US2220914A - Elastic fluid turbine bucket wheel - Google Patents
Elastic fluid turbine bucket wheel Download PDFInfo
- Publication number
- US2220914A US2220914A US222225A US22222538A US2220914A US 2220914 A US2220914 A US 2220914A US 222225 A US222225 A US 222225A US 22222538 A US22222538 A US 22222538A US 2220914 A US2220914 A US 2220914A
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- bucket
- buckets
- blades
- members
- cover
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
Definitions
- the present invention relatestoelastic fluid 4 and 5 are views illustrating another modificaturbine bucket wheels and more particularly to arrangements for covering and tying together the outer ends of the buckets.
- adjacent buckets or blades are usually connected together by some form of a cover or shroud band attached to the ends ofthe buckets-to confine the operating fluid within the working passage U and to prevent it from spilling outwardly past the ends.
- a cover or shroud band attached to the ends ofthe buckets-to confine the operating fluid within the working passage U and to prevent it from spilling outwardly past the ends.
- a further object is to produce a new and improved turbine bucket cover arrangement by which a large portion of the loading stress isdis- W tributed to the adjacent buckets on both sides of the one being acted upon by the operating fluid,
- FIG. 1 represents a section of a 5" turbine bucket wheel in perspective provided with a cover according to my invention
- Fig. 2 is a fragmentary elevation illustrating a detail of the cover-shown in Fig. 1
- Fig, 3 is a fragmentary elevation illustrating an alternative arrangement 65 of the invention disclosed in Figs. 1 and 2;
- Figs. 1 represents a section of a 5" turbine bucket wheel in perspective provided with a cover according to my invention
- Fig. 2 is a fragmentary elevation illustrating a detail of the cover-shown in Fig. 1
- Fig, 3 is a fragmentary elevation illustrating an alternative arrangement 65 of the invention disclosed in Figs. 1 and 2
- l0 indicates the web of the wheel disk or rotor and II the 6 grooved rim thereof which on opposite sides is provided with annular shoulders defining a dovetailed portion l2 for retaining the buckets I3 thereon.
- the bucket blades are curved and have thin inlet and outlet edge portions and thick in- 19 termediate portions.
- the bucket bases I4 are provided with a grooved slot defining an inverted dovetail for cooperatively fitting over the rim of the rotor substantially 'as shown.
- This bucket fastening means forms what is commonly termed the inverted dovetail type of fastening and in itself is well-known in the art and typical of bucket wheels in connection with which my present invention may be carried out. It is understood, of course, that the buckets may be secured to the 20 rotor in any other suitable manner.
- the buckets I3 are each provided with relatively rigid cover portions 15 substantially bridging the space between the adjacent buckets at the outen ends thereof.
- cover portions prevent the operating fluid from escaping outwardly past the ends of thebuckets and absorb the outward pressure which would otherwise be directed against the cover band or tying means. It is preferred that the cover portions be formed integrally with the buckets and be so dimensioned that the facing surfaces of adjacent covers substantially abut with each other around the periphery of the wheel, although it may be desirable to provide 36 suitable clearance to allow necessary thermal and elastic strains to take place without giving rise to accompanying stresses.
- the cover portions I5 together form a continuous band with edge portions projecting axially beyond the inlet and out- 0 let edges respectively of the bucket blades. In a turbine these projecting edgeportions are in cooperative relation with similar bands of adjacent diaphragms.
- Means are also provided for connecting or tying v a group of adjacent buckets together, While in the drawing I have shown groups of four buckets tied together, it is otvious that any suitablenumber may be included in a group.
- the outer surface of each cover portion is provided with a ciroumferentially extending slot I6 so located that it aligns with the adjacent endsof the slots. formed in the; adjacent covers thereby defining a continuous circumferential slot adapted to receiveone or more tying members H.
- the side walls 18 of the slot form spaced-apart extensions projecting upwardly from the cover surface.
- the slot is preferably rectan ular in configuration so that the inner or facing surfaces of 5 the side walls l8 lie in planes parallel with the plane of the disk.
- the tying .members I] are also preferably rectangular in cross-section so as to cooperatively fit into the slot IS, the plane side faces thereof substantially engaging with the slot 10 side' walls.
