US1694481A - Propeller-type turbine or pump - Google Patents

Propeller-type turbine or pump Download PDF

Info

Publication number
US1694481A
US1694481A US121787A US12178726A US1694481A US 1694481 A US1694481 A US 1694481A US 121787 A US121787 A US 121787A US 12178726 A US12178726 A US 12178726A US 1694481 A US1694481 A US 1694481A
Authority
US
United States
Prior art keywords
runner
blades
wall
clearance
blade
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
Application number
US121787A
Inventor
Moody Lewis Ferry
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US121787A priority Critical patent/US1694481A/en
Application granted granted Critical
Publication of US1694481A publication Critical patent/US1694481A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03BMACHINES OR ENGINES FOR LIQUIDS
    • F03B11/00Parts or details not provided for in, or of interest apart from, the preceding groups, e.g. wear-protection couplings, between turbine and generator
    • F03B11/006Sealing arrangements
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Definitions

  • the object of this invention is to provide means for reducing the clearance between the periphery of the runner and the outer wall so as to increase the efliciency and to improve the operation of the turbine.
  • a further obj ect'of the invention is to provide means for preventing breakage of the runner blades when any foreign material or obstructionv passes within the clearance between the runner and the outer wall, or if the blades should touch the wall.
  • FIG. 1 is a plan view on section A-A of the turbine shown in Fig. 2 embodying the invention
  • Fig. 2 is an enlarged sectional elevation through a hydraulic turbine showing the runner and the surrounding parts;
  • Fig. 3 is an enlarged sectional view of an edge or tip of a runner blade
  • Figs. 4 and 5 show other arrangements for fastening thematerial to the runner tips
  • Fig. 6 is an enlarged sectional elevation through a hydraulic turbine showing the runner and the surrounding parts with an adjliistable rubber lined ring in the stationary wa
  • Fig. 7 is an enlarged sectional elevation showmg an adjustable metal ring in the stationar wall and runner blades tipped with yielda le material.
  • the tip of the blades are provided with a strip of rubber or other material of a relativel soft or ielding nature 15 which is cemente molded vulcanized or mechanically fastened to the metal.
  • the metal tip of the blade 11 is provided with a flange 16, around which the rubber is secured so as to provide the blade with a continuous smooth surface, the rubber being ground to merge with the metal surface.
  • the rubber strip is secured to the tip of the blade by cementing, molding or vulcanizing, the rubber is further ground down to fit the clearance space, substantially eliminating the clearance between the runner and the outer casting 17
  • the grinding is accom; plished with the ordinary portable grinder, the runner mounted for rotation on a boring mill I or rotating table.
  • the blades are ground to fit the required shape of the outer casting, which is usually conical or cylindrical or formed with a circular arc in meridian section.
  • the rubber tip of the blades closely spaced from the casting 17 will yield if for any reason foreign material, obstructions or trash enters the turbine casing.
  • the obstruction if small enough to enter the clearance space will pass through to the draft tube without causing breakage of the runner blade.
  • Tne use of rubber tipped runner blades increases the efficiency because it makes possible the provision of very small clearance between'thc runner blades and the surrounding wall, and therefore permits little leakage of water to pass between the runner and the stationary wall.
  • the leakage which occurs when there is considerable clearance is objectionable not only on account of the direct loss of useful flow, but also from the disturbance which it causes in the adjacent flow near the bladetips.
  • Fig. 4 shows another modification of the invention in which the yielding material 15 is dovetailed into the tip of the runner blade and projects beyond the metal portion of the blade to form a close seal between the surrounding wall and the blade.
  • Fig. 5 shows a further modification in which the strip of yielding material 15 is held mechanically in place in the tips of the runner blades.
  • This strip may be made of rubber or material of like nature or might be made of wood or of soft metal, such' as lead or babbitt.
  • the metal should be soft enough llvi that it would wear down if therunner touched the surrounding wall without scorlng or -1njuring the latterin any we
  • the blades 11 are provided with' removable plates 18 which are held in lace by means of screws 19 tapped into the b ades.
  • a modification ofthe invention is shown wherein an adjustable ring 20 having a rubber lining 21 is set into a circular open ing 22 in the casting 17
  • the ring 20 is held in position b screws or bolts 28 tapped into the casting 1 at 24. These bolts are in recesses 25 filled with type metal finished flush with the wall surface. If the ring 20 or the blade tips become worn or if the ring needs adjustment to decrease the clearance between the wall and the runner blades 11, the type vided with a yielding means at its tip for reducin clearance between the runner and the walfi 5.
  • the combination with an outer stationary wall, of a 'runner having a central hub ortion and a plurality .of blades, and means or adjusting the clearmetal 26 can be melted out of the recesses, the
  • Fig. 7 shows a modification wherein the blade tips are provided with rubber and the casting 17 is provided with an adjustable clearance ring 27.
  • I claim 1 In a runner for a turbine or pump the combination with a central hub portion, of a circumferential series of unshrouded blades thereon normally having a fixed relation thereto, each blade being provided with yielding means at its tip for reducing clearance and increasing the efliciency of the runner.
  • a rotary hydraulic machine the combination with an outer stationary wall, of a runner having a central hub ortion and a plurality of blades all dispose substantially in a plane normal to the runner axis, said blades having normally an immovable relation to said hub, the clearance space between said wall and said runner blades being provided on one' side with a rigid material and on 1the opposite side with a yieldable mater1a 8.
  • the combination with an outer stationary wall, of a runner having a central hub portion and a plurality of blades the clearance space between said wall and said runner blades being provided on one side with a rigid material and on the opposite side with a yieldable material, and means for adjusting the clearance between said wall and said blades.
  • a runner having a plurality of unshrouded blades and a circular and concentric stationary surroundin wall,'said blades at their tips being closely isposed to said wall with small running clearance therebetween and eachv blade being provided with yieldable means at its tip to permit the provision of said small bination of a runner having a plurality of unshrouded blades and a stationary surrounding wall, said blades at their tips being closely disposed to said wall with small running clearance therebetween, said wall having a generally conical shape smaller at one end than the other, and means for effecting relative axial adjustment between said runner and the portion of said wall adjacent the runner to provide adjustment of the clearance between said wall and runner.
  • a runner havin a plurality of unshrouded blades and a circufir and concentric stationary surrounding wall, said blades at their tips being closely disposed to said wall with small running clearance therebetween, the clearance s ace between the blade tips and stationary wa lhavingyieldable material on one side thereof and r1g1d material on the other side.
  • a runner having a plurality of unshrouded blades having during normal operation a fixed relation to the runner hub and an outer stationary wall extending in an axial direction and coaxial with said runner, said blades at their tips being disposed closely to said wallwith small running clearance therebetween, and each blade being provided with yieldable means at its tip to permit the provision of said small clearance.

