US2350309A - Blade shrouding - Google Patents

Blade shrouding Download PDF

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US2350309A
US2350309A US356411A US35641140A US2350309A US 2350309 A US2350309 A US 2350309A US 356411 A US356411 A US 356411A US 35641140 A US35641140 A US 35641140A US 2350309 A US2350309 A US 2350309A
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blade
shroud
base
blades
portions
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US356411A
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Hans P Dahlstrand
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Allis Chalmers Corp
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Allis Chalmers Corp
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Priority to US356411A priority Critical patent/US2350309A/en
Priority to US465672A priority patent/US2350310A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making

Definitions

  • This invention relates to blade shrouding and more particularly to a. method of forming a builtup shroud and seal structure for the tip portions of turbine blades.
  • the primary object of this invention is to provide a method of forming an improved built-up shroud and seal structure for turbine blades which is extremely durable and cheap to manufacture.
  • Another object of this invention is to provide a method of forming an improved shroud and seal structure for turbine blades in which the shroud and seal structure is formed from a plurality of stampings which are welded together and to the blade tip to form an integral shroud and seal structure having at least three sealing flanges.
  • a further object of this invention is to provide an improved method of constructing a built-up welded shroud and seal structure for turbine blades.
  • Fig. 1 is a partial sectional view of a turbine spindle and stator having coacting blades em-' bodying the invention
  • Fig. 2 is a plan view of a portion of a moving blade row taken on line IIII of Fig. 1 with a part of the shroud structure broken away;
  • Fig. 3 is a side view of the top portion of one of the blades shown in Fig. 2 with the shroud removed;
  • Fig. 4 is a plan view of the blade shown in Fig. 3;
  • Fig. 5 is a side view, partly in section, of the type of blade shown in Figs. 3 and 4 with the shroud and sealin means attached thereto;
  • Fig. 6 is a side view of the top portion-of a blade illustrating a modified construction
  • Fig. '7 is a plan view of the blade shown in Fig.6;
  • Fig. 8 is a side view, partly in section, of the type of blade shown in Figs. 6 and '7 with the shroud and sealing means attached thereto;
  • Fig. 9 is a perspective view of a segmental group of blades with the shroud removed.
  • Fig. 10 is a vertical section illustrating apparatus for temporarily holding the shroud and sealing structure on a blade or on a group of blades preparatory to Welding the structure thereto.
  • FIG. 1 of the drawing it is seen that the invention isshown as applied to the stationary and moving blades l and 2, respectively, of a turbine structure comprising a stator 3 and a rotor 4.
  • the individual blades l and 2 are provided with conventional root or base portions 6 and 1, respectively, which are removably secured in circ-umferentially extending grooves 8 and 9 in the stator and rotor, respectively, in the usual manner.
  • the manner in which the blades are secured in the turbine structure forms no part of this invention and since any desired form of securing means may be used, a further description in this connection is not necessary for a complete understanding of "the present invention.
  • the tip portions of the blades 2 are shaped to provide a stepped projection comprising a relatively short'porti-on II which is made approximately equal in length to the thickness of the shroud member to be secured to the blade tip and a relatively long portion [2 which is made approximately equal in length to twice the thick-
  • the shrouding and sealing means comprises a first member having a base or shroud portion l3 and an upstanding sealing flange l4 and a, second channel shaped member having a base or Web portion N3 of less width than the base portion l3 of the first member and presenting when mounted on the tip portion of a blade a pair of laterally spaced upstanding sealing flanges H.
  • the base portion I3 of the first member is provided with an opening l8 adapted to snugly receive the stepped projection and the base member 16 0f the second member is also provided with an opening l9 adapted to snugly receive the relatively long portion l2 of the said projection.
  • the Width of the base portion l3 of the first member is such that when the first member is positioned on the blade tip as shown in Fig. 5, an edge portion of said base member extends beyond and overhangs the edge of the blade thereby providing a laterally extending sealing flange 2
  • the dimensions of the first and second members, the arrangement of the openings [8 and I9 therein, respectively, and the dimensions and the arrangement ofthe stepped projection are such that when the first and second members are positioned on the tip portion of a blade in the order named, the shrouding and sealing means are arranged as shown in Fig. 5.
  • the thickness of the baseor web portion l6 of the second member' is substantially the same as the thickness of the base or shroud portion 13 of the first member. Consequently, since the length of the portions II and I2 of the stepped projection is approximately equal to the thickness and to twice the thickness of the shroud portion l3, respectively, it should be obvious that when the first and second members are positioned on the blade as shown in Fig.
