts in the corresponding nuts 310′ so as to make the junction between the two casings fixed and relatively leaktight.

(43) Although the attachment elements in the two variants described above are bolts 310, 330 and nuts 310′ respectively, the attachment elements may also be studs, the central part of the stud forming a bearing member comprising a stop portion 317 forming a locking means, without going outside the scope of the invention.

(44) Similarly, without going outside the scope of the invention, different types of attachment elements can be associated with each other on a single flange 200. Thus, it would be possible to match a bolt and a stud on each pair 300, the stop portions 317, 317′ of each type of attachment element being adapted to cooperate with the stop portion of an element of the other type.

(45) Similarly, although the stop portion 317 is plane in shape and is identical for each self-locked element, without going outside the scope of the invention, it would also be possible to envisage self-locked elements of a first type with a stop portion 317, 317′ of a first shape, such as a curved surface, and self-locked elements of a second type with a stop portion 317 of a second shape complementary to the first shape, the self-locked elements of the first type in each pair 300 being associated with an element of the second type when the elements are fitted on the part to be fixed.

(46) Similarly, although the part to be fixed in the embodiment disclosed above is a flange and the line 250 is a circular line, the part to be fixed may be in a shape other than a ring, such as a linear shape, and may be another part to be fixed in a turbomachine, such as a rail, without going outside the scope of the invention. According to this possibility, the line would also have an appropriate shape, such as a straight line, for a linear part to be fixed.