Description

Dec. 11, 1928.
L. F. MOODY PROPELLER TYPE TURBINE OR PUMP Filed July 12, 1926 2 Sheets-Sheet 1 anoantoz Ill/1100a? Zen i4 351 M45 Stigma/54 Dec. 11, 1928.
L. F. MOODY PROPELLER TYPE TURBINE OR PUMP.
Filed July 12, 1926 2 Sheets-Sheet 2 m w W u 0 m m E F. f i .w W 1% 6 m Z fl WW 8 My MM 2 w ,//,v////// V/ P\ a a g ,,/M//
Patented Dec. 11, 1928.
UNITED STATES :PATENT' OFFlCE.
LEWIS FERRY MOODY, OF PHIIIAD ELPHIA, PENNSYLVANIA.
PBOPELLEB-TYPE TUERBINE OB PUMP.
Application filed July 12, 1926. Serial N0. 121,787.
surrounding wall to allow clearance between the periphery of the runner and the wall. This clearance which in some installations, usually of the larger propeller type runners, is considerable, causes loss of efliciency. The
. clearance must be suflicient to prevent the runner blades touching the surrounding wall in case there is any vibration, in perfect alignment or irregularity of construction, or in case the thrust bearing should allow the runner to drop a small distance or in case a rubber or wood lined bearing is used which may permit lateral displacement of the runner. The object of this invention is to provide means for reducing the clearance between the periphery of the runner and the outer wall so as to increase the efliciency and to improve the operation of the turbine.
A further obj ect'of the invention is to provide means for preventing breakage of the runner blades when any foreign material or obstructionv passes within the clearance between the runner and the outer wall, or if the blades should touch the wall.
Further objects and advantages of the invention will be apparent by reference to the following specification and accompanying drawings, in which Fig. 1 is a plan view on section A-A of the turbine shown in Fig. 2 embodying the invention;
Fig. 2 is an enlarged sectional elevation through a hydraulic turbine showing the runner and the surrounding parts;
Fig. 3 is an enlarged sectional view of an edge or tip of a runner blade;
Figs. 4 and 5 show other arrangements for fastening thematerial to the runner tips;
Fig. 6 is an enlarged sectional elevation through a hydraulic turbine showing the runner and the surrounding parts with an adjliistable rubber lined ring in the stationary wa Fig. 7 is an enlarged sectional elevation showmg an adjustable metal ring in the stationar wall and runner blades tipped with yielda le material.
directed to the runner from the volute casmg 12 through the stay vanes 13 and guide vanes 14. The tip of the blades are provided with a strip of rubber or other material of a relativel soft or ielding nature 15 which is cemente molded vulcanized or mechanically fastened to the metal. In Fig. 3 the metal tip of the blade 11 is provided with a flange 16, around which the rubber is secured so as to provide the blade with a continuous smooth surface, the rubber being ground to merge with the metal surface.
After the rubber strip is secured to the tip of the blade by cementing, molding or vulcanizing, the rubber is further ground down to fit the clearance space, substantially eliminating the clearance between the runner and the outer casting 17 The grinding is accom; plished with the ordinary portable grinder, the runner mounted for rotation on a boring mill I or rotating table. The blades are ground to fit the required shape of the outer casting, which is usually conical or cylindrical or formed with a circular arc in meridian section.
The rubber tip of the blades closely spaced from the casting 17 will yield if for any reason foreign material, obstructions or trash enters the turbine casing. The obstruction if small enough to enter the clearance space will pass through to the draft tube without causing breakage of the runner blade. Tne use of rubber tipped runner blades increases the efficiency because it makes possible the provision of very small clearance between'thc runner blades and the surrounding wall, and therefore permits little leakage of water to pass between the runner and the stationary wall. The leakage which occurs when there is considerable clearance is objectionable not only on account of the direct loss of useful flow, but also from the disturbance which it causes in the adjacent flow near the bladetips.
Fig. 4 shows another modification of the invention in which the yielding material 15 is dovetailed into the tip of the runner blade and projects beyond the metal portion of the blade to form a close seal between the surrounding wall and the blade. I
