APPARATUS FOR SHORTENING THE ROTOR BLADES OF A TURBOMACHINE
20190047108 ยท 2019-02-14
Inventors
Cpc classification
Y02P70/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B24B21/165
PERFORMING OPERATIONS; TRANSPORTING
B24B55/08
PERFORMING OPERATIONS; TRANSPORTING
F01D5/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/307
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B24B55/10
PERFORMING OPERATIONS; TRANSPORTING
F05D2230/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B24B21/16
PERFORMING OPERATIONS; TRANSPORTING
B24B55/10
PERFORMING OPERATIONS; TRANSPORTING
B23Q11/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A belt grinding apparatus for grinding the tips of rotor blades is supported on a rotating rotor. A casing contains the rotatable rotor. An opening in the casing permits access of a grinding belt into the casing where the belt grinds the tips of the blades rotating past. The belt grinding apparatus is attached at the opening at a parting line in the casing.
Claims
1. An apparatus for shortening at least one rotor blade of a turbomachine by grinding a blade tip of the at least one rotor blade of the turbomachine, the apparatus comprising: a casing; a blade tip grinding device comprising only one grinding belt, only one contact roller, and only one tensioning roller, the only one grinding belt running around the only one contact roller and the only one tensioning roller, the blade tip grinding device being positioned at the casing; a rotor in the casing, the rotor being configured for supporting rotor blades on the rotor and oriented for the blades to extend outwardly from the rotor, wherein each supported blade has a tip extending outwardly from the rotor so as to be ground by the grinding device; an opening into the casing formed by removing an upper half of the casing, the opening extending a distance around the rotor and a lower half of the casing to allow access by the grinding device to the tips of the rotor blades as the rotor blades on the rotor rotate past the opening in the casing and past the grinding device; a support surface of the lower half of the casing at the opening, the grinding device being supported on the lower half of the casing at the support surface of the lower half of the casing, the grinding device being positioned to cause the grinding device to extend to the tips of the rotor blades moving past the grinding device for causing the grinding device to grind the tips of the blades; an orienting device located and configured for orienting the rotor blade tips and the grinding device with respect to each other so that when the grinding device is grinding the tips rotating past, the grinding device grinds the tips of the rotor blades in a selected manner; and an attachment device configured to attach the blade tip grinding device at a location on the lower half of the casing at the opening in the casing so that the blade tips are rotated by the rotor past the grinding device at the opening in the casing for the grinding device to grind the blade tips, wherein the apparatus further comprises the turbomachine, the casing is a casing of the turbomachine, the rotor is installed in the casing of the turbomachine, and each supported blade is ground by the grinding device while the rotor and the rotor blades remain installed in the casing of the turbomachine.
2. The apparatus of claim 1, wherein the opening in the casing is configured to define a parting joint of the casing at the opening and the blade tip grinding device is attached to the lower half of the casing at the parting joint of the casing.
3. The apparatus of claim 1, wherein the grinding device in the opening in the casing is movable past the blade tips for grinding the blade tips as they are rotated past the grinding device.
4. The belt grinding apparatus of claim 3, wherein the grinding device further comprises a guide and support for moving the grinding belt past the blade tips for grinding the blade tips as the blade tips rotate past the grinding belt.
5. The apparatus of claim 1, further comprising a grinding dust extraction device configured and located for extracting grinding dust produced during the grinding of the blade tips.
6. The apparatus of claim 5, wherein the extraction device comprises an extraction fan operable and of such strength as to remove the grinding dust generated during grinding.
7. The apparatus of claim 5, wherein the extraction device comprises a filter for filtering dust out of air that is extracted from the casing during the grinding of the blade tips.
8. The apparatus of claim 1, wherein the casing is arcuate in shape around the rotor and the casing has a parting line defined by ends of the arcuate shape, and the blade tip grinding device is attached to the lower half of the casing at the parting line.
9. The belt grinding apparatus of claim 8, wherein the grinding device further comprises a guide and support for moving the grinding belt past the blade tips for grinding the blade tips as the blade tips rotate past the grinding belt.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0031]
[0032]
[0033]
[0034]
[0035]
DETAILED DESCRIPTION OF THE EMBODIMENTS OF THE INVENTION
[0036] The belt grinding apparatus 1 comprises a motor 4, a grinding belt 5 which is driven by the motor 4 and is laid around a contact roller 6 and a tensioning roller 7 and is tensioned between these, a feed/travel device 8 and an orienting device 9, wherein the abovementioned components are arranged on a base plate 10. The belt grinding apparatus 1 further comprises an attachment device 11 by means of which the base plate 10 can be attached to a parting joint 12 of a lower casing half 13 of the turbomachine 3.