- the opposite side walls or extensions 18 are provided with aligned holes 19 and the tying members I! with suitably spaced holes 20 so that pins 2
- may be secured in position in any suitable manner such as by peening the ends thereof 7 as shown.
- the tying members may be secured to the extensions l8 so as to allow relative pivotal movements therebetween permitting the ends of the buckets tied together to deflect in the radial plane under the impulse of the operating fluid.
- is provided through the extensions I8 of each bucket and the tie member H, the pin lying substantially parallel with the axis of the wheel.
- the tie member I! is supported in the slot between the extensions I8 slightly above the base of the slot by a small clearance :21) 22. This arrangement will allow limited rocking or flexing movements of the outer ends of the buckets.
- the outer ends of the buckets :15 rigidly together so as to preclude the deflection thereof under the impulse of the operating fluid.
- the depth of the slot, or the length of the extensions l8,' is such as to accommodate a plurality of pins 2
- the tie member H is further snugly seated against the base of the slot as distinguished from'the provision of a clearance corresponding to 22 as shown in Fig 2.
- the tie member is substantially protected by the cover portions l from the outward force of the operating fluid flowing through the working passage between adjacent buckets.
- the cover portions alsodirectly absorb and transmit a considerable amount of the circumferential stress 55 to the adjacent buckets.
- Figs. 4 and 5 a second modification of the invention in which the circumferential slot provided in the bucket covers, extends all the way therethrough to the upper ends of 65 the buckets.
- the slot side walls or extensions 30, and the cover portions .1 are preferably integrally formed with the buckets l3, and are of such width as to substantially bridge the space between the 70 outer ends-of adjacent buckets, although suitable ":-.-75 flowing throughthe working passage, but because this side is relatively narrow as regards its height, as viewed in Fig. 4, it is capable of withstanding relatively high pressures without being unduly stressed thereby.
- Figs. 6 and '7 is illustrated a modification 5 similar to that last described except that the integral extensions or portions 40 are centrally disposed with respect to the ends of the buckets l3. These portions are so aligned as to form a substantially continuous peripheral] rim around the outer ends of the buckets. As in the case of the covers of the first modification and the portions 30 and 3
- the tie members in this in-' 15 stance comprise a pair of similar right angle straps M which are secured as by pins 42 upon opposite sides of the portions 40.
- the lower flanges 43 of the tie members together with the lower edge of the spacer member 40 act as covers to prevent the escape of operating fluid past the ends of the buckets. 1
- tie members of the last two described modifications may be secured to the integral extensions in the two alternative manners as described in connection with the first modification, That-is, a single pin may be used as shown in Fig. 2 whereby relative pivotal movements may take place between the-bucket ends and the tie members, or a plurality of pins may be used as shown in Fig. 3, in which case the bucket ends will be rigidly secured to the tie members.
- Either the L-shaped members or the bar-shaped member is integrally formed with the ends of the blades, while the other member or members are separately formed and bridge a plurality of blades.
- one kind of the members are integrally formed with the blades and the other kind of the members are separately formed.
- each blade has an end portion integrally formed with two L-shaped m1 'nbers l8, whereas in the arrangement of Fig. 7,,for instance, each blade has an .end portion integrally formed with a bar member.
- the legs of. the L-shaped members are united by an intermediate portion so that this intermediate portion together with the base portionsof the legs 5 form a continuous band
- the cover portions integrally formed at the outer ends are essentially U-shaped with the base of the U adjacent'the ends of the blades and the legs of the U defining a channel for receiving a tie member.
- the baseportion of the U is' extended in opposite directions to project beyond the edges of the bucket blades.
- the radial projections of the legs are located inside the con-. necting lines of the outer edges of the blades,
- the legs are axially spaced from and located between the thin inlet and outlet edges of each blade.
- the overall axial distance between-the legs is less than the width of the outer portions of the blades. This is important because in this manner the heavy leg portions and the heavy tie bar'are supported by the thick intermediate blade portions and not by the thin edge portions of the blades.