Fig. 5 shows a further modification in which the strip of yielding material 15 is held mechanically in place in the tips of the runner blades. This strip may be made of rubber or material of like nature or might be made of wood or of soft metal, such' as lead or babbitt. The metal should be soft enough llvi that it would wear down if therunner touched the surrounding wall without scorlng or -1njuring the latterin any we The blades 11 are provided with' removable plates 18 which are held in lace by means of screws 19 tapped into the b ades.
In Fig. 6 a modification ofthe invention is shown wherein an adjustable ring 20 having a rubber lining 21 is set into a circular open ing 22 in the casting 17 The ring 20 is held in position b screws or bolts 28 tapped into the casting 1 at 24. These bolts are in recesses 25 filled with type metal finished flush with the wall surface. If the ring 20 or the blade tips become worn or if the ring needs adjustment to decrease the clearance between the wall and the runner blades 11, the type vided with a yielding means at its tip for reducin clearance between the runner and the walfi 5. In a hydraulic turbine, the combination with an outer stationary wall, of a 'runner having a central hub ortion and a plurality .of blades, and means or adjusting the clearmetal 26 can be melted out of the recesses, the
screws or bolts 28 loosened to permit the ring 20 to be raised a small amount, and the bolts 28 again made tight and the recesses 25 refilled with type metal. The slightly tapering or conical outer surface of ring 20 will thus be moved toward the runner blades to decrease the clearance. By these means the clearance between the casing and runner is made adjustable.
Fig. 7 shows a modification wherein the blade tips are provided with rubber and the casting 17 is provided with an adjustable clearance ring 27.
While the invention is illustrated and described more particularly with reference to propeller type turbines, the invention is not.
confined thereto, but is applicable to pumps having unshrouded impellers or any other uses or modificationswithin the scope of the appended claims.
I claim 1. In a runner for a turbine or pump the combination with a central hub portion, of a circumferential series of unshrouded blades thereon normally having a fixed relation thereto, each blade being provided with yielding means at its tip for reducing clearance and increasing the efliciency of the runner.
2. In a runner for a turbine or pump the combination with a central hub portion, of a circumferential series of unshrouded blades thereon, normally having a fixed relation thereto, each blade being provided with a rubber tip for reducing clearance-and increasing the efiiciency of the runner.
3. In a runner for a turbine or pump the combination with a'central hub portion, of a plurality of blades thereon, each blade being flanged at its tip, and a rubber strip secured to said flange for reducing clearance and increasing the efliciency of the runner.
4. In a hydraulic turbine the combination with an outer stationary Wall, of a runner surrounded by said wall having a central hub portion and a plurality of unshrouded blades thereon having normally an immovable relation thereto, each blade being proance bet-ween said outer wall and the runner blades.
6. In a hydraulic turbine the combination with an outer stationary wall, of a runner surrounded by said wall havin acentral hub portion and a plurality of blades all disposed substantially in a plane normal to the runner axis, said blades having normally an immovable relation to said hub and yielding material for the clearance between said outer wall and the runner blades.
7. In a rotary hydraulic machine the combination with an outer stationary wall, of a runner having a central hub ortion and a plurality of blades all dispose substantially in a plane normal to the runner axis, said blades having normally an immovable relation to said hub, the clearance space between said wall and said runner blades being provided on one' side with a rigid material and on 1the opposite side with a yieldable mater1a 8. In a rotary hydraulic machine the combination with an outer stationary wall, of a runner having a central hub portion and a plurality of blades, the clearance space between said wall and said runner blades being provided on one side with a rigid material and on the opposite side with a yieldable material, and means for adjusting the clearance between said wall and said blades.
