Rotary machine with improved shaft
11821433 · 2023-11-21
Assignee
Inventors
Cpc classification
F05B2240/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/122
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/051
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/076
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D29/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/051
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A rotary machine is disclosed, which includes a rotary shaft having a rotation axis, a first shaft end, and a second shaft end; a first bearing arrangement at the first shaft end; a second bearing arrangement at the second shaft end; a coupling flange mechanically connected to the first shaft end. The coupling flange is mechanically connected to the first shaft end by means of a first axial-contact coupling.
Claims
1. A rotary machine comprising: a rotary shaft comprising a rotation axis, a driven shaft end, and a non-driven shaft end; stationary pads circularly arranged about the rotation axis of the rotary shaft; bearings disposed at the driven shaft end and the non-driven shaft end, the bearings comprising a radial bearing and a thrust bearing, the thrust bearing comprising a thrust collar mounted for co-rotating with the rotary shaft and co-acting with the stationary pads; on the driven shaft end, a coupling flange; and a first axial-contact coupling mechanically connecting the coupling flange to the driven shaft end, the first axial-contact coupling comprising a first Hirth joint with radial teeth formed on an annular front surface of the driven shaft end and radial teeth formed on an annular surface of the thrust collar on the driven shaft end; and on the non-driven end, a second axial-contact coupling connecting the thrust collar to the non-driven shaft end, the second axial-contact coupling comprising a second Hirth joint including radial teeth formed on an annular front surface of the non-driven shaft end and radial teeth formed on an annular surface of the thrust collar on the non-driven shaft end, and tie-rods that reside in the shaft on both the driven shaft end and the non-driven shaft end, wherein the radial teeth on the driven shaft end and the non-driven shaft end mesh with one another when pressed together in mechanical engagement due to threaded engagement between the tie-rods and threaded nuts.
2. The rotary machine of claim 1, wherein the coupling flange has an outer flange diameter greater than a diameter of the first shaft end.
3. The rotary machine of claim 1, wherein the rotary shaft supports centrifugal impellers disposed between the bearings on the driven shaft end and the non-driven shaft end, the rotary machine being a centrifugal compressor.
4. The rotary machine of claim 1, wherein the coupling flange comprises connection members for mechanical connection to a motion transmission joint.
5. The rotary machine of claim 1, wherein a tie rod and ring nut arrangement axially presses the coupling flange against the rotary shaft.
6. The rotary machine of claim 1, wherein the thrust collar on the driven end is mounted on a shaft portion overhanging from a the radial bearing.
7. The rotary machine of claim 1, wherein the first axial contact coupling comprises a rigid bush-shaped member connected via axially spaced resilient members to respective end rings that mechanically coupled to the coupling flange.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) A more complete appreciation of the disclosed embodiments of the invention and many of the attendant advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
(2)
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DETAILED DESCRIPTION
(8) The following detailed description of exemplary embodiments refers to the accompanying drawings. The same reference numbers in different drawings identify the same or similar elements. Additionally, the drawings are not necessarily drawn to scale. Also, the following detailed description does not limit embodiments of the invention. Instead, the scope of the invention is defined by the appended claims.
(9) Reference throughout the specification to “one embodiment” or “an embodiment” or “some embodiments” means that the particular feature, structure or characteristic described in connection with an embodiment is included in at least one embodiment of the subject matter disclosed. Thus, the appearance of the phrase “in one embodiment” or “in an embodiment” or “in some embodiments” in various places throughout the specification is not necessarily referring to the same embodiment(s). Further, the particular features, structures or characteristics may be combined in any suitable manner in one or more embodiments.
(10) The following description specifically relates to applications of the subject matter disclosed herein in combination with turbomachines, such as in particular centrifugal compressors. However, the scope of the disclosure is not limited to such machinery. Those skilled in the art will appreciate that applications to other rotary machines and equipment are possible, where similar problems arise in connection with the natural frequencies of the rotating components and which can be at least partly alleviated by using the teaching of the present disclosure.
(11) In
(12) In
(13) As better shown in
(14) In the exemplary embodiment disclosed herein, referring to
(15) In the exemplary embodiment of
(16) Sealing members, such as dry-gas sealing arrangements schematically shown at 25, 27 are provided in the compressor casing 9, to reduce or prevent fluid leakages from the interior of compressor 3 towards the bearing assemblies 10 and 11.
(17) Referring now to
(18) A coupling flange 31 is mechanically connected to the first shaft end 7A. The coupling flange 31 has an outer flange diameter D31 which is larger than the outer diameter D7A of the first shaft end 7A. Connection members 33, such as bolts or the like, can be circularly arranged about the rotation axis A-A of the compressor 9, for mechanically connecting the coupling flange 31 to the motion transmission joint 17. This latter can be comprised of a rigid central bush-shaped member 17A, which is connected, through axially spaced resilient members 17B, 17C, to respective end rings 17D, 17E. The ring 17D is in turn mechanically coupled to the coupling flange 31.