- Axial flow elastic fluid turbine bucket wheel comprising a disk having a rim, a row of circumferentially spaced bucket blades extending radially from the disk and having inner ends secured to the rim, and tie means for the outer ends of the blades, said tie means including mem- .beyond the inlet and outlet'edges respectively of the blades and the legs .0! the L's extendingparallel to each other, bar members engaging adjacent races or the legs and means securing the barmembers to the legs, one kind 0! the L-shaped and bar members being integrally io'rmed with the ends of the blades and the other kind of the members are separately formed and bridge a plurality of blades.
- Axial flow elastic fluid turbine bucket wheel comprising a disk having a rim, a row of circumferentially spaced bucket blades extending radially from the disk and having inner ends secured to the,rim, and bucket cover and tie means including a cover member for each bucket blade integrally formed with the outer end thereof, the cover members being U-shaped in cross-section with the bases of th Usforming a continuous band having edges p (fleeting axially beyond opposite edges of the blades and legs extending radially outward from the outer surfaces of .the bases and being spaced inward from the corresponding-edges of the blades, and a tie bar located between and secured to the legs.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
ENoU. .12, 1940.
E. L. ROBINSON ELASTIC FLUID TURBINE BUCKET WHEELY Filed July 30, 1938 w m t n e v 1 HIS Att orney.
I so
Patented Nov. 1 2, 1 940 PATENT OFFICE ELASTIC FLUID TURBINE BUCKET WHE Ernest L. Robinson, Schenectady, N. Y., assignor to General Electric Company, a corporation of New York Application July so, 1938, Serial No. 222,225
3 Claims.
The present invention relatestoelastic fluid 4 and 5 are views illustrating another modificaturbine bucket wheels and more particularly to arrangements for covering and tying together the outer ends of the buckets.
n In turbine bucket wheel construction, adjacent buckets or blades are usually connected together by some form of a cover or shroud band attached to the ends ofthe buckets-to confine the operating fluid within the working passage U and to prevent it from spilling outwardly past the ends. Because of the relatively great tangential force exerted by the operating fluid against the buckets, particularly in the high pressure stages, a certain amount of bending of the individual 5 buckets takes place which is accompanied by a corresponding distortion of the cover band between adjacent buckets. This is particularly pronounced in turbines of the partial admission type. ,This distortion of the cover band together with the centrifugal force, due to the wheel rotation, acting outwardly on the cover band and the force exerted by the operating fluid acting directly against the surface of the cover band stresses the attaching means as well as the 1 band itself. In elastic fluid turbines designed not only for high speed operation but also for modcm high pressures and temperatures, the combined forces acting upon the cover band are very large. The usual form of covers consisting of a single tie member riveted onto the bucket ends has proved incapable of withstanding such stresses under severe operating conditions.
It is an object of this invention to provide a new and improved turbine bucket wheel shroud- Kh ing arrangement of increased strength capable of withstanding extreme operating conditioirs.
A further object is to produce a new and improved turbine bucket cover arrangement by which a large portion of the loading stress isdis- W tributed to the adjacent buckets on both sides of the one being acted upon by the operating fluid,
4 while a relatively small percent of the total load is carried by the tie member.
For a consideration of what I believe to be novel and my invention, attention is directed to the following description and the claims appended thereto taken in connection withthe accompanying drawing.
In the drawing, Fig. 1 represents a section of a 5" turbine bucket wheel in perspective provided with a cover according to my invention; Fig. 2 is a fragmentary elevation illustrating a detail of the cover-shown in Fig. 1; Fig, 3 is a fragmentary elevation illustrating an alternative arrangement 65 of the invention disclosed in Figs. 1 and 2; Figs.
tion of the invention; while Figs. 6 and 7 illustrate a still further modification.
Referring to Fig. 1 of the drawing, l0 indicates the web of the wheel disk or rotor and II the 6 grooved rim thereof which on opposite sides is provided with annular shoulders defining a dovetailed portion l2 for retaining the buckets I3 thereon. The bucket blades are curved and have thin inlet and outlet edge portions and thick in- 19 termediate portions. The bucket bases I4 are provided with a grooved slot defining an inverted dovetail for cooperatively fitting over the rim of the rotor substantially 'as shown. This bucket fastening means forms what is commonly termed the inverted dovetail type of fastening and in itself is well-known in the art and typical of bucket wheels in connection with which my present invention may be carried out. It is understood, of course, that the buckets may be secured to the 20 rotor in any other suitable manner.
