US2350310A - Blade shrouding - Google Patents

Blade shrouding Download PDF

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US2350310A
US2350310A US465672A US46567242A US2350310A US 2350310 A US2350310 A US 2350310A US 465672 A US465672 A US 465672A US 46567242 A US46567242 A US 46567242A US 2350310 A US2350310 A US 2350310A
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blade
shroud
blades
base
members
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US465672A
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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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    • 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

Definitions

  • This invention relates to blade shrouding and more particularly to a built-up shroud and seal structure for the tip portions of turbine blades; the method of constructing same being fully disclosed and claimed in applicant's, copending application Serial No. 356,411, filed September 12, 1940, of which this application is a division.
  • the primary object of this invention is to provide 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 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.
  • Fig. 1 is a partial sectional view of a turbine spindle and stator having coasting blades embodying the invention
  • Fig. 2 is a plan view of a portion of a moving blade row taken on line II-H 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 sealing 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; I
  • 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 grouper blades preparatory to welding the structure theretoJ
  • Fig. 1 of the drawing it is seen that the invention is shown as applied to the-itationary and moving blades l and 2, respectively,
  • a stepped projection comprising avrelatively short portion II which ismade approximately equal in length. to the thickness of, the shroud member to be secured tothe bladetip and a relatively long portion l2 .whichjfis made approximately equal in length. to twice the thick ness of the said shroud member.
  • the shrouding and sealing means comprise a first member having a base or shroud portion i3 and an up standing sealing flange i4 and ase cond channel shaped member having af base or Web portion l5 of less width than the base portiOnQlt of the first member and presentingwhen-mounted, on the tip portion of a blade pair ol laterally spaced upstanding sealing fianges'l'l- Th'ebase portion l3 of thei'lrst member is providedwitli an opening l8 adaptedto snugly receive the stepped projection .and thebase member .jl'fiv of 'the'sfe'cond member is also provided with an opening 1.!) adapted to snuglyreceiv the relatively long tion 12 of the said.
  • the dimensions of the first and secondme'mbers, the arrangementof the openings 18 and ⁇ !!! therein, respectively; and the dimensions and the arrangement of the stepped projection are such that when the first and second'members are po- .sitioned on the. tip portionlof a 'bladej'in the order named, the shrouding and. sealing mean are arranged as shown .in Fig. 5.]f'1he thickness of the base or web portion 16 for, thef'second member is substantially the samei'jas,,the thick- 'ness of the base or shroud, portion l3'of the first member. Consequently, since thelength of'the portions H and I2 or the stepped projection is approximately equal to the thicknessand totwjice the, thickness of the shroud portion" l3, respep a commercially practical construction.
  • first and second members When the first and second members are dimen- I2 of the sloned to span a series of blades asindicated in 1 Fig. 2, the said members are positioned on and welded or otherwise secured to the blades afterthey have been mounted on the turbine rotor or stator. Any suitable means may be employed for holding said members in-their proper assembled relation during the welding operation and in this connection apparatus somewhat similar to that shown in Fig. 10 has been found entirely satisfactory.
  • the length of the projection 22 is approximately equal to the thickness of the base or shroud portion 13 of the first member and the length of the projection 23 is approximately equal to the combined thickness of the base or shroud member I 3 of the first member and the baseor web portion I6 01 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 portionsof the blades and welded thereto in exactly the same manner as setforth 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 space 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 portions H and I2 similar to those shown in Figs. 3-5, inclusive.
  • These segmental blade groups are formed in a known manner-by'casting or otherwise securing the blades 28 in a common base member 29 to form a unitary structure of the general form indicated.
  • the base member 23 may be made in any desired or preferred shape in order to facilitate mounting and securing the segmental blade group on the turbine rotor or stator, and that. shown is merely illustrative Inf T e shroudlng and sealing means to be secured toeach such group of blades is of course identical to that disclosed in connection with Figs.
  • the first and second members comprising the shrouding and sealing means are preferably secured to the individual groups before they are mounted on the turbine bers 34 and 36 having edge portions 31 and 38, respectively, adapted to coact with the flanges l4 and 2! of thefirst member and with the flanges ll of the second member, spacing members 39 and 4
  • is merely illustrative of a commercially 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 web portion 44 of the first member constitutes the shroud portion and the channels 46 sealing flanges.
  • the base member 41 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 fiange 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 centrifugal force acting on the freeedges 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 blade structure embodying shroud and seal members comprising a blade having on one end thereof juxtapositioned short and long tenon portions, a first element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said short and long tenon portions, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a width sufficiently less than the width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and means securing said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
  • a blade structure embodying shroud and seal members comprising a blade having on one end thereof juxtapositioned short and long tenon portions, a first element disposed on said blade end and being apertured to receive and aocessibly expose the end parts of said short and long tenon portions, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a width suiiiciently less than the width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and weld metal fusibly uniting said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
  • a blade structure embodying shroud and seal members comprising a blade having on an end thereof adjacent one of its edges a first upstanding tenon portion and having on said end adjacent its other edge a second upstanding tenon portion of greater length than said first portion, a first element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said short and long tenon portion, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a Width sufficiently less than the Width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and means securing said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
  • a blade structure embodying shroud and seal members comprising a blade having on one end thereof a pair of spaced, upstanding tenon portions of different length, a shroud element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said tenon portions, a seal element having a base portion superimposed on said shroud element, said base portion being apertured to receive and accessibly expose the end'part of the longer one of said tenon portions and having a width sufficiently less than the width of said shroud element to leave exposed and accessible a part of the end of the short tenon portion, and means securing said shroud element and the base portion of said sealelement to the exposed and accessible end parts of said short and long tenon portions, respectively.
  • a blade structure embodying shroud and seal members comprising a blade having on one end thereof 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, a shroud element disposed on said blade end and being apertured to receive and accessibly expose said projection, a seal element having a base portion superimposed on said shroud element, said base portion being apertured to receive and accessibly expose said higher step and having a width sufficiently less than said shroud element to leave exposed and accessible a part of the top of said lower step, and means securing said shroud element and the base portion of said seal element to the exposed and accessible parts of said lower and higher steps, respectively.

