US2372518A - Centrifugal type compressor - Google Patents

Centrifugal type compressor Download PDF

Info

Publication number
US2372518A
US2372518A US536920A US53692044A US2372518A US 2372518 A US2372518 A US 2372518A US 536920 A US536920 A US 536920A US 53692044 A US53692044 A US 53692044A US 2372518 A US2372518 A US 2372518A
Authority
US
United States
Prior art keywords
walls
diffuser
vane
centrifugal type
passages
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
US536920A
Inventor
Manuel G Robinson
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to US536920A priority Critical patent/US2372518A/en
Application granted granted Critical
Publication of US2372518A publication Critical patent/US2372518A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/52Outlet

Definitions

  • the present invention relates to centrifugal type compressors having a variable vane vdiffuser l for converting'a part of the velocity energy of a medium impelled by the impeller into pressure energy and for varying the diiuser action upon changes in ow through the compressor.
  • the object of my invention is to provide an improved construction and arrangement of compressors with 'variable vane diiusers.
  • the arrangement comprises a compressor casing having two halves i and 2 with flanges securely lioined together by a plurality of circumferentially Vspaced bolts 3.
  • the casing half 2 has a number of circumferentially spaced ears 4 for attaching the compressor to a suitable support, not shown.
  • the two casing halves have inner portions forming an impelier chamber for accommodating en impeller d secured to a shaft d rotatably supported on a Vbearing l. Outer portions of the casing halves form a scroll 8 with.
  • N"I'he casing half l has a central opening or inlet l for air or like medium to be' compressed. -Fluicl impelled by the impeller is passed through a diffuser into the scroll 8.
  • the .diffuser has two axially spaced walls or rings Il and I2 with a plurality of circumfer- -entially spaced vanes I3 located between the walls and forming diii'user passages therewith for conducting'medium discharged from the im- 'peller to the scroll.
  • each diffuser vane has a movable portion'with 9, wedge-shaped bulge. Means are provided for moving such portions into and out oi' the diiuser passages;
  • each 4diduser has anl inner stationary part H and an outer stationary part l5 secured to or integrally formed with the diffuser wall Il.
  • Each intermediate part I 6 has another portion I8 (Fig. 4) of about the same thicknesses the inner and outer parts and upon insertion between the diffuser walls formsga smooth continuation of the inner and outer parts I4, I5 associated. therewith.
  • the flow area formed by the diffuser passages may be gradually decreased by the insertion and withdrawal of the portions I1, the minimum flow areas being attained when the portions Il are fully inserted and the maximum flow area being attained when the portions I'I are completely removed from the passages.
  • the mechanism for positioning the intermediate vane parts I6 comprises an internal ring gear lil located in an annular ring chamber 2liv formed' between the casing half I andthe diffuser
  • the ring gear i9 has an outer cylindrical surface bearing on a -cylindrical wall 2l,
  • the axial movement of the ring gear i9 is limited by the pro vision of a ring or plate 22 axially spaced from and integrally ⁇ formed with the diffuser wall l2.
  • the ring gear i9 may be'rotated in either direction by means of avpinion ZSs'ecured toa shaft 24 which is rotatably supported on the vcasing and the plate 22.
  • the shaft 2t is driven "ironi a drive shaft 25 through beveled gears 26.
  • the wall 22 is integrally formed with thedifiuser wall I2. The two walls are connected by yan annular cylindrical flange 30 between the inner ends of the wall I2 and the plate 22.
  • the walll2 and the plate" 22 are connected by aplurality of circumferentially vspaced curved walls.3I. These walls 3l togetherwith the walls l2, 22 and the flange 3l) form rircumferentially spaced chambers 32.
  • chambers 32 (Fig. l) are shaped to form a slidis completely disposed between the diuser walls u, l2 (Fina.)
  • the wall II of the diffuser has an, inner portion seated in an annular recess of the casing casing half I by the bolts 3.
  • a variable vane diffuser comprising twol axially spaced ring walls, and a plurality of cir- During assembly the After assembly of the impeller. in the casing half 2 the latter is secured to the' cumfcrentially spaced vanes forming diffuser A passages between said walls, each vane having inner and outer stationary parts supported on one of the walls and an intermediate part slidably projecting through aligned openings' in the walls, said intermediate part having an end portion with outer surfaces forming smooth continuations of the corresponding surfaces of the other -vane parts when disposed between said walls and another end portion which is wedgeshaped in section and forms a minimum area of ow between the vanes when disposed between said walls.
  • a variable vane diiuser comprising two axially spaced ring walls, a plurality of circumferentially spaced vanes forming diffuser passages between said walls, each vane having inner and outer parts secured to one of the walls and an intermediate Dart projecting slidably through aligned openings in the walls, said intermediate part having an end portion with outer surfaces* which is Wedge-shaped in section gradually to vary the area of flow between the vanes upon insertion between said walls, and means for simultaneously moving the intermediate parts.

Description

Manh ZZ i945. M G, RB|N5QN 2,372,518
CENTRIFUGAL TYPE COMPRES SOR Filed May 2 3, 1944 Invetor: Manuel @Robinson H Attorney.
Patented Mar. 2 7,
UNITED sTATEsA PATENT o rrica Manuel G. Robinson, Swampscott, Mass., assignor to General Electric Company, a corporation of New York Appucencn May 23, 1944, serial No. saaszo 2 blume. (ci. 23o-114) -The present invention relates to centrifugal type compressors having a variable vane vdiffuser l for converting'a part of the velocity energy of a medium impelled by the impeller into pressure energy and for varying the diiuser action upon changes in ow through the compressor. A
The object of my invention is to provide an improved construction and arrangement of compressors with 'variable vane diiusers.
- a diffuser vane ci Fis. 1.-
"The arrangement comprises a compressor casing having two halves i and 2 with flanges securely lioined together by a plurality of circumferentially Vspaced bolts 3. The casing half 2 has a number of circumferentially spaced ears 4 for attaching the compressor to a suitable support, not shown. The two casing halves have inner portions forming an impelier chamber for accommodating en impeller d secured to a shaft d rotatably supported on a Vbearing l. Outer portions of the casing halves form a scroll 8 with.
a enged discharge end t. N"I'he casing half l has a central opening or inlet l for air or like medium to be' compressed. -Fluicl impelled by the impeller is passed through a diffuser into the scroll 8.
The .diffuser has two axially spaced walls or rings Il and I2 with a plurality of circumfer- -entially spaced vanes I3 located between the walls and forming diii'user passages therewith for conducting'medium discharged from the im- 'peller to the scroll. According to my invention,
means are provided to. vary the diiuser passages. To this end each diffuser vane has a movable portion'with 9, wedge-shaped bulge. Means are provided for moving such portions into and out oi' the diiuser passages; In the present example each 4diduser has anl inner stationary part H and an outer stationary part l5 secured to or integrally formed with the diffuser wall Il. Be-
,tween the parts Ii and I5 is an inter-mediate movable partv I6 of an axial width about twice that of the inner and outer portions Il and I5. One portion of the intermediate part has a Wedge-shaped bulge I'l (Fig. 4) which upon inwall I2.
sertioninto the diffuser passages reduces considerably the cross-sectional area of the passages. Each intermediate part I 6 has another portion I8 (Fig. 4) of about the same thicknesses the inner and outer parts and upon insertion between the diffuser walls formsga smooth continuation of the inner and outer parts I4, I5 associated. therewith. The flow area formed by the diffuser passages may be gradually decreased by the insertion and withdrawal of the portions I1, the minimum flow areas being attained when the portions Il are fully inserted and the maximum flow area being attained when the portions I'I are completely removed from the passages.
The mechanism for positioning the intermediate vane parts I6 comprises an internal ring gear lil located in an annular ring chamber 2liv formed' between the casing half I andthe diffuser The ring gear i9 has an outer cylindrical surface bearing on a -cylindrical wall 2l,
'- Fig. 3, of the casing half i. The axial movement of the ring gear i9 is limited by the pro vision of a ring or plate 22 axially spaced from and integrally `formed with the diffuser wall l2. The ring gear i9 may be'rotated in either direction by means of avpinion ZSs'ecured toa shaft 24 which is rotatably supported on the vcasing and the plate 22. The shaft 2t is driven "ironi a drive shaft 25 through beveled gears 26.
Each intermediate or movable vane part I6 1s vprovided with a threaded rod 2l loosely prof jecting through an axial bore 28 in the casing half I and having screw engagement with a pinion 29 whereby rotation of the latter causes axial movement of the intermediate vane part ions 29. l The wall 22, as pointed out before, is integrally formed with thedifiuser wall I2. The two walls are connected by yan annular cylindrical flange 30 between the inner ends of the wall I2 and the plate 22. In addition the walll2 and the plate" 22 are connected by aplurality of circumferentially vspaced curved walls.3I. These walls 3l togetherwith the walls l2, 22 and the flange 3l) form rircumferentially spaced chambers 32. The
chambers 32 (Fig. l) are shaped to form a slidis completely disposed between the diuser walls u, l2 (Fina.)
The wall II of the diffuser has an, inner portion seated in an annular recess of the casing casing half I by the bolts 3.
Having described the method of operation of my invention, together with the apparatus which I now believe to be the best embodiment thereof, I desire to have it understood that the apparatus described is only illustrative and that 'the invention may be carried out by other means.
What I claim as' new and desire to secure by Letters Patent ofthe United States is:
1. A variable vane diffuser comprising twol axially spaced ring walls, and a plurality of cir- During assembly the After assembly of the impeller. in the casing half 2 the latter is secured to the' cumfcrentially spaced vanes forming diffuser A passages between said walls, each vane having inner and outer stationary parts supported on one of the walls and an intermediate part slidably projecting through aligned openings' in the walls, said intermediate part having an end portion with outer surfaces forming smooth continuations of the corresponding surfaces of the other -vane parts when disposed between said walls and another end portion which is wedgeshaped in section and forms a minimum area of ow between the vanes when disposed between said walls.
2. A variable vane diiuser comprising two axially spaced ring walls, a plurality of circumferentially spaced vanes forming diffuser passages between said walls, each vane having inner and outer parts secured to one of the walls and an intermediate Dart projecting slidably through aligned openings in the walls, said intermediate part having an end portion with outer surfaces* which is Wedge-shaped in section gradually to vary the area of flow between the vanes upon insertion between said walls, and means for simultaneously moving the intermediate parts.
2 MANUEL G. ROBINSON.
US536920A 1944-05-23 1944-05-23 Centrifugal type compressor Expired - Lifetime US2372518A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US536920A US2372518A (en) 1944-05-23 1944-05-23 Centrifugal type compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US536920A US2372518A (en) 1944-05-23 1944-05-23 Centrifugal type compressor

Publications (1)

Publication Number Publication Date
US2372518A true US2372518A (en) 1945-03-27

Family

ID=24140465

Family Applications (1)

Application Number Title Priority Date Filing Date
US536920A Expired - Lifetime US2372518A (en) 1944-05-23 1944-05-23 Centrifugal type compressor

Country Status (1)

Country Link
US (1) US2372518A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645410A (en) * 1947-05-05 1953-07-14 Construction De Moteurs D Avia Gaseous fluid compressor
US2798439A (en) * 1951-04-12 1957-07-09 Chain Belt Co Self-priming centrifugal pump
US2930579A (en) * 1955-09-19 1960-03-29 Dominion Eng Works Ltd Turbine guide vane locking and vibration preventing arrangement
US3160392A (en) * 1962-01-05 1964-12-08 David U Hunter Turbine with variable nozzle
DE1211746B (en) * 1956-01-07 1966-03-03 Dresser Ind Device for adjusting radial guide vanes of a centrifugal compressor
US3291236A (en) * 1961-10-12 1966-12-13 Aerophysics Company Ground effect machine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645410A (en) * 1947-05-05 1953-07-14 Construction De Moteurs D Avia Gaseous fluid compressor
US2798439A (en) * 1951-04-12 1957-07-09 Chain Belt Co Self-priming centrifugal pump
US2930579A (en) * 1955-09-19 1960-03-29 Dominion Eng Works Ltd Turbine guide vane locking and vibration preventing arrangement
DE1211746B (en) * 1956-01-07 1966-03-03 Dresser Ind Device for adjusting radial guide vanes of a centrifugal compressor
US3291236A (en) * 1961-10-12 1966-12-13 Aerophysics Company Ground effect machine
US3160392A (en) * 1962-01-05 1964-12-08 David U Hunter Turbine with variable nozzle

Similar Documents

Publication Publication Date Title
US2285976A (en) Centrifugal compressor
US3824029A (en) Centrifugal supersonic compressor
US2396319A (en) Pump
US2318990A (en) Radial flow elastic fluid turbine or compressor
US3289919A (en) Centrifugal gas compressors
US2392200A (en) Centrifugal compressor
US2520697A (en) Internal-combustion turbine plant
US2526618A (en) Pressure exchange apparatus
GB731822A (en) Improvements relating to turbines or compressors for operation with gaseous fluids
US2944785A (en) Impeller for turbine engine and the like
US2925954A (en) Compressor group with intercooler
US2372518A (en) Centrifugal type compressor
US2429978A (en) Centripetal-centrifugal pump
US2374122A (en) Double case pump
US2819837A (en) Compressor
US2543923A (en) Radial air compressor
US2578617A (en) Multistage centrifugal compressor
US2405048A (en) Centrifugal compressor
US2321810A (en) Rotary pump
US2306951A (en) Pump
US1896809A (en) Multistage turbine
US1287367A (en) Centrifugal compressor.
US2420940A (en) Gas purifier and compressor
US2381700A (en) Rotary pump
US1255852A (en) Gas-turbine.