- According to my invention, the buckets I3 are each provided with relatively rigid cover portions 15 substantially bridging the space between the adjacent buckets at the outen ends thereof.
These cover portions prevent the operating fluid from escaping outwardly past the ends of thebuckets and absorb the outward pressure which would otherwise be directed against the cover band or tying means. It is preferred that the cover portions be formed integrally with the buckets and be so dimensioned that the facing surfaces of adjacent covers substantially abut with each other around the periphery of the wheel, although it may be desirable to provide 36 suitable clearance to allow necessary thermal and elastic strains to take place without giving rise to accompanying stresses. The cover portions I5 together form a continuous band with edge portions projecting axially beyond the inlet and out- 0 let edges respectively of the bucket blades. In a turbine these projecting edgeportions are in cooperative relation with similar bands of adjacent diaphragms.
Means are also provided for connecting or tying v a group of adjacent buckets together, While in the drawing I have shown groups of four buckets tied together, it is otvious that any suitablenumber may be included in a group. The outer surface of each cover portion is provided with a ciroumferentially extending slot I6 so located that it aligns with the adjacent endsof the slots. formed in the; adjacent covers thereby defining a continuous circumferential slot adapted to receiveone or more tying members H. The side walls 18 of the slot form spaced-apart extensions projecting upwardly from the cover surface. The slot is preferably rectan ular in configuration so that the inner or facing surfaces of 5 the side walls l8 lie in planes parallel with the plane of the disk. The tying .members I] are also preferably rectangular in cross-section so as to cooperatively fit into the slot IS, the plane side faces thereof substantially engaging with the slot 10 side' walls. The opposite side walls or extensions 18 are provided with aligned holes 19 and the tying members I! with suitably spaced holes 20 so that pins 2| may be extended therethrough to secure the tying members in the slot. The pins 2| may be secured in position in any suitable manner such as by peening the ends thereof 7 as shown.
The tying members may be secured to the extensions l8 so as to allow relative pivotal movements therebetween permitting the ends of the buckets tied together to deflect in the radial plane under the impulse of the operating fluid. As
shown in Fig. 1,- a single pin 2| is provided through the extensions I8 of each bucket and the tie member H, the pin lying substantially parallel with the axis of the wheel. As illustrated more clearly in Fig. 2, the tie member I! is supported in the slot between the extensions I8 slightly above the base of the slot by a small clearance :21) 22. This arrangement will allow limited rocking or flexing movements of the outer ends of the buckets.
In certain stages of the turbine, it may be desirable to connect the outer ends of the buckets :15 rigidly together so as to preclude the deflection thereof under the impulse of the operating fluid. As shown in Fig. 3, the depth of the slot, or the length of the extensions l8,'is such as to accommodate a plurality of pins 2| therethrough and 40 through the tie member 1'. The tie member H is further snugly seated against the base of the slot as distinguished from'the provision of a clearance corresponding to 22 as shown in Fig 2. By this arrangement relative movements between 45 the extensions of any one bucket and the tie member are precluded and the ends of adjacent buckets are thereby substantially rigidly fixed.
In this modification of the invention, Figs. 1-3, inclusive, the tie member is substantially protected by the cover portions l from the outward force of the operating fluid flowing through the working passage between adjacent buckets. The cover portions alsodirectly absorb and transmit a considerable amount of the circumferential stress 55 to the adjacent buckets. By ruggedly proportioning the dimensions of the slot, the side walls or extensions, the tie member, and the pins, the remaining stresses may be carried by such parts with little danger of failure, even under the most 60 severe of operating conditions.
