US1061648A - Blades. - Google Patents
Blades. Download PDFInfo
- Publication number
- US1061648A US1061648A US57924710A US1910579247A US1061648A US 1061648 A US1061648 A US 1061648A US 57924710 A US57924710 A US 57924710A US 1910579247 A US1910579247 A US 1910579247A US 1061648 A US1061648 A US 1061648A
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- US
- United States
- Prior art keywords
- blades
- blade
- mounting
- face
- row
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000010276 construction Methods 0.000 description 2
- 101100001674 Emericella variicolor andI gene Proteins 0.000 description 1
- 235000017276 Salvia Nutrition 0.000 description 1
- 241001072909 Salvia Species 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
Images
Classifications
-
- 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
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
-
- 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
- Patentedll Iay 13, 1913 Patentedll Iay 13, 1913.
- My invention relates to blading andparticula-rly to turbine blading,- k
- An object of my invention is to produce a new and improved blading and also new and I improved means for assembling and mountin'gblades.
- Figure l is a'perspective -viewof bladingembodyin'g my Invention shown; in connection With'a' portion .ofa 'blademoimting elementj.
- Figs; 2. and 3 are.
- I group'of blades taken alongthe longltud mal perspective views-of blades embody ng my Fig, 4 is atransverse section of a axes of the blades and illustratesa modifica f tio'n'ofmy invention.
- blades isre-directedtan d re-delivered to the "blades: I do not desire to limitthe ap plication of myinventipn to blades for thls type nor to the arrangement. or. con
- the blades are assembled n a. row.
- the mounting 1 tongue 14 isadapted to. fit-snugly into a slot ,15' formed in a mounting element 16, andeach blade is 'rigidly' and positivel secured a of rivets 17, which n versely extending ⁇ holes 18 provided'.' in the .tonguel of each blade and gistering holes 1 [-19 provided in the blade mQlIIIiGLDF
- the over-portlqnso v shrouding flange 6 provided at theend of each blade projects laterally beyond the convex face of the blade in the same'direct-ion I as the spacingpiece 95 and is provided" with a convex edgeadapted to engage the concave next'adjacent blade and to 00- blades to form a shroud forthe row ofhlades' whenithe blades are assembled in a row.
- Th-Ipins 12 fit snugly into the holes 11 and are so arrangedjth'at' theseparate segments-may be -lblade: mount ng element.v into anorgamzed row, 'in'which thepins 1 2 all codperate.
- the mounting portion 5 ofieach blade is Y piece of metal, the spacl'ng piece9 and the base portion fi-being the -,milling operation.
- the mounting portion consists of a shoulder 13 and-a narrow-tongue 14.-which projects'coj the body portion'ofthe blade. 'The'shoulder'i13-is soiiconstru'cted that it co; operates with the concave face. of I the next jacent blade andiiorms a spacing piece be ends of the blades, The
- each blade maybe milled out of a single fiangefi, the intermediate v pert esjs 1tsrmaes;m5 'sideof the -ton'guei e ⁇ couldffte Q-thinner: and; Sign the 1410 a'hla ea e pfiejdei' enmt W fl l'.
- blades togethe v o g I the bladesishowninrFig. 4 issimilar to. that 6.
- constructions I may find it preferable to rovnde two binding members 22 in place M the single member illustrated, since the flanges Copies 9! this patent may be obtained .for five cents each, by addressing the Commissioner of Peter" Washington, D. G.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
G. WESTINGHOUSE.
BLADES.
' APPLIoAflon nun AUG.'27,1910.
Patentedll Iay 13, 1913.
s ATTORNEY 1'11 FACT.
a ononen WESTINGHOUSE, on PITTSBURGH, PENNSYLVANIA.
f Application filed August 27, 1911;.- Seria1No..ti79 ,247.
Specification of Letters Patent.
, Patented May 1351913.
To all 'wlmm it may concern v Be iti known that I; 'GEORGE W'Esfrmo- HOUSE, a citizen'of-the United States, and a resident of Pittsburgh, in .the county of Allegheny and State'o'f Pennsylvania, have made a newand useful-Invention in Bladesf and Means for- Mounting Blades of which.-
- the following is a Specification.