9. In a rotary hydraulic machine a runner having a plurality of unshrouded blades and a circular and concentric stationary surroundin wall,'said blades at their tips being closely isposed to said wall with small running clearance therebetween and eachv blade being provided with yieldable means at its tip to permit the provision of said small bination of a runner having a plurality of unshrouded blades and a stationary surrounding wall, said blades at their tips being closely disposed to said wall with small running clearance therebetween, said wall having a generally conical shape smaller at one end than the other, and means for effecting relative axial adjustment between said runner and the portion of said wall adjacent the runner to provide adjustment of the clearance between said wall and runner.
11. In a rotary hydraulic machine, the combination of a runner havin a plurality of unshrouded blades and a circufir and concentric stationary surrounding wall, said blades at their tips being closely disposed to said wall with small running clearance therebetween, the clearance s ace between the blade tips and stationary wa lhavingyieldable material on one side thereof and r1g1d material on the other side.- v
12. In a rotary hydraulic machine a runner having a plurality of unshrouded blades having during normal operation a fixed relation to the runner hub and an outer stationary wall extending in an axial direction and coaxial with said runner, said blades at their tips being disposed closely to said wallwith small running clearance therebetween, and each blade being provided with yieldable means at its tip to permit the provision of said small clearance.
13. In a rotary hydraulic machine the combination with a runner of generally axial flow type having unshrouded blades having during normal operation a fixed relation to the runner hub and a continuous outer circular wall surrounding said runner and slightly spaced therefrom to provide a small running clearance therebetween, said blades at their tips engaging said wall with small running clearance, said blades being provided with yieldable material at the tips to permit the provision of said small clearance.
14. In a hydraulic turbine or pump the combination with a central hub portion of a circular series of unshrouded blades thereon of relatively unyielding material, said blades having a radially fixed position with respect to said hub during normal operation of the runner and each blade being provided with a different material at its tip forreducingclearance and increasing the efliciency of the runner.
15. In a hydraulic turbine or pump the combination with a central hub portion of a circular series of unshrouded blades thereon of relatively un ieldin materiahsaid blades havin a radial fixe position withvre'spect to said hub during normal operation of the runner and each blade being provided with a yielding material at its tip for reducing clearance and increasing the efficiency of the runner.
16. In a hydraulic turbine orpump thev combination with a central hub portion of a circular series of unshrouded blades thereon of relatively unyieldin material, said blades having a radially fixe position with respect to said hub during normal operation of the runner and each blade being provided with a relatively soft material at 1ts tip for reducing clearance and increasing the efliciency of the runner. 1
' 17. The combination in a hydraulic turbine or pump comprising a runner having a hub and a plurality of unshrouded blades all lying substantially in a plane normal to the runner axis and having during normal operation a radially fixed position with respect to said hub, a stationary wall surrounding said blades which at their tips are. closely dis- LEWIS FERRY MOODY.
CERTIIFIGATE 0F CORRECTIIQN.
Patent No. 1,694,481.
Granted December n, 1928, m'
LEWlS FERRY MOODY.
It is hereby certified that error appears inv the printed specification of the above numbered patent requiring correction as follows: Page 1, line 14, for the words in perfect" read "imperfect"; and that the said Letters Patents should be read with this correction therein that the same may conform to the record of the case in the Patent Office.
Signed and sealed this 12th day of March, A. D. 1929.
(sen
. M. J. Moore, Acting Commissioner of Patents.
US121787A 1926-07-12 1926-07-12 Propeller-type turbine or pump Expired - Lifetime US1694481A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US121787A US1694481A (en) 1926-07-12 1926-07-12 Propeller-type turbine or pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US121787A US1694481A (en) 1926-07-12 1926-07-12 Propeller-type turbine or pump