In Figs. 4 and 5 is shown a second modification of the invention in which the circumferential slot provided in the bucket covers, extends all the way therethrough to the upper ends of 65 the buckets. As'in the first described modification, the slot side walls or extensions 30, and the cover portions .1 are preferably integrally formed with the buckets l3, and are of such width as to substantially bridge the space between the 70 outer ends-of adjacent buckets, although suitable ":-.-75 flowing throughthe working passage, but because this side is relatively narrow as regards its height, as viewed in Fig. 4, it is capable of withstanding relatively high pressures without being unduly stressed thereby.
In Figs. 6 and '7 is illustrated a modification 5 similar to that last described except that the integral extensions or portions 40 are centrally disposed with respect to the ends of the buckets l3. These portions are so aligned as to form a substantially continuous peripheral] rim around the outer ends of the buckets. As in the case of the covers of the first modification and the portions 30 and 3| of the second modification, they may act to distribute part of the bucket loading to adjacent buckets. The tie members in this in-' 15 stance comprise a pair of similar right angle straps M which are secured as by pins 42 upon opposite sides of the portions 40. The lower flanges 43 of the tie members together with the lower edge of the spacer member 40 act as covers to prevent the escape of operating fluid past the ends of the buckets. 1
It is understood that the tie members of the last two described modifications may be secured to the integral extensions in the two alternative manners as described in connection with the first modification, That-is, a single pin may be used as shown in Fig. 2 whereby relative pivotal movements may take place between the-bucket ends and the tie members, or a plurality of pins may be used as shown in Fig. 3, in which case the bucket ends will be rigidly secured to the tie members.
Thus, with my invention I have accomplished an improved construction and arrangement of bucket covers and tie means for covering and tieing together a row of bucket blades which have inner ends secured tothe rim of a bucket wheel disk. Each of the several embodiments shown in the drawing and described above has a plural- 4O ity of buckets with bucket cover and tie means including members on opposite sides at the outer ends of the blades, which members are L-shaped in cross section. The bases of the Us extend axially beyond the inlet and outlet edges respec- 45 tively of the blades and the legs of the Us of each blade are spaced and parallel to each other. The legs. of each of a group of blades are connected by bar members I! engaging adjacent faces of the legs. Either the L-shaped members or the bar-shaped member is integrally formed with the ends of the blades, while the other member or members are separately formed and bridge a plurality of blades. In other words, one kind of the members are integrally formed with the blades and the other kind of the members are separately formed. In the arrangement of Fig. 1 each blade has an end portion integrally formed with two L-shaped m1 'nbers l8, whereas in the arrangement of Fig. 7,,for instance, each blade has an .end portion integrally formed with a bar member. In the arrangement of Figs. 1 to 3 the legs of. the L-shaped members are united by an intermediate portion so that this intermediate portion together with the base portionsof the legs 5 form a continuous band,
Looking at the invention as shown in Figs, 1 to 3 from still another viewpoint, it will be found that the cover portions integrally formed at the outer ends are essentially U-shaped with the base of the U adjacent'the ends of the blades and the legs of the U defining a channel for receiving a tie member. The baseportion of the U is' extended in opposite directions to project beyond the edges of the bucket blades. The radial projections of the legs are located inside the con-. necting lines of the outer edges of the blades,
that is, the legs are axially spaced from and located between the thin inlet and outlet edges of each blade. With such-an arrangement the overall axial distance between-the legs is less than the width of the outer portions of the blades. This is important because in this manner the heavy leg portions and the heavy tie bar'are supported by the thick intermediate blade portions and not by the thin edge portions of the blades.
Having described the principle of operation of my invention together with the apparatus which I now considertorepresent the best embodiment thereof, I desire to have it understood that the :apparatus shown is only illustrative and that the invention may be carried out by other means.
What I claim as new and desire to secure by Letters Patent of the-United States is? 1. Axial flow elastic fluid turbine bucket wheel comprising a disk having a rim, a row of circumferentially spaced bucket blades extending radially from the disk and having inner ends secured to the rim, and tie means for the outer ends of the blades, said tie means including mem- .beyond the inlet and outlet'edges respectively of the blades and the legs .0! the L's extendingparallel to each other, bar members engaging adjacent races or the legs and means securing the barmembers to the legs, one kind 0! the L-shaped and bar members being integrally io'rmed with the ends of the blades and the other kind of the members are separately formed and bridge a plurality of blades.