My invention relates to blading andparticula-rly to turbine blading,- k An object of my invention is to produce a new and improved blading and also new and I improved means for assembling and mountin'gblades. w
. These and other-objects I attain by means of the blades and bIading illustrated inthe drawings accompanying.thisapplication and.
- forming a part thereof.-
In the" drawings, Figure l is a'perspective -viewof bladingembodyin'g my Invention shown; in connection With'a' portion .ofa 'blademoimting elementj. Figs; 2. and 3 are.
invention; I group'of blades taken alongthe longltud mal perspective views-of blades embody ng my Fig, 4 is atransverse section of a axes of the blades and illustratesa modifica f tio'n'ofmy invention.
. For'convenienceof' descripti'bn, -I have illustrated my invention m'connection with bla'des adaptedto be employed-in a turbine,
in which motive. fluid is delivered to a row of blades, 'andafter having traversed the of turbine,
blades isre-directedtan d re-delivered to the "blades: I do not desire to limitthe ap plication of myinventipn to blades for thls type nor to the arrangement. or. con
struction' illustrated, .andI desire-it to be 'understood that the drawingsar'e merely tee- 1mm:-
illus'trative-and' that various changes and modifieationsimay be made wlthout departthesplrit andscope of my inven- Referring a5 the drawi ngsf'each blade illustrated 6. The body portion islsubstantially cres-.--'
consists of a body portion 4", a" mounting portion 5-,.and a shroudin'g flange I cent shaped in cross section, being'provided; on one side Witconcave .workmg face-"7 v i and on the other side with a' convex working face 8. The oonjv'iex face i's divided into two portions by an intermediate spacing piece 9,, I which is formed integrally with the body portion of-the blade and which is provided with a convex face 10 adapted to en age the concave face oithe next adjacent bla again;
the blades are assembled n a. row.
. face of the operate with the flanges 6 of all the-other through the body portion of-theblades and assembled on the.
formed by axially with tween the mounting 1 tongue 14 isadapted to. fit-snugly into a slot ,15' formed in a mounting element 16, andeach blade is 'rigidly' and positivel secured a of rivets 17, which n versely extending}holes 18 provided'.' in the .tonguel of each blade and gistering holes 1 [-19 provided in the blade mQlIIIiGLDF The over-portlqnso v shrouding flange 6 provided at theend of each blade projects laterally beyond the convex face of the blade in the same'direct-ion I as the spacingpiece 95 and is provided" with a convex edgeadapted to engage the concave next'adjacent blade and to 00- blades to form a shroud forthe row ofhlades' whenithe blades are assembled in a row.
I contemplate assembling the bladesinto short segments prior to mounting-them on the'blade carry-fngelement, and 'to thisend I provide holes 11, which extend transversely the intermediate spacing pi'eces 9. I then assemblei several blades ton a binding member or pin12, which are shaped and'extends" through'th'e holes 11 in the blades. Th-Ipins 12 fit snugly into the holes 11 and are so arrangedjth'at' theseparate segments-may be -lblade: mount ng element.v into anorgamzed row, 'in'which thepins 1 2 all codperate. to hold the blades in placeand to laterally strengthen-the row ofiblades, I accomplish this byso arranging the ins mt-hat: they project beyond thel'ast bla eof s m nt at one end of the Se ment and dO'IlOt extnd'entirely throu h the final bladeat theother end of the segment. With this arrangementthe 1 projecting end ofthe pin of one segment extends into the:
hole..l 1 ofthe adjacent blade of the next; segment when thesegments are assembled in an annularrow. 1
The mounting portion 5 ofieach blade is Y piece of metal, the spacl'ng piece9 and the base portion fi-being the -,milling operation. The mounting portion consists of a shoulder 13 and-a narrow-tongue 14.-which projects'coj the body portion'ofthe blade. 'The'shoulder'i13-is soiiconstru'cted that it co; operates with the concave face. of I the next jacent blade andiiorms a spacing piece be ends of the blades, The
in place on the mountmgelementy means extend through transelement" a formed integrally with the bodylportion; 'in fact, each blade maybe milled out of a single fiangefi, the intermediate v pert esjs 1tsrmaes;m5 'sideof the -ton'guei e} couldffte Q-thinner: and; Sign the 1410 a'hla ea e pfiejdei' enmt W fl l'.
