US1445310A - Benjamin hall - Google Patents

Benjamin hall Download PDF

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US1445310A
US1445310A US1445310DA US1445310A US 1445310 A US1445310 A US 1445310A US 1445310D A US1445310D A US 1445310DA US 1445310 A US1445310 A US 1445310A
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fluid
rotor
passageway
chamber
case
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/042Turbomolecular vacuum pumps

Definitions

  • Figure 1 is a viewin central longitudinal section through the structure.
  • ig. 2 is a view in central transverse section through the turbine disclosing tion ofthe volute oase'to i l
  • 10 indicates a volute
  • This struc ⁇ ture is substantially circular, having an ine uction nozzle ⁇ 11, and eduction passageways 2 and 13.
  • v a and 13 cominunithe conoidal case cuinferential portion of i ⁇ case is which is a continuation arranged induction nozzle 11 and sageway decreases in sectional area as it Y Y within the case with its central transverse plane with the transverse ⁇ center of the conoidal case.
  • the rotor is mounted upon a i shaft19"disposed. eccentrically of the volute f of greater section than the reinainin ⁇ at eith is formed with which is beveled Huid to produce r
  • the present invention contemplates-the use f 'ch a laminated ns bein@ ⁇ to insure that a ⁇ motive fluid will be made throughout the the fluid may take place as its tion openings 25 openings as shown in :increasing area toward 16 and into the eduction i will b axis in the saine 1921.
  • Serial No. l52,650 Serial No. l52,650.
  • d receive e rotor itself is formed with a plurality of laminated disks.
  • large turbines the central er side and which a throat 22, establishing communication between th Whichwill thereafter encounter the surfaces of other rotor disks.
  • n t e present instance three other sets of disks are shown as indicated at 23, 24 and hese disks are all formed with double fe edges and are arranged and designed uniform distribution of the kni rotor and that )ended and. as the fluid i travels toward educin each of the disks.
  • Fig. 1 are of graduallyr rotors and are the fluid pacing washers 27 tween the various plates and form the hub ofthe rotor. These washers and the plates ⁇ are secured together bv fasteners such as rivets 28 arid are hired to the rotor shaft 19. In 1 th so that the Slightly used as a generator a fluid is delivered to the nozzle 'll under high pressure and velocity.
  • rl ⁇ his nozzle is tangent to the circumference ot the volute case and will direct the tluid into the volute passageway 17 which ⁇ gradually decreases in its sectional area.
  • This arrangement will cause the gases to pass through the annular throat 22 leadingfrom the passageway 17 to the main chamber of the casel it is divided into various streams which .pass between the laminations of the rotor.
  • t is intended that the laminations arranged as tc equally divide oi' ⁇ fluid passing therebetween. but it this does not lexactly occ-ur7V equilibrium may be established by the passage ot fluid through slots Q9 in the disks.
  • rlfhese slots are 'formed with substantially radial lrnite'edges which will oiler slight Vresistance to the fluid as it ⁇ passes through the dislr.
  • Eis-shown' in the drawings sets ot these slots' are arranged in alignment along dverent. circles yon the disks.
  • the passage of the fluid between the glates will cause a rotation ofthe rotorin vthe direction ot travel of the fluid which. rotation will be imparted to the shalt 19.
  • the ll'uid may then pass 'from thecase through the eduction passageways l2 and lf3.
  • the vturbine is to be used as apump or a conipressor the rotor 19 is driven at ot' speed, and will act to impart motion to a fluid drawn in the rase, which fluid will be yenpelled through the tangential nozzle vl1.
  • turbine comprising a volute casing having a tangentially vlisposed ⁇ inductibn port and central eduction ports, a circular pass geway extending around ⁇ and within the casing, ⁇ one end oi whichiis 4in communication with said induction port and the .sectionof whichcircular passageway gradually'decreases, and afrotor within the casxingy-said rotorbeing cunqir'ised ottwor sets at the same time a spi-y ral motion will be imparted tothe ilu'id as shall be: so i which a a high rate in vdiameter and the bases 'of the" sets oi' spaced conoidal vanas and the bases oi the two sets coinciding.
  • a turbine comprising a volute case having a central chamber termed by two conveXed side members, the bases ot which coincide, a circular passageway extending around said chamber and in communication therewith throughout its length, said passageway gradually decreasing in sectional area, a tangentiallyarranged nozzle formed as a continuatioii ot the large end ot said ⁇ circular passageway, central eduction ports at the center ot said chamber and through which a fluid may pass 'trom the circular passageway to the @duction ports.
  • said chamber and'throu'gh fluid may lpass trom the circular passageway to the eduction ports, and means tor dividing the ymotive 'fluid so that substantially equal volumes will pass between the-various plates of the rotor.
  • fi turbine comprising a volute case having acentralfcliamber termed two convened side members, the bases ot ⁇ which coincide, a ⁇ circular passageway extending around said chamber and' in communication therewith throughout its length, said passageway gradually decreasing ⁇ in sectional area7 a tangentiallyarranged nozzle formed as a continuation of the large end ot Vsaid circular passageway/f5 central.
  • a itluid may pass 'from the circular passagewayto the eductionportsi means for dividing the motive fluid so that substantially tequal volumesawill passfbetween the lll central eduction ports various plates of the rotor, means' for perinto which a mlttlng a gradual expanslon 0l the motlve ered, and a 1f Hmd as 1t )asses throuvh and around the snaeed dlsks val' uw 111 dlameter to a ree 10 l c y a rotor, and means S anequlibwlth the contour of the casing and between 5 mum of pressure of the motlve luld between Whlch d1sks the fluid passes.
  • Huid u 'ilder pressure is clelvn otor compmsmg a plurallty of

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Description

Feb. 13, 1923, 1,445,3l0
B. HALL TURBINE yFiled Mar. 16 1921 2 sheets-sheet 2 l invention Patented Feb. l, w23.
BENJAMN HALL, OF NEVADA CITY, CALIFORNIA.
TURBINE.
` Application iled March 16,
compressing` the flui o avol ute case, within wh rotor is provided,l said laminatio The invention is illustrated bv ample in t which: i
Figure 1 is a viewin central longitudinal section through the structure.
ig. 2 is a view in central transverse section through the turbine disclosing tion ofthe volute oase'to i l Referring more particularly to the drawings, 10 indicates a volute This struc` ture is substantially circular, having an ine uction nozzle `11, and eduction passageways 2 and 13. By referring to'F" way'ofexhe accompanying drawings, in
of te case. v a and 13 cominunithe conoidal case cuinferential portion of i `case is which is a continuation arranged induction nozzle 11 and sageway decreases in sectional area as it Y Y within the case with its central transverse plane with the transverse `center of the conoidal case.
The rotor is mounted upon a i shaft19"disposed. eccentrically of the volute f of greater section than the reinainin `at eith is formed with which is beveled Huid to produce r The present invention contemplates-the use f 'ch a laminated ns bein@ `to insure that a `motive fluid will be made throughout the the fluid may take place as its tion openings 25 openings as shown in :increasing area toward 16 and into the eduction i will b axis in the saine 1921. Serial No. l52,650.
d receive e rotor itself is formed with a plurality of laminated disks. large turbines the central er side and which a throat 22, establishing communication between th Whichwill thereafter encounter the surfaces of other rotor disks.
n t e present instance three other sets of disks are shown as indicated at 23, 24 and hese disks are all formed with double fe edges and are arranged and designed uniform distribution of the kni rotor and that )ended and. as the fluid i travels toward educin each of the disks. These Fig. 1 are of graduallyr rotors and are the fluid pacing washers 27 tween the various plates and form the hub ofthe rotor. These washers and the plates `are secured together bv fasteners such as rivets 28 arid are hired to the rotor shaft 19. In 1 th so that the Slightly used as a generator a fluid is delivered to the nozzle 'll under high pressure and velocity. rl`his nozzle is tangent to the circumference ot the volute case and will direct the tluid into the volute passageway 17 which `gradually decreases in its sectional area. This arrangement will cause the gases to pass through the annular throat 22 leadingfrom the passageway 17 to the main chamber of the casel it is divided into various streams which .pass between the laminations of the rotor. t is intended that the laminations arranged as tc equally divide oi' `fluid passing therebetween. but it this does not lexactly occ-ur7V equilibrium may be established by the passage ot fluid through slots Q9 in the disks. rlfhese slots are 'formed with substantially radial lrnite'edges which will oiler slight Vresistance to the fluid as it `passes through the dislr. Eis-shown' in the drawings, sets ot these slots' are arranged in alignment along diilerent. circles yon the disks. The passage of the fluid between the glates will cause a rotation ofthe rotorin vthe direction ot travel of the fluid which. rotation will be imparted to the shalt 19. The ll'uid may then pass 'from thecase through the eduction passageways l2 and lf3. lf the vturbine is to be used as apump or a conipressor the rotor 19 is driven at ot' speed, and will act to impart motion to a fluid drawn in the rase, which fluid will be yenpelled through the tangential nozzle vl1.
lt'will thus be seen that the turbine here disclosed, while otsiinple construction, yet provides eilect'ii'e means tor obtaining power from a motive luidor tor imparting motion to a liuid.
While ll have the volumes shown the prei'erred torni ol. my invention as now known to me it wil be understood that if'arious changes might be made in,the combinationa` construction and arrangement otl parts by tho-se skilled in the art, without departing` from the spirit of the invention` asclaimed.`
Having thus described my invention, what .l claimand desire tosecure bylictteii's Patent is: i
L A turbinecomprising a volute casing having induction and ed'uction portse anda rotor f composed Loi two connected.'v sets `ot' spaced conoidal va.nes-,'tlie `varies oi each'set varying coincidii'igh v A. turbine comprising a volute casing having a tangentially vlisposed `inductibn port and central eduction ports, a circular pass geway extending around `and within the casing, `one end oi whichiis 4in communication with said induction port and the .sectionof whichcircular passageway gradually'decreases, and afrotor within the casxingy-said rotorbeing cunqir'ised ottwor sets at the same time a spi-y ral motion will be imparted tothe ilu'id as shall be: so i which a a high rate in vdiameter and the bases 'of the" sets oi' spaced conoidal vanas and the bases oi the two sets coinciding.
3. A turbine comprising a volute case having a central chamber termed by two conveXed side members, the bases ot which coincide, a circular passageway extending around said chamber and in communication therewith throughout its length, said passageway gradually decreasing in sectional area, a tangentiallyarranged nozzle formed as a continuatioii ot the large end ot said `circular passageway, central eduction ports at the center ot said chamber and through which a fluid may pass 'trom the circular passageway to the @duction ports. Y
4. A turbinecoiriprising a'vgolut'e case having a centralchai'nb'cr vliornied by two convened side members,.t-he bases `of vwhich 4coincide, --a circular passageway extending around said chamber and in communication therewith throughout its length, said passageway gradually decreasingin sectional area, a tangentially arranged'nozzleformed a continuation ol? the large end' of said circular passagewavcentral eduction ports at the center oit; said chamber and'throu'gh fluid may lpass trom the circular passageway to the eduction ports, and means tor dividing the ymotive 'fluid so that substantially equal volumes will pass between the-various plates of the rotor.
5a fi turbine comprising a volute case having acentralfcliamber termed two convened side members, the bases ot `which coincide, a `circular passageway extending around said chamber and' in communication therewith throughout its length, said passageway gradually decreasing` in sectional area7 a tangentiallyarranged nozzle formed as a continuation of the large end ot Vsaid circular passageway/f5 central. eduction ports at the center o said chamber' and through which af `fluid may pass from the circular passageway to the eduction ports'7 dividing the motive 'fluid so that substantially equal volumes will pass between the various plates of the rotor, and means tor permitting a `gradual expansion of the nio- `tive fluid as it passes through and around the rotor'. i
v 6. A turbine ccinprisingV a. volute case having a central chamber Jorined by two convened sidemembers, the bases ci which coincideJl a circular passageway extending around said chamber and in `communication therewith throughout its "length, said passageway gradually decreasing in sectional,
area, atangentially arranged nozzle termed as a continuation ol the large end ot said ci rcul ar passa geway, at the center 'of said chamber and through; which. a itluid may pass 'from the circular passagewayto the eductionportsi means for dividing the motive fluid so that substantially tequal volumesawill passfbetween the lll central eduction ports various plates of the rotor, means' for perinto which a mlttlng a gradual expanslon 0l the motlve ered, and a 1f Hmd as 1t )asses throuvh and around the snaeed dlsks val' uw 111 dlameter to a ree 10 l c y a rotor, and means S anequlibwlth the contour of the casing and between 5 mum of pressure of the motlve luld between Whlch d1sks the fluid passes.
the varlous plates of the rotor.
turblne Comprising an outer case, vBENJAMIN HALL.
Huid u 'ilder pressure is clelvn otor compmsmg a plurallty of
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944786A (en) * 1953-10-15 1960-07-12 Thompson Ramo Wooldridge Inc Super and subsonic vaneless nozzle
US2988266A (en) * 1959-01-19 1961-06-13 Hughes John Wesley Self-cooled radial rotor
US3063673A (en) * 1958-10-20 1962-11-13 Caterpillar Tractor Co Centripetal turbine
US4036584A (en) * 1975-12-18 1977-07-19 Glass Benjamin G Turbine
US4050636A (en) * 1977-03-29 1977-09-27 Possell Clarence R Energy saving garbage disposal unit
US4534699A (en) * 1983-06-22 1985-08-13 Possell Clarence P Coal fired turbine
WO2000042291A1 (en) * 1999-01-08 2000-07-20 Fantom Technologies Inc. Friction turbine
US6224325B1 (en) 1999-01-08 2001-05-01 Wayne Ernest Conrad Prandtl layer turbine
US6238177B1 (en) 1999-01-08 2001-05-29 Fantom Technologies Inc. Prandtl layer turbine
US6261052B1 (en) * 1999-01-08 2001-07-17 Fantom Technologies Inc. Prandtl layer turbine
US20060216149A1 (en) * 2004-10-26 2006-09-28 Wilson Erich A Fluid Flow Channels in Bladeless Compressors, Turbines and Pumps
US20060291997A1 (en) * 2004-10-26 2006-12-28 Wilson Erich A Fluid Flow Chambers and Bridges in Bladeless Compressors, Turbines and Pumps
US20070092369A1 (en) * 2005-10-25 2007-04-26 Erich Wilson Bracket/Spacer Optimization in Bladeless Turbines, Compressors and Pumps
US20110311347A1 (en) * 2010-06-16 2011-12-22 John Marsden Flash Steam Turbine

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944786A (en) * 1953-10-15 1960-07-12 Thompson Ramo Wooldridge Inc Super and subsonic vaneless nozzle
US3063673A (en) * 1958-10-20 1962-11-13 Caterpillar Tractor Co Centripetal turbine
US2988266A (en) * 1959-01-19 1961-06-13 Hughes John Wesley Self-cooled radial rotor
US4036584A (en) * 1975-12-18 1977-07-19 Glass Benjamin G Turbine
US4050636A (en) * 1977-03-29 1977-09-27 Possell Clarence R Energy saving garbage disposal unit
US4534699A (en) * 1983-06-22 1985-08-13 Possell Clarence P Coal fired turbine
WO2000042291A1 (en) * 1999-01-08 2000-07-20 Fantom Technologies Inc. Friction turbine
US6224325B1 (en) 1999-01-08 2001-05-01 Wayne Ernest Conrad Prandtl layer turbine
US6238177B1 (en) 1999-01-08 2001-05-29 Fantom Technologies Inc. Prandtl layer turbine
US6261052B1 (en) * 1999-01-08 2001-07-17 Fantom Technologies Inc. Prandtl layer turbine
US20060216149A1 (en) * 2004-10-26 2006-09-28 Wilson Erich A Fluid Flow Channels in Bladeless Compressors, Turbines and Pumps
US20060291997A1 (en) * 2004-10-26 2006-12-28 Wilson Erich A Fluid Flow Chambers and Bridges in Bladeless Compressors, Turbines and Pumps
US20070092369A1 (en) * 2005-10-25 2007-04-26 Erich Wilson Bracket/Spacer Optimization in Bladeless Turbines, Compressors and Pumps
US7478990B2 (en) 2005-10-25 2009-01-20 Wilson Erich A Bracket/spacer optimization in bladeless turbines, compressors and pumps
US20110311347A1 (en) * 2010-06-16 2011-12-22 John Marsden Flash Steam Turbine

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