Description

y 30,1944. H. P. DAHLS'TRAQD 2,3 0,310
BLADE SHROUDING Original Filed Sept. 12, 1940 Patented May 30, 1944 .BLADE SHROUDING Original application September 12, 1940, Serial No. 356,411. I Divided and this application November 16, 1942, Serial No. 465,672
Claims.
' This invention relates to blade shrouding and more particularly to a built-up shroud and seal structure for the tip portions of turbine blades; the method of constructing same being fully disclosed and claimed in applicant's, copending application Serial No. 356,411, filed September 12, 1940, of which this application is a division.
The primary object of this invention is to provide 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 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.
The invention accordingly consists of the various features of construction, combinations ofelements 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 coasting blades embodying the invention; I
Fig. 2 is a plan view of a portion of a moving blade row taken on line II-H 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 sealing 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; I
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 grouper blades preparatory to welding the structure theretoJ Referring to Fig. 1 of the drawing, it is seen that the invention is shown as applied to the-itationary 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 removablysecured in circumferentially extending grooves ,8 and 9 in the stator and rotor, respectively, inthe 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 thepresent invention.
Referring to Figs. 2-5 inclusive, ibis seen that the tip portions of the blades 2- a: e shaped, to
provide a stepped projection comprising avrelatively short portion II which ismade approximately equal in length. to the thickness of, the shroud member to be secured tothe bladetip and a relatively long portion l2 .whichjfis made approximately equal in length. to twice the thick ness of the said shroud member. The shrouding and sealing means comprise a first member having a base or shroud portion i3 and an up standing sealing flange i4 and ase cond channel shaped member having af base or Web portion l5 of less width than the base portiOnQlt of the first member and presentingwhen-mounted, on the tip portion of a blade pair ol laterally spaced upstanding sealing fianges'l'l- Th'ebase portion l3 of thei'lrst member is providedwitli an opening l8 adaptedto snugly receive the stepped projection .and thebase member .jl'fiv of 'the'sfe'cond member is also provided with an opening 1.!) adapted to snuglyreceiv the relatively long tion 12 of the said. projection. The width'o' base portion I 3 oithe firstn emb'er issu'ch that when the first member is positioned onthelbladc tip as shown in Fig.v 5, an edgeportiori' oi'said base member extends beyond and overhangs-the edge of the blade, thereby providing 'a laterally extending sealingfiange 2|. v v
The dimensions of the first and secondme'mbers, the arrangementof the openings 18 and}!!! therein, respectively; and the dimensions and the arrangement of the stepped projection are such that when the first and second'members are po- .sitioned on the. tip portionlof a 'bladej'in the order named, the shrouding and. sealing mean are arranged as shown .in Fig. 5.]f'1he thickness of the base or web portion 16 for, thef'second member is substantially the samei'jas,,the thick- 'ness of the base or shroud, portion l3'of the first member. Consequently, since thelength of'the portions H and I2 or the stepped projection is approximately equal to the thicknessand totwjice the, thickness of the shroud portion" l3, respep a commercially practical construction.
tively, 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 l I will be nearly flush with the top surface of the base or shroud portion l3 and the top of the portion I2 will be nearly fiush with the top surface of the base or web portion l6. 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 preferably to weld or otherwis secure the base portions of the first and second members to the juxtapositioned portions H and stepped projection as indicated .in Figs. 1, 2 and 5. When the first and second members are dimen- I2 of the sloned to span a series of blades asindicated in 1 Fig. 2, the said members are positioned on and welded or otherwise secured to the blades afterthey have been mounted on the turbine rotor or stator. Any suitable means may be employed for holding said members in-their proper assembled relation during the welding operation and in this connection apparatus somewhat similar to that shown in Fig. 10 has been found entirely satisfactory.
' The modified arrangement shown in Figs. 6-8, inclusive, in which like numerals are used to designate the same 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 upstanding projections 22 and "23, and in that the base or shroud portion l3 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 13 of the first member and the length of the projection 23 is approximately equal to the combined thickness of the base or shroud member I 3 of the first member and the baseor web portion I6 01 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 portionsof the blades and welded thereto in exactly the same manner as setforth 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 space 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 portions H and I2 similar to those shown in Figs. 3-5, inclusive. These segmental blade groups are formed in a known manner-by'casting or otherwise securing the blades 28 in a common base member 29 to form a unitary structure of the general form indicated. The base member 23 may be made in any desired or preferred shape in order to facilitate mounting and securing the segmental blade group on the turbine rotor or stator, and that. shown is merely illustrative Inf T e shroudlng and sealing means to be secured