strength of bindingTmember could"- to; secure the'blades'. ofl' agrowag'ainst lateral working' passages'andagbindingmember'ex limotion." In: addition"tof'thigtthe pins 12 jtending,through-the bladesj-andrsai'd' meansi-zg firmly-thefbladesofeachsegment and ;-4}=In'combinationcwith 'ablade-mounting:
36] a a ldirectlonsjiiijthel blades illustrated" in the element, at'plurality of bladesprovided with ateral-istiffnessfjef- Having; t di'n place onv-the" What .1;A7lblzide PT S i g- '3 I .v thl-i 'in me eti pa'cingfi -pie e's' Zloca'ted between the ends' of j he bladesfand -fornied-. integrally therewith elinixtft' respe I 1=ljocatingthe bladesr. i n'...th ounting element gor, the g'blfade.
- andlS-drill'ed 2. Ablade-segmentcomprising-I pluralv 2' f{ntj'lof bla'desymeansformedintegrallyfitith J J 3 pparent-{thatthe; blades are l the-blades ford-iridingthe' passagesf between.
ach endfand at- -an'--;intermediate. =1-tl1e-blades'into' two 'sets of workingifpassages 7o po t ,etween'itheir'l'endsfwhen' theyarefin' and a binding member pnssfingthroughsaid, "Iilflfij an the; blade' mounting element and {means for securingzjthe,blades 'together;
that the jfianges' 16, the fintermedjiate is'pacing' :f 3. A blade segment .comprifsi-ng afplumb and 1 the base-portions '5' co6perate: ".ityfofblades, manger dividing t-hepas- E";
thithel jeoncave iace'spf. theladj aeent' blades 5 sages "between the blades into two? sets of-fl organized structure, andedd to the lateral mounting p'ortiopS,j-' and shro ding; flflan'gesj II ifin s ix h 'il d s;.gThe" intermediate vloca at 0PP 1 i ofrth blades n pacing:ipice 9, in addition to spa'cing the 'means extendingthroughfthebladesQ'andh v d r es divide. the--"1assages;between the located betWeensaid-flange's and saidr n( unt- Iade intoitwo. sets (if-working liassages mg p r -i n for se uringth mqtogether;-.-'--
h which'th'e fiiiid flo'wsid-opposite 5. Infcombinationiiiith a blademounting ."draiwings." The-flangesj fi, spacing pieces" 9- integrally formed spacingpieceslo cated"at a jd-fthesshoulderf13oftheblades are preftheir outer flor-free ends, and intermedia't ej ereb1 l sp-{formed that theblajdes' occupy- 'spacing pieces' located bet'wee n'ther outer ends a 1 rad iapositions when 'assembled'in segments. and themounting'end's ofthe b'lades; means In -F .ig.' ij4 I [have ';illust-ra ted."blades" in :for securing-said blades to'said mounting ele-' w jthef'shroudingiflangesti are-provided ment-"anda binding member extending with.holes flIfthrougli which-a binding memthrough said spacing pieces for securing the of theblades-shown in Figs-1,2 and 3. I
bet pi1122feirtends. The construction of blades togethe v o g I the bladesishowninrFig. 4 issimilar to. that 6. In combinatlon With a blade mounting '95 element, a plurality of blades,- a binding- 7 It. i11 b nt th t, th t r d member extending. through the outer or free "of theblades maybe flanged and secured toends of the blades, means for securing said I gether wi-thout the necessity of providing blades to said mounting element-and a bindthe intermediatespacing pieces 9,"and withing mem er x en ing r gh h bl des I00.
I out thejnecessity of providing intermediate and loc edbe we s d o n i g me ns binding member 01' pin 12. .Itwill alsofbe and said first mentioned binding member.
apparent that I may employ two u mo e 5 In testimony whereof, I have hereunto binding members 22 at" the outer ends of subscri y n m thlS 23rd day Of the blades, or that I may employ'two or August, 1910., moreplns 12 extending through'the inter- I medlate portions of the blades. With some GEO. WESTINGHOUSE.