Publications (1)

Publication Number Publication Date
US1694481A true US1694481A (en) 1928-12-11

Family

ID=22398783

Family Applications (1)

Application Number Title Priority Date Filing Date
US121787A Expired - Lifetime US1694481A (en) 1926-07-12 1926-07-12 Propeller-type turbine or pump

Country Status (1)

Country Link
US (1) US1694481A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503025A (en) * 1946-01-09 1950-04-04 Borg Warner Torque converter
US2751187A (en) * 1953-12-08 1956-06-19 English Electric Co Ltd Feathering runner vane type hydraulic turbines and pumps
US2917275A (en) * 1952-10-03 1959-12-15 Napier & Son Ltd Turbo machines having adjustable guide blades
US3101926A (en) * 1960-09-01 1963-08-27 Garrett Corp Variable area nozzle device
US3756739A (en) * 1970-06-12 1973-09-04 Etude Soc Dev Turbines Hydraul Turbine-pumps
US4583913A (en) * 1983-10-03 1986-04-22 Kawasaki Jukogyo Kabushiki Kaisha Liner of a semi-axial flow pump
WO2004051078A1 (en) * 2002-11-29 2004-06-17 Voith Siemens Hydro Power Generation Gmbh & Co. Kg Water turbine
US20070231128A1 (en) * 2006-03-31 2007-10-04 Caterpiller Inc. Fan assembly
US20140056697A1 (en) * 2011-03-24 2014-02-27 Pierburg Pump Technology Gmbh Mechanical coolant pump
DE102022132483B3 (en) 2022-12-07 2024-02-29 Voith Patent Gmbh Process for producing a rotor blade

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503025A (en) * 1946-01-09 1950-04-04 Borg Warner Torque converter
US2917275A (en) * 1952-10-03 1959-12-15 Napier & Son Ltd Turbo machines having adjustable guide blades
US2751187A (en) * 1953-12-08 1956-06-19 English Electric Co Ltd Feathering runner vane type hydraulic turbines and pumps
US3101926A (en) * 1960-09-01 1963-08-27 Garrett Corp Variable area nozzle device
US3756739A (en) * 1970-06-12 1973-09-04 Etude Soc Dev Turbines Hydraul Turbine-pumps
US4583913A (en) * 1983-10-03 1986-04-22 Kawasaki Jukogyo Kabushiki Kaisha Liner of a semi-axial flow pump
WO2004051078A1 (en) * 2002-11-29 2004-06-17 Voith Siemens Hydro Power Generation Gmbh & Co. Kg Water turbine
US20070231128A1 (en) * 2006-03-31 2007-10-04 Caterpiller Inc. Fan assembly
US20140056697A1 (en) * 2011-03-24 2014-02-27 Pierburg Pump Technology Gmbh Mechanical coolant pump
US9464635B2 (en) * 2011-03-24 2016-10-11 Pierburg Pump Technology Gmbh Mechanical coolant pump
DE102022132483B3 (en) 2022-12-07 2024-02-29 Voith Patent Gmbh Process for producing a rotor blade

Similar Documents

Publication Publication Date Title
US1694481A (en) Propeller-type turbine or pump
US2285976A (en) Centrifugal compressor
US2013455A (en) Pump
US2163464A (en) Centrifugal pump
US3146722A (en) Centrifugal pumps and the like
US1955929A (en) Impeller
US10190565B2 (en) Method of refurbishing an energy conversion facility and refurbished energy conversion facility
US2784936A (en) Runner for hydraulic machines having a center portion and an outer segmented portionsecured together to provide an assembled runner
US1334461A (en) Centrifugal pump
US1619286A (en) Pump
US1516822A (en) mccormack
US2245094A (en) Pump
US3176960A (en) Hydraulic turbines or pumps
US2613609A (en) Compressing machine such as centrifugal blower or pump
US1958108A (en) Centrifugal pump
US1493154A (en) Hydraulic-power station
US1404717A (en) Hydraulic machine
US2265448A (en) Fluid actuating device
US1820150A (en) Labyrinth packing for turbines
US1879803A (en) Rotary pump
US2416268A (en) Hydraulic turbine seal
US1896219A (en) Adjustable centrifugal pump
US1741787A (en) Runner for turbines
US1860817A (en) Rotary pump
US1972865A (en) Centrifugal pump