  • the top of the portion II will be nearl flush with the top surface of the base or shroud portion l3 and the top of the portion 12 will be nearly flush with the top surface of the base or web portion I6. Therefore, when the first and second members are thus positioned on the blade tip, all that remains to be done in order to obtain a permanent structure is to weld the base portions of the first and second members to,
  • first and second members are dimensioned to span a series of blades as indicated in Fig. 2, the said members are positioned on and welded to the blades after they have been mounted on'the turbine rotor or stator. Any suitable means may be employed for holdin said members in their proper assembled relation duringthe welding operation and in this connection apparatus somewhat similar to that shown in Fig. has been found entirely satisfactory.
  • the modified arrangement shown in Figs. 6-8, inclusive, in which like numerals are used to designate thesame or similar parts, differs from that shown in Figs. 1-5, inclusive, in that the tip portion of the blade 2 is provided with two laterally spaced upstandin projections 22 and 23, and in that the base or shroud portion [3 of the first member is provided with two laterally spaced openings 24 and 26 adapted to snugly receive the projections 22 and 23, respectively.
  • the length of the projection 22 is approximately equal to the thickness of the base or shroud portion I3 of the first member and the length of the projection 23 is approximately equal to the combined thickness of the base or shroud member iii of the first member and the base or web portion I5 of the second member as best shown in Fig. 8.
  • the first and second members comprising the shrouding and sealing means are positioned and held in position on the tip portions of the blades and welded thereto in exactly the same manner as set forth in connection with the description of Figs. 1-5, inclusive, and a repetition of this procedure is not deemed necessary for a complete understanding of the invention.
  • the resultant structure affords all of the advantages with respect to assembly and strength'inherent in the preferred construction shown in Figs. 1-5, inclusive, but is less desirable in that shaping spaced projections is more difficult and therefore more costly than shaping the stepped projection employed in the preferred construction.
  • Fig. 9 shows a unitary segmental blade group 21 in which the tip portion of each blade 28 is provided with a stepped projection comprising each such group of blades is of course identical to that disclosed in connection with Figs. 1-5, inclusive, but in this construction, the first and second members comprising the shrouding and sealing means are preferably secured to the individual groups before they are mounted on the turbin rotor or stator.
  • Fig. 10 illustrates a suitable jig or fixture 3
  • comprises a base 32 having a portion 33 adapted to receive thereon the base member 29 of a segmental blade group, a pair of top members 34 and 36 having edge portions 31 and 38, respectively, adapted to coact with the flanges l4 and 2! of the first member and with the flanges ll of the second member, spacing members 39 and M, and clamping bolts 42 and 43 by means of which the top members 34 and 36 may be drawn toward the base 32 thereby firmly holding the first and second members in their assembled relation on the tip portions of the blades.
  • the jig 3! is merely illustrative of a commercial ly practical construction adapted for carrying out the present invention with respect to segmental blade groups and it should be understood that any other suitable jig or fixture may be used if it is so desired.
  • the shrouding and sealing means applied to the stationary blades I differs from that employed on the moving blades 2 in that the first member is channel shaped and in that the second member is L-shaped.
  • the web portion 44 of the first member constitutes the shroud portion and the channels 46 sealing flanges.
  • the base member 4'! of the second member is of less width than the web portion 44 of the first member and is adapted to be positioned on the base or web portion 44 of the first member so that the sealing flange 48 is disposed approximately midway between the channels 46 on the first member.
  • the first and second members are positioned on the tip portion of the stationary blades and secured thereto in exactly the same manner as disclosed in connection with the moving blades 2 and therefore a further description in this connection is deemed unnecessary.
  • the length of the centrally disposed sealing flange is preferably made higher than the height of the other sealing flanges and the opposed surfaces of the rotor and stator are provided with coacting grooves 49 and 5
  • the disclosed construction is much stronger than the tenoned constructions heretofore employed since, as clearly shown, a shroud and seal structure embodying the invention is secured or attached to the end of the blade by an effective bond area which is substantially equal to the area of the blade end, thereby materially reducing, and in some instances, entirely eliminating the cantilever effect produced by cantrifugal force acting on the free edges of shroud and seal strips which are secured to the end of a blade by a centrally disposed tenon.
  • Shrouding and sealing structures with multiple spaced sealing flanges can be readily built up in accordance with this invention more cheaply than has heretofore been possible with the prior art methods and the structures produced in accordance with this invention have excellent physical properties with respect to stress resistance and with respect to corrosion and erosion resistance.