Witnesses:
C. W. MOGHEE, E. W. McCALnIs'rEn.
constructions I may find it preferable to rovnde two binding members 22 in place M the single member illustrated, since the flanges Copies 9! this patent may be obtained .for five cents each, by addressing the Commissioner of Peter" Washington, D. G.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US57924710A US1061648A (en) | 1910-08-27 | 1910-08-27 | Blades. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US57924710A US1061648A (en) | 1910-08-27 | 1910-08-27 | Blades. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1061648A true US1061648A (en) | 1913-05-13 |
Family
ID=3129894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US57924710A Expired - Lifetime US1061648A (en) | 1910-08-27 | 1910-08-27 | Blades. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1061648A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2440069A (en) * | 1944-08-26 | 1948-04-20 | Gen Electric | High-temperature elastic fluid turbine |
| US2454115A (en) * | 1945-04-02 | 1948-11-16 | Allis Chalmers Mfg Co | Turbine blading |
| US2500745A (en) * | 1944-09-21 | 1950-03-14 | Gen Electric | Bucket structure for high-temperature turbomachines |
| US2603453A (en) * | 1946-09-11 | 1952-07-15 | Curtiss Wright Corp | Cooling means for turbines |
| DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
| US4699569A (en) * | 1985-07-05 | 1987-10-13 | Bbc Brown, Boveri & Company, Limited | Rotor blade ring of an axial flow turbomachine |
| US4840539A (en) * | 1987-03-12 | 1989-06-20 | Alsthom | Moving blading for steam turbines |
| US5238366A (en) * | 1992-07-06 | 1993-08-24 | Westinghouse Electric Corp. | Method and apparatus for determining turbine blade deformation |
| US20120020793A1 (en) * | 2009-01-29 | 2012-01-26 | Mccracken James | Turbine blade system |
| US20190017393A1 (en) * | 2015-07-20 | 2019-01-17 | Nuovo Pignone Tecnologie Srl | Unshrouded turbomachine impeller with improved rigidity |
| US10385702B2 (en) * | 2015-06-30 | 2019-08-20 | Napier Turbochargers Ltd | Turbomachinery rotor blade |
| US11428106B2 (en) * | 2017-09-20 | 2022-08-30 | Sulzer Management Ag | Assembly of vane units |
-
1910
- 1910-08-27 US US57924710A patent/US1061648A/en not_active Expired - Lifetime
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2440069A (en) * | 1944-08-26 | 1948-04-20 | Gen Electric | High-temperature elastic fluid turbine |
| US2500745A (en) * | 1944-09-21 | 1950-03-14 | Gen Electric | Bucket structure for high-temperature turbomachines |
| US2454115A (en) * | 1945-04-02 | 1948-11-16 | Allis Chalmers Mfg Co | Turbine blading |
| US2603453A (en) * | 1946-09-11 | 1952-07-15 | Curtiss Wright Corp | Cooling means for turbines |
| DE1551173B1 (en) * | 1966-06-21 | 1971-07-08 | Rolls Royce | DEVICE FOR VIBRATION DAMPING ON FREE-STANDING BLADES OF FLOW MACHINERY |
| US4699569A (en) * | 1985-07-05 | 1987-10-13 | Bbc Brown, Boveri & Company, Limited | Rotor blade ring of an axial flow turbomachine |
| US4840539A (en) * | 1987-03-12 | 1989-06-20 | Alsthom | Moving blading for steam turbines |
| US5238366A (en) * | 1992-07-06 | 1993-08-24 | Westinghouse Electric Corp. | Method and apparatus for determining turbine blade deformation |
| US20120020793A1 (en) * | 2009-01-29 | 2012-01-26 | Mccracken James | Turbine blade system |
| US8894353B2 (en) * | 2009-01-29 | 2014-11-25 | Siemens Aktiengesellschaft | Turbine blade system |
| US10385702B2 (en) * | 2015-06-30 | 2019-08-20 | Napier Turbochargers Ltd | Turbomachinery rotor blade |
| US20190017393A1 (en) * | 2015-07-20 | 2019-01-17 | Nuovo Pignone Tecnologie Srl | Unshrouded turbomachine impeller with improved rigidity |
| US10669864B2 (en) * | 2015-07-20 | 2020-06-02 | Nuovo Pignone Srl | Unshrouded turbomachine impeller with improved rigidity |
| US11428106B2 (en) * | 2017-09-20 | 2022-08-30 | Sulzer Management Ag | Assembly of vane units |
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