[0037] The feed/travel device 8 is configured so as to carry out the feed and travel movement of the grinding belt 5 and in the present case is formed by a cross table. With the aid of the feed/travel device 8, the grinding belt 5 may be moved in mutually perpendicular directions by actuating corresponding handwheels 14 and 15, as indicated by the double arrows 16 and 17.
[0038] In the present case, the orienting device 9 is formed by a rotatably mounted plate which is rotated by hand and can be secured in any desired rotational position.
[0039] The feed/travel device 8 and/or the orienting device 9 can be provided with a contactless measurement system in order to measure the distance to the workpiece to be machined and thus to support the setting of the feed/travel and/or the orientation of the grinding belt 5 with respect to the workpiece.
[0040] In the present case, the attachment device 11 is formed by clamping pieces which can be attached to the parting joint 12 via attachment screws and via tapped bores present in the parting joint 12 of the lower casing half 13.
[0041] The belt grinding apparatus 1 also comprises an extraction device 18 which, in the present case, is provided as a separate unit. Alternatively, however, it may also be formed integrally with the belt grinding apparatus 1. The extraction device 18 comprises a filter (not shown in more detail) and serves to separate carcinogenic dust and to avoid dust explosions. The extraction device 18 further comprises an extractor fan (not shown in more detail) which is strong enough to entirely or at least almost entirely remove the grinding dust generated during grinding machining.
[0042] In order to shorten rotor blades of a turbomachine 3 in the installed state, as shown in
[0043] If there is a risk of the extraction device 18 being unable to prevent the cooling air bores of the rotor blades 2 to be shortened from being blocked with grinding dust, the cooling air bores of the rotor blades 2 to be shortened may be sealed or covered before the grinding machining is carried out. The sealing can for example be carried out using wax. An adhesive film or the like, for example, may be used for the covering.
[0044] In a further method according to one embodiment of the present invention, rotor blades 2 to be shortened may, in the context of new production or in the context of an overhaul, also be attached to a dummy rotor disk which is then mounted on a rotating device. In that context, the rotating device is configured such that it continuously rotates the dummy rotor disk about its axis of rotation. A belt grinding apparatus, such as a belt grinding apparatus 1 arranged on a frame as shown in
[0045]
[0046] The belt grinding apparatus 19 can also be equipped with an extraction device 18, if this is desired, even though such an extraction device 18 is not shown in
[0047] The feed/travel device 25, the orienting device 26 and the extraction device 18 may be formed in similar fashion to the corresponding components of the belt grinding apparatus 1 represented in
[0048] In order to shorten a rotor blade 2, this is removed from the turbomachine 3 in a first step. The rotor blade 2 is then attached to the quick-release device 27 of the belt grinding apparatus 19. In a further step, the grinding belt 22 is oriented relative to the rotor blade 2 by means of the orienting device 26. Thereupon, the rotor blade 2 is shortened using the belt grinding apparatus 19 while the quick-release device 27, together with the rotor blade 2 attached thereto, is pivoted about the pivot axis 28 by means of the drive 32. The grinding particles produced during the grinding machining can be extracted by the extraction device, if such a device is present.
[0049] In the case of this variant according to the invention, too, the cooling air bores of the rotor blade 2 to be shortened can be sealed or covered before the grinding machining is carried out, as has already been described with reference to the first method variant. However, it is also possible to use barrier air which flows from inside the blade through the cooling air bores and thus prevents the bores being blocked. Alternatively or in addition, the rotor blade 2 may simply be cleaned after it has been machined.
[0050] An essential advantage of the belt grinding apparatuses 1 and 19 according to the invention, and of the methods, carried out using these, for shortening rotor blades of a turbomachine by removal of material at the blade tip, resides in the fact that by using a grinding belt which is wider than the blade tip to be shortened, the entire blade tip can be machined in one pass. Accordingly, in contrast to grinding machining using a grinding disk and in contrast to milling machining, it is not necessary to move the grinding belt along the contour of the blade tip, which results in a compact, lightweight and cost-effective construction. In addition, the machining time is decisively reduced. A further advantage of using a belt grinding apparatus is that grinding belts are not as susceptible to transport damage as straight grinding disks and milling cutters. Furthermore, tests have shown that, when using a belt grinding apparatus, there is no risk of the ceramic coating of the blades breaking off. In addition, grinding machining with a grinding belt generates no or almost no burrs, which has the advantage that no or only limited manual post-treatments need be carried out. Yet a further advantage is that with the reduced machining time also comes a reduced hazard period for staff.