toeach 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 turbine bers 34 and 36 having edge portions 31 and 38, respectively, adapted to coact with the flanges l4 and 2! of thefirst member and with the flanges ll of the second member, spacing members 39 and 4|, 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 commercially 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 dilTers 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 41 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 fiange 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 theend 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 fiange 11 (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 centrifugal force acting on the freeedges 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 blade structure embodying shroud and seal members comprising a blade having on one end thereof juxtapositioned short and long tenon portions, a first element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said short and long tenon portions, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a width sufficiently less than the width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and means securing said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
2. A blade structure embodying shroud and seal members comprising a blade having on one end thereof juxtapositioned short and long tenon portions, a first element disposed on said blade end and being apertured to receive and aocessibly expose the end parts of said short and long tenon portions, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a width suiiiciently less than the width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and weld metal fusibly uniting said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
3. A blade structure embodying shroud and seal members comprising a blade having on an end thereof adjacent one of its edges a first upstanding tenon portion and having on said end adjacent its other edge a second upstanding tenon portion of greater length than said first portion, a first element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said short and long tenon portion, a second element having a base portion superimposed on said first element, said base portion being apertured to receive and accessibly expose the end part of said long tenon portion and having a Width sufficiently less than the Width of said first element to leave exposed and accessible a part of the end of said short tenon portion, and means securing said first element and the base portion of said second element to the exposed and accessible end parts of said short and long tenon portions, respectively.
4. A blade structure embodying shroud and seal members comprising a blade having on one end thereof a pair of spaced, upstanding tenon portions of different length, a shroud element disposed on said blade end and being apertured to receive and accessibly expose the end parts of said tenon portions, a seal element having a base portion superimposed on said shroud element, said base portion being apertured to receive and accessibly expose the end'part of the longer one of said tenon portions and having a width sufficiently less than the width of said shroud element to leave exposed and accessible a part of the end of the short tenon portion, and means securing said shroud element and the base portion of said sealelement to the exposed and accessible end parts of said short and long tenon portions, respectively.
5. A blade structure embodying shroud and seal members comprising a blade having on one end thereof 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, a shroud element disposed on said blade end and being apertured to receive and accessibly expose said projection, a seal element having a base portion superimposed on said shroud element, said base portion being apertured to receive and accessibly expose said higher step and having a width sufficiently less than said shroud element to leave exposed and accessible a part of the top of said lower step, and means securing said shroud element and the base portion of said seal element to the exposed and accessible parts of said lower and higher steps, respectively.
HANS P. DAHLSTRAND.
US465672A 1940-09-12 1942-11-16 Blade shrouding Expired - Lifetime US2350310A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459850A (en) * 1945-12-10 1949-01-25 Westinghouse Electric Corp Turbine apparatus
US2640679A (en) * 1950-03-21 1953-06-02 Gen Motors Corp Turbine or compressor stator ring
US2749026A (en) * 1951-02-27 1956-06-05 United Aircraft Corp Stator construction for compressors
US2956733A (en) * 1954-09-28 1960-10-18 Stalker Corp Fluid turning wheels for compressors
US2963268A (en) * 1957-03-25 1960-12-06 Gen Electric Pressurized seal
US5035578A (en) * 1989-10-16 1991-07-30 Westinghouse Electric Corp. Blading for reaction turbine blade row
US20170002659A1 (en) * 2015-07-01 2017-01-05 United Technologies Corporation Tip shrouded high aspect ratio compressor stage
US20180094637A1 (en) * 2015-04-15 2018-04-05 Robert Bosch Gmbh Free-tipped axial fan assembly

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459850A (en) * 1945-12-10 1949-01-25 Westinghouse Electric Corp Turbine apparatus
US2640679A (en) * 1950-03-21 1953-06-02 Gen Motors Corp Turbine or compressor stator ring
US2749026A (en) * 1951-02-27 1956-06-05 United Aircraft Corp Stator construction for compressors
US2956733A (en) * 1954-09-28 1960-10-18 Stalker Corp Fluid turning wheels for compressors
US2963268A (en) * 1957-03-25 1960-12-06 Gen Electric Pressurized seal
US5035578A (en) * 1989-10-16 1991-07-30 Westinghouse Electric Corp. Blading for reaction turbine blade row
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
US20170002659A1 (en) * 2015-07-01 2017-01-05 United Technologies Corporation Tip shrouded high aspect ratio compressor stage

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