  • the invention is applicable to all types of turbine blading with respect to which it is necessary to employ a shrouding and sealing means and while the invention has been disclosed in connection with shrouding and sealing means adapted to span a series of blades, it should be understood that the invention is not in any manner limited to the exact mode of construction or to the exact constructions herein shown and described as various modifications within the scope of the appended claims may occur to persons skilled in the art.
  • a method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on said end and adjacent one edge thereof a first upstanding portion and having in said end adjacent its other edge a second upstanding portion of materially greater length than said first portion, placing on said end of the blade a first element of said structure apertured to receive said upstanding portions and having a thickness approximately equal to the length of said first portion, superimposing on said first element, a second element of said structure including a base apertured to receive said second portion and having a thickness approximately equal to the exposed length of said second portion and a width sufiiciently less than the width of said first element to leave exposed a part of said end of said first portion, and securing said first element and the base of said second element to the exposed parts of said first and second portions, respectively.
  • a method of forming a combined shroud and seal structure on the end of a blade member presenting in spaced upstanding relation, a first portion and a second portion of materially greater length than said first portion which comprises placing on said end of the blade a shroud element apertured to receive said upstanding portions and having a thickness approximately equal to the length of said first portion, superimposing on said shroud strip a seal element including a base apertured to receive said second portion and having a thickness approximately equal to the exposed length of said second portion and a width sufiiciently less than the width of said shroud element to leave exposed a part of the end of said first portion, and securing said shroud element and the base of said seal element to the exposed parts of said first and second portions, respectively.
  • a method of forming a combined shroud and seal structure on the end of a blade member presenting an upstanding stepped projection having its lower step disposed adjacent one edge of said blade and having its higher step disposed adjacent the other edge of said blade which comprises placing on said end of the blade a shroud element apertured to receive said upstanding projection and having a thickness approximately equal to the height of said lower step, superimposing on said shroud strip a seal element including a base apertured to receive said higher step and having a thickness approximately equal to the height of said higher step and a width sufficiently less than the width of said shroud element to leave exposed a part of the top of said lower step, and securing said shroud element and the base of said seal element to the exposed parts of said lower and higher steps, respectively.
  • a method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on one end thereof juxtapositioned short and long tenon portions, placing on said one end of the blade a first element of said structure apertured to receive and expose the end parts of said short and long tenon portions, superimposing on said first element a second element of said structure including a base apertured to receive and expose the end part of said long tenon portion and having a width sufiiciently less than the width of said first element to leave exposed a part of the end of the short tenon portion, and securing saidfirst element and the base of said second element to the exposed end parts of said short and long tenon portions, respectively.
  • a method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on one end thereof juxtapositioned short and long tenon portions, placing on said one end of the blade a first element of said structure apertured to receive and expose the end parts of said short and long tenon portions and having a thickness approximately equal to the length of said short tenon portion, superimposing on said first element a second element of said structure including a base apertured to receive and expose the end part of said long tenon portion and having a thickness approximately equal to the exposed length of said long tenon portion and a width sufiiciently less than the width of said first element to leave exposed a part of the end of the short tenon portion, and fusibly uniting said first element and the base of said second element to the exposed end parts of said short and long tenon portions, respectively.

Description

y l944v- H. P. DAHLSTRAND f 2,350,309
BLADE SHROUDING Filed Sept. 12, 1940 Patented May 30, 1944 BLADE SHROUDING Hans P. Dahlstrand, Wauwatosa, Wis., assignor to Allis-Chalmers Manufacturing. Company, Milwaukee, Wis, a corporation of Delaware Application September 12, 1940, Serial No. 356,411
5 Claims.
This invention relates to blade shrouding and more particularly to a. method of forming a builtup shroud and seal structure for the tip portions of turbine blades.
The primary object of this invention is to provide a method of forming an improved built-up shroud and seal structure for turbine blades which is extremely durable and cheap to manufacture.
Another object of this invention is to provide a method of forming an improved shroud and seal structure for turbine blades in which the shroud and seal structure is formed from a plurality of stampings which are welded together and to the blade tip to form an integral shroud and seal structure having at least three sealing flanges.
A further object of this invention is to provide an improved method of constructing a built-up welded shroud and seal structure for turbine blades.
The invention accordingly consists of the method of construction and of the various features of construction, combinations of elements and arrangements of parts as more fully pointed out in the appended claims and in the detailed description, in which:
Fig. 1 is a partial sectional view of a turbine spindle and stator having coacting blades em-' bodying the invention;
Fig. 2 is a plan view of a portion of a moving blade row taken on line IIII of Fig. 1 with a part of the shroud structure broken away;
Fig. 3 is a side view of the top portion of one of the blades shown in Fig. 2 with the shroud removed;
Fig. 4 is a plan view of the blade shown in Fig. 3;
Fig. 5 is a side view, partly in section, of the type of blade shown in Figs. 3 and 4 with the shroud and sealin means attached thereto;
Fig. 6 is a side view of the top portion-of a blade illustrating a modified construction;
Fig. '7 is a plan view of the blade shown in Fig.6;
Fig. 8 is a side view, partly in section, of the type of blade shown in Figs. 6 and '7 with the shroud and sealing means attached thereto;
Fig. 9 is a perspective view of a segmental group of blades with the shroud removed; and
Fig. 10 is a vertical section illustrating apparatus for temporarily holding the shroud and sealing structure on a blade or on a group of blades preparatory to Welding the structure thereto.
mass of the said shroud member.
Referring to Fig. 1 of the drawing, it is seen that the invention isshown as applied to the stationary and moving blades l and 2, respectively, of a turbine structure comprising a stator 3 and a rotor 4. The individual blades l and 2 are provided with conventional root or base portions 6 and 1, respectively, which are removably secured in circ-umferentially extending grooves 8 and 9 in the stator and rotor, respectively, in the usual manner. The manner in which the blades are secured in the turbine structure forms no part of this invention and since any desired form of securing means may be used, a further description in this connection is not necessary for a complete understanding of "the present invention.
Referring to Figs. 2-5 inclusive, it is seen that the tip portions of the blades 2 are shaped to provide a stepped projection comprising a relatively short'porti-on II which is made approximately equal in length to the thickness of the shroud member to be secured to the blade tip and a relatively long portion [2 which is made approximately equal in length to twice the thick- The shrouding and sealing means comprises a first member having a base or shroud portion l3 and an upstanding sealing flange l4 and a, second channel shaped member having a base or Web portion N3 of less width than the base portion l3 of the first member and presenting when mounted on the tip portion of a blade a pair of laterally spaced upstanding sealing flanges H. The base portion I3 of the first member is provided with an opening l8 adapted to snugly receive the stepped projection and the base member 16 0f the second member is also provided with an opening l9 adapted to snugly receive the relatively long portion l2 of the said projection. The Width of the base portion l3 of the first member is such that when the first member is positioned on the blade tip as shown in Fig. 5, an edge portion of said base member extends beyond and overhangs the edge of the blade thereby providing a laterally extending sealing flange 2|.
The dimensions of the first and second members, the arrangement of the openings [8 and I9 therein, respectively, and the dimensions and the arrangement ofthe stepped projection are such that when the first and second members are positioned on the tip portion of a blade in the order named, the shrouding and sealing means are arranged as shown in Fig. 5. The thickness of the baseor web portion l6 of the second member' is substantially the same as the thickness of the base or shroud portion 13 of the first member. Consequently, since the length of the portions II and I2 of the stepped projection is approximately equal to the thickness and to twice the thickness of the shroud portion l3, respectively, it should be obvious that when the first and second members are positioned on the blade as shown in Fig. 5, the top of the portion II will be nearl flush with the top surface of the base or shroud portion l3 and the top of the portion 12 will be nearly flush with the top surface of the base or web portion I6. Therefore, when the first and second members are thus positioned on the blade tip, all that remains to be done in order to obtain a permanent structure is to weld the base portions of the first and second members to,
the juxtapositioned portions H and I2 of the stepped projection as indicated in Figs. 1, 2 and 5. When the first and second members are dimensioned to span a series of blades as indicated in Fig. 2, the said members are positioned on and welded to the blades after they have been mounted on'the turbine rotor or stator. Any suitable means may be employed for holdin said members in their proper assembled relation duringthe welding operation and in this connection apparatus somewhat similar to that shown in Fig. has been found entirely satisfactory.
The modified arrangement shown in Figs. 6-8, inclusive, in which like numerals are used to designate thesame or similar parts, differs from that shown in Figs. 1-5, inclusive, in that the tip portion of the blade 2 is provided with two laterally spaced upstandin projections 22 and 23, and in that the base or shroud portion [3 of the first member is provided with two laterally spaced openings 24 and 26 adapted to snugly receive the projections 22 and 23, respectively. The length of the projection 22 is approximately equal to the thickness of the base or shroud portion I3 of the first member and the length of the projection 23 is approximately equal to the combined thickness of the base or shroud member iii of the first member and the base or web portion I5 of the second member as best shown in Fig. 8. The first and second members comprising the shrouding and sealing means are positioned and held in position on the tip portions of the blades and welded thereto in exactly the same manner as set forth in connection with the description of Figs. 1-5, inclusive, and a repetition of this procedure is not deemed necessary for a complete understanding of the invention. The resultant structure affords all of the advantages with respect to assembly and strength'inherent in the preferred construction shown in Figs. 1-5, inclusive, but is less desirable in that shaping spaced projections is more difficult and therefore more costly than shaping the stepped projection employed in the preferred construction.
Fig. 9 shows a unitary segmental blade group 21 in which the tip portion of each blade 28 is provided with a stepped projection comprising each such group of blades is of course identical to that disclosed in connection with Figs. 1-5, inclusive, but in this construction, the first and second members comprising the shrouding and sealing means are preferably secured to the individual groups before they are mounted on the turbin rotor or stator.
Fig. 10 illustrates a suitable jig or fixture 3| for holding the first and second members in their proper assembled relation on the tip portions of the blades 28 during the welding operation. The jig 3| comprises a base 32 having a portion 33 adapted to receive thereon the base member 29 of a segmental blade group, a pair of top members 34 and 36 having edge portions 31 and 38, respectively, adapted to coact with the flanges l4 and 2! of the first member and with the flanges ll of the second member, spacing members 39 and M, and clamping bolts 42 and 43 by means of which the top members 34 and 36 may be drawn toward the base 32 thereby firmly holding the first and second members in their assembled relation on the tip portions of the blades. The jig 3! is merely illustrative of a commercial ly practical construction adapted for carrying out the present invention with respect to segmental blade groups and it should be understood that any other suitable jig or fixture may be used if it is so desired.
Referring again to Fig. 1, it is seen that the shrouding and sealing means applied to the stationary blades I differs from that employed on the moving blades 2 in that the first member is channel shaped and in that the second member is L-shaped. The web portion 44 of the first member constitutes the shroud portion and the channels 46 sealing flanges. The base member 4'! of the second member is of less width than the web portion 44 of the first member and is adapted to be positioned on the base or web portion 44 of the first member so that the sealing flange 48 is disposed approximately midway between the channels 46 on the first member. The first and second members are positioned on the tip portion of the stationary blades and secured thereto in exactly the same manner as disclosed in connection with the moving blades 2 and therefore a further description in this connection is deemed unnecessary. In all modifications, the length of the centrally disposed sealing flange is preferably made higher than the height of the other sealing flanges and the opposed surfaces of the rotor and stator are provided with coacting grooves 49 and 5|, respectively.
From a consideration of the foregoing and the accompanying drawing, it should be obvious that in accordance with this invention the end of a blade or the ends of a group of blades can be readily shrouded and provided with an intermediate or centrally disposed upstanding'and circumferentially extending sealing'flange I! (such a construction is impractical with blades having a centrally disposed tenon of the type heretofore employed) without in any manner weakening the connection between the end of the blade and the superimposed shroud and seal structure. In fact, the disclosed construction is much stronger than the tenoned constructions heretofore employed since, as clearly shown, a shroud and seal structure embodying the invention is secured or attached to the end of the blade by an effective bond area which is substantially equal to the area of the blade end, thereby materially reducing, and in some instances, entirely eliminating the cantilever effect produced by cantrifugal force acting on the free edges of shroud and seal strips which are secured to the end of a blade by a centrally disposed tenon.
Shrouding and sealing structures with multiple spaced sealing flanges can be readily built up in accordance with this invention more cheaply than has heretofore been possible with the prior art methods and the structures produced in accordance with this invention have excellent physical properties with respect to stress resistance and with respect to corrosion and erosion resistance. The invention is applicable to all types of turbine blading with respect to which it is necessary to employ a shrouding and sealing means and while the invention has been disclosed in connection with shrouding and sealing means adapted to span a series of blades, it should be understood that the invention is not in any manner limited to the exact mode of construction or to the exact constructions herein shown and described as various modifications within the scope of the appended claims may occur to persons skilled in the art.
It is claimed and desired to secure by Letters Patent:
1. A method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on said end and adjacent one edge thereof a first upstanding portion and having in said end adjacent its other edge a second upstanding portion of materially greater length than said first portion, placing on said end of the blade a first element of said structure apertured to receive said upstanding portions and having a thickness approximately equal to the length of said first portion, superimposing on said first element, a second element of said structure including a base apertured to receive said second portion and having a thickness approximately equal to the exposed length of said second portion and a width sufiiciently less than the width of said first element to leave exposed a part of said end of said first portion, and securing said first element and the base of said second element to the exposed parts of said first and second portions, respectively.
2. A method of forming a combined shroud and seal structure on the end of a blade member presenting in spaced upstanding relation, a first portion and a second portion of materially greater length than said first portion which comprises placing on said end of the blade a shroud element apertured to receive said upstanding portions and having a thickness approximately equal to the length of said first portion, superimposing on said shroud strip a seal element including a base apertured to receive said second portion and having a thickness approximately equal to the exposed length of said second portion and a width sufiiciently less than the width of said shroud element to leave exposed a part of the end of said first portion, and securing said shroud element and the base of said seal element to the exposed parts of said first and second portions, respectively.
3. A method of forming a combined shroud and seal structure on the end of a blade member presenting an upstanding stepped projection having its lower step disposed adjacent one edge of said blade and having its higher step disposed adjacent the other edge of said blade, which comprises placing on said end of the blade a shroud element apertured to receive said upstanding projection and having a thickness approximately equal to the height of said lower step, superimposing on said shroud strip a seal element including a base apertured to receive said higher step and having a thickness approximately equal to the height of said higher step and a width sufficiently less than the width of said shroud element to leave exposed a part of the top of said lower step, and securing said shroud element and the base of said seal element to the exposed parts of said lower and higher steps, respectively.
4. A method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on one end thereof juxtapositioned short and long tenon portions, placing on said one end of the blade a first element of said structure apertured to receive and expose the end parts of said short and long tenon portions, superimposing on said first element a second element of said structure including a base apertured to receive and expose the end part of said long tenon portion and having a width sufiiciently less than the width of said first element to leave exposed a part of the end of the short tenon portion, and securing saidfirst element and the base of said second element to the exposed end parts of said short and long tenon portions, respectively.
5. A method of forming a combined shroud and seal structure on the end of a blade which comprises providing a blade having on one end thereof juxtapositioned short and long tenon portions, placing on said one end of the blade a first element of said structure apertured to receive and expose the end parts of said short and long tenon portions and having a thickness approximately equal to the length of said short tenon portion, superimposing on said first element a second element of said structure including a base apertured to receive and expose the end part of said long tenon portion and having a thickness approximately equal to the exposed length of said long tenon portion and a width sufiiciently less than the width of said first element to leave exposed a part of the end of the short tenon portion, and fusibly uniting said first element and the base of said second element to the exposed end parts of said short and long tenon portions, respectively.
HANS P. DAI-ILSTRAND.
US356411A 1940-09-12 1940-09-12 Blade shrouding Expired - Lifetime US2350309A (en)

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US465672A US2350310A (en) 1940-09-12 1942-11-16 Blade shrouding

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2467168A (en) * 1944-07-05 1949-04-12 Sulzer Ag High-temperature turbomachine
DE1033678B (en) * 1954-12-21 1958-07-10 Maschf Augsburg Nuernberg Ag Shroud for flow machine blades
US2959393A (en) * 1956-04-16 1960-11-08 Gen Electric Turbine bucket cover assembly
US3173655A (en) * 1961-09-08 1965-03-16 Stalker Corp Bladed rotor
US20180094637A1 (en) * 2015-04-15 2018-04-05 Robert Bosch Gmbh Free-tipped axial fan assembly

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2467168A (en) * 1944-07-05 1949-04-12 Sulzer Ag High-temperature turbomachine
DE1033678B (en) * 1954-12-21 1958-07-10 Maschf Augsburg Nuernberg Ag Shroud for flow machine blades
US2959393A (en) * 1956-04-16 1960-11-08 Gen Electric Turbine bucket cover assembly
US3173655A (en) * 1961-09-08 1965-03-16 Stalker Corp Bladed rotor
US20180094637A1 (en) * 2015-04-15 2018-04-05 Robert Bosch Gmbh Free-tipped axial fan assembly
US10844868B2 (en) * 2015-04-15 2020-11-24 Robert Bosch Gmbh Free-tipped axial fan assembly
US20210095684A1 (en) * 2015-04-15 2021-04-01 Robert Bosch Gmbh Free-tipped axial fan assembly
US11499564B2 (en) * 2015-04-15 2022-11-15 Robert Bosch Gmbh Free-tipped axial fan assembly

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