2. Axial flow elastic fluid turbine bucket wheel at the outer endoi each bucket with the base of the L extending axially beyond the edge of the bucket blade and the leg of the L axially spaced from and located between the inlet and outlet edges of the blade, and a bar bridging a group'of blades and secured to each 'L-shaped member of y the group.
3. Axial flow elastic fluid turbine bucket wheel comprising a disk having a rim, a row of circumferentially spaced bucket blades extending radially from the disk and having inner ends secured to the,rim, and bucket cover and tie means including a cover member for each bucket blade integrally formed with the outer end thereof, the cover members being U-shaped in cross-section with the bases of th Usforming a continuous band having edges p (fleeting axially beyond opposite edges of the blades and legs extending radially outward from the outer surfaces of .the bases and being spaced inward from the corresponding-edges of the blades, and a tie bar located between and secured to the legs.
ERNEST L. ROBINSON.
Priority Applications (1)
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US222225A US2220914A (en) | 1938-07-30 | 1938-07-30 | Elastic fluid turbine bucket wheel |
Applications Claiming Priority (1)
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US222225A US2220914A (en) | 1938-07-30 | 1938-07-30 | Elastic fluid turbine bucket wheel |
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US2220914A true US2220914A (en) | 1940-11-12 |
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US222225A Expired - Lifetime US2220914A (en) | 1938-07-30 | 1938-07-30 | Elastic fluid turbine bucket wheel |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1035662B (en) * | 1956-04-16 | 1958-08-07 | Gen Electric | Shroud of a blade ring for axial turbines or compressors |
US2959393A (en) * | 1956-04-16 | 1960-11-08 | Gen Electric | Turbine bucket cover assembly |
US3070350A (en) * | 1958-06-02 | 1962-12-25 | Gen Motors Corp | Rotor shroud |
DE1426778B1 (en) * | 1962-07-11 | 1969-11-20 | Bbc Brown Boveri & Cie | Method of assembling a series of rigid blades with cover plates |
DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
US20080080970A1 (en) * | 2006-10-03 | 2008-04-03 | Rolls-Royce Plc. | Gas turbine engine vane arrangement |
EP2682566A1 (en) * | 2011-02-28 | 2014-01-08 | Mitsubishi Heavy Industries, Ltd. | Stator blade unit of rotary machine, method for producing stator blade unit of rotary machine, and method for joining stator blade unit of rotary machine |
-
1938
- 1938-07-30 US US222225A patent/US2220914A/en not_active Expired - Lifetime
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1035662B (en) * | 1956-04-16 | 1958-08-07 | Gen Electric | Shroud of a blade ring for axial turbines or compressors |
US2959393A (en) * | 1956-04-16 | 1960-11-08 | Gen Electric | Turbine bucket cover assembly |
US3070350A (en) * | 1958-06-02 | 1962-12-25 | Gen Motors Corp | Rotor shroud |
DE1426778B1 (en) * | 1962-07-11 | 1969-11-20 | Bbc Brown Boveri & Cie | Method of assembling a series of rigid blades with cover plates |
DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
US20080080970A1 (en) * | 2006-10-03 | 2008-04-03 | Rolls-Royce Plc. | Gas turbine engine vane arrangement |
US8356981B2 (en) * | 2006-10-03 | 2013-01-22 | Rolls-Royce Plc | Gas turbine engine vane arrangement |
EP2682566A1 (en) * | 2011-02-28 | 2014-01-08 | Mitsubishi Heavy Industries, Ltd. | Stator blade unit of rotary machine, method for producing stator blade unit of rotary machine, and method for joining stator blade unit of rotary machine |
EP2682566A4 (en) * | 2011-02-28 | 2014-10-29 | Mitsubishi Heavy Ind Ltd | Stator blade unit of rotary machine, method for producing stator blade unit of rotary machine, and method for joining stator blade unit of rotary machine |
US9086078B2 (en) | 2011-02-28 | 2015-07-21 | Mitsubishi Hitachi Power Systems, Ltd. | Stationary vane unit of rotary machine, method of producing the same, and method of connecting the same |
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