(19) The coupling flange 31 is mechanically coupled to the first shaft end 7A by means of an axial-contact coupling. According to the embodiment shown in
(20) In the embodiment of
(21) The coupling flange 31 can be mounted on the first shaft end 7A by means of a tie rod 45 and a ring nut 47 (
(22) The axial-contact coupling provided by the Hirth joint 35 in combination with the coupling flange 31 provide a mechanical coupling between the rotary shaft 7 and the motion transmission joint 17. By means of the axial-contact mechanical coupling between shaft 7 and motion transmission joint 17, the shaft end 7A is made substantially shorter than shaft ends of the current art, which are required for mechanical coupling using a radial interference involving conical interference surfaces.
(23) According to some embodiments, compared with current art couplings, the other dimensions being the same, the use of a Hirth joint can reduce the length of the shaft portion overhangingly projecting beyond the first bearing arrangement 10 by around 38%, which in turn reduces the overhanging mass (i.e. the mass of the shaft end portion projecting in an overhanging fashion from the first bearing arrangement 10) by around 49%. An increase of the fourth natural frequency of the rotary shaft 7 can thus be obtained, such that the centrifugal compressor 3 can rotate at a higher speed without reaching the fourth critical speed. Similar results can be achieved also with other axial-contact couplings, e.g. using simple friction surfaces, rather than a Hirth joint. This latter, however, is particularly advantageous since the teeth of the Hirth joint allow a high torque to be transmitted through the joint.
(24) Referring now to
(25) The second bearing arrangement 11 can further comprise a thrust bearing, i.e. an axial bearing, labeled 11B. The thrust bearing comprises a thrust collar 51 mounted on the second end 7B of rotary shaft 7 for co-rotation with rotary shaft 7, and co-acting with stationary pads 53, 55 supported in a bearing housing. The thrust collar 51 is mechanically coupled to the second shaft end 7B by means of a respective axial-contact coupling. According to embodiments, the axial-contact coupling comprises a Hirth joint 56. The thrust collar 51 has an outer diameter D51, which can be larger than the diameter of the shaft end 7B.
(26)
(27) The Hirth joint 56 has an outer diameter D56 which is larger than the outer diameter D51 of the thrust collar 51.
(28) By using an axial-contact coupling, instead of a radial interference coupling of the current art, for coupling the thrust collar 51 to the second shaft end 7B, the length of the shaft end portion, which overhangingly projects beyond the second bearing arrangement 11, becomes substantially shorter.
(29) According to some embodiments, compared with current art couplings, the other dimensions being the same, the use of an axial-contact coupling, e.g. provided by a Hirth joint for connecting the thrust collar 51 to the rotary shaft 7 can reduce the length of the shaft portion projecting beyond the second bearing arrangement 11 by around 23%, which in turn reduces the overhanging mass (i.e. the mass of the shaft end portion projecting in an overhanging fashion from the second bearing arrangement 11) by around 19%. An increase of the fourth natural frequency of the rotary shaft 7 can thus be obtained.
(30) Even though in the embodiment described herein two axial-contact couplings, both embodied by Hirth joints 35, 56 are used in order to reduce the overhanging mass on both the drive end side and the non-drive end side of the centrifugal compressor 3, those skilled in the art will understand that advantages in terms of rotor dynamic and increase of the natural speeds of the higher order (above the first critical speed) of the rotary shaft 7 can be achieved also if only one axial-contact coupling is used, e.g. on the first shaft end 7A, or else only on the second shaft end 7B, the other shaft end being provided with a radial interference coupling using a conical interference connection according to the current art. Best performances are obtained, if both the first shaft end 7A and the second shaft end 7B are provided with axial-contact couplings for connecting the coupling flange 31 and the thrust collar 51 to the rotary shaft ends 7A and 7B, respectively.
(31) It shall also be understood that, while in the above description and in the drawings both axial-contact couplings are embodied by Hirth joints, in other embodiments two different axial-contact couplings can be used instead, for instance a Hirth joint at one end and an axial friction contact at the other.
(32) While the disclosed embodiments of the subject matter described herein have been shown in the drawings and fully described above with particularity and detail in connection with several exemplary embodiments, it will be apparent to those of ordinary skill in the art that many modifications, changes, and omissions are possible without materially departing from the novel teachings, the principles and concepts set forth herein, and advantages of the subject matter recited in the appended claims. Hence, the proper scope of the disclosed innovations should be determined only by the broadest interpretation of the appended claims so as to encompass all such modifications, changes, and omissions. In addition, the order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments.