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Publication numberUS2392858 A
Publication typeGrant
Publication dateJan 15, 1946
Filing dateMar 8, 1943
Priority dateMar 8, 1943
Publication numberUS 2392858 A, US 2392858A, US-A-2392858, US2392858 A, US2392858A
InventorsMcmahan Kenton D
Original AssigneeGen Electric
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
High-speed rotor for centrifugal compressors and the like
US 2392858 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

K. D. M MAHAN 2,392,858 HIGH SPEED ROTOR FOR CENTRIFUGAL COMPRESSORS AND THE LIKE Jan. 15, 1946.

Filed marens, 194s Inventor. Kenton D. Mc Mahan, 4 by D ,//4/ M m. B m 7% m V//w W A %%W A v His Attorney- Patented 15, 1946 UNITED srA-frss- PATENT.

FH E

HIGH-SPEED ROTOR FOR CENTRIFUGAL GOIWIPRESSJRS AND THE LIKE Kenton D. Mcltiahan, Scotia, N. Yi, assignor to General Electric Co New York mpany, a corporation of Application March 8,1943, Serial No. 478,334

8 Claims. (or. 230-134 The present invention relates to rotors such as rotors for centrifugal compressors and the like, intended for operation at high speed and has for its object to provide animproved construction and arrangement in rotors of this type.

The invention is especially applicable to shrouded impellers for high speed centrifugal air I compressors and it is this application of my invention which I have elected specifically to illustrate and describe. It is to be understood, however, that the invention is not limited thereto necessarily.

For a consideration of what I believe to be novel and my invention, attention is directed to the following 'speciflcationand to the claims appended thereto.

i0, 1. e., straighten it, serves to force outer relaforcing ring 8 more firmly on its seat.

The rings 8 and 9 and the tie ring I 0 form a unitary ring structure. Viewed from one aspect,

they may be considered a single S-shaped ring or order of 400 F., the ring structure may be readily In the drawing, Fig. 1 is a sectional view of a shrouded impeller embodying my invention, and Fig. 2 is a sectional view of a, reinforcing ring with a diagram therein. f

Referring to the drawing, I indicates the hub of theimpeller, 2 the web, 3 the impeller vanes and i the shroud. The inlet ends of the vanes are indicated at 5 and the discharge ends at t. The impeller receives air or other gasto be compressed through the annular inlet 7 and discharges it at the periphery of the impeller. The air or other gas enters in an axial direction, is turned gradually and is discharged radially. A structure such as that so far described may be formed as an integral pasting, the shroud i being cast integral with and carried by the. vanes 3.

For certain applications, such as for example I superchargers for, aircraft, it is desirable that the impeller be constructed of light weight material such as an aluminum alloy in order to keep down the weight. At the same time, such impellers are required to operate at high speeds, speeds of the order of 20,000 R. P. for example. This means that the centrifugal stresses are high, a thing which presents a serious problem especially in connection \with the shroud since the bursting, stresses in it are high.

According to my invention, I reinforce the shroud d by means of two high strength steel rings, an inner ring 8 located adjacent to the hub and an outer ring 9 located adjacent to the periphery and I tie the outer ring to the inner. ring by means of a tie ring it which is reversely curved where: m, re, re and rn=radii of the center of gravity of v ore-shaped in transverse section. The use of the tie ring id to anchor the outer ring 9 to the inner ring dis an important feature of my invention. By its use, the inner ring 8 which is closer to the axis of rotation and hence subject to lower centrifugal stresses assists-in carrying the outer ring 9 which is further from theaxis of rotation and hence-subject to higher centrifugal stresses.

And by making the tie ring s-shaped in cross section, centrifugal force tending to stretch ring positioned on the shroud and a good shrink and I reverse taper fit obtained.

For best results, it is important that the reinforcing ring structure support the impeller shroud at the inner and outer surfaces ii and i2 and at the same time be free from a-twisting moment tending to unhook the ring structure from the shroud's outer surface 12 due to forces acting on the ring whenvthe impeller is rotating at high,

speed. To this end, the contour of'the ring is such that the forces in the one portion of the ring a structure tending to twist the structure and unhook the end 9 is, at least, equalized by the forces in another portion of the ring structure tending to twist the structure in the opposite direction. This result is obtained by the use of a ring structure which may be S-shaped in cross section and dimensioned as illustrated particularly in Fig. 2. Referring to Fig. 2, it indicates the center of gravity of the ringstructure and it indicates a radial line through the center of gravity dividing the ring into two portions. A first approximation of the desired condition is obtained by divide ing the ring into four equal sections indicated A.

B, C and D about the radial center line it of the ring section, by determining the centers of gravity of the respective sections, which centers'of gravity are indicated at C's, Cs,C'o and On, and by I satisfying the equation rmXa+ro.Xc=ra.Xa-i-rnXn the respective sections A, B, C and D, a d

Xe and Xo=distances from center of gravity of the respective sections to the center line of the ring. H

it as being s-shaped in cross section, it is possible to design rings having other shapes'which -i?--..

will exhibit the specified characteristics at high speed. It should be understood that my invention covers reinforcing rings of all cross section shapes so designedthat the influence of centrifugal forces at high rotational speeds tending to deflect the outer ring portion awayfrom contact with the outer shoulder of the rotor wall is substantially or completely equalized by centrifugal forces acting on some other portion of the ring tending to cause the-outer end portion to move radially towards the shoulder. With rotor walls of certain shapes it is possible, and may be desirable, to "over-compensate,"that is, design the cross section so that the net force tending to move the outer end portion of the ring into tighter engagement with the outer shoulder in-.

creases as centrifugal force increases. The exact design required to produce the desired result depends on the shape of the wall to be reinforced, and must be determined in each particular case by analysis and calculation verified by experiment.

In the present instance, the hub I is shown as 'being reinforced by suitable high strength steel rings l3 and it which may be positioned with a shrink fit. 'I'hese rings serve to strengthen the aluminum alloy casting and in addition function to hold the ends of the bore of the hub more nearly to size at all operatin speeds.

By my invention, I am enabled to construct a rotor which is light in weight but which at the same time is capable of operating at high speeds.

While the use of the invention in the construction of shrouded impellers for centrifugal com-- pressors, such as superchargers for aircraft en- I gines, is an important application of my invention, it will be clear that the invention is not limited necessarily to this use but may be used wherever found applicable. In accordance with the provisions of the patent statutes, I have described the principle of operation of my invention, together with the apparatus which I now consider to represent the Foest embodiment thereof. but I desire to have it understood that the apparatus shown 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 of the United States. is:

1. A rotor subject to high centrifugal stresses comprising a disk member having an outer surface forming two axially and radially spaced outer annular shoulders, and a reinforcing ring substantially S-shaped in cross-section with inher and outer end portions forming radially and axially spaced inner surfaces tightly engaging the respective outer shoulders of the disk member to resist radial expansion thereof and an intermediate portion connecting the end portions and having a surface axially facing the disk member and gradually curving away therefrom in radial direction.

2. A rotor comprising a disk member having v a central opening and an outer annular edge, a

said disk member having an outer surface form- .ing a first annular shoulder near the opening and a secondv annular shoulder near the outer edge,

and a reinforcing structure permitting operation of the disk member at speeds at which the centrlfugalstresses therein reach magnitudes'of the order of the bursting stresses of the disk member, said-reinforcing structure comprising a solid ring member substantially S-shaped in section and having axially and radially spaced cylindrical surfaces forming a shrink fit with the first and second shoulders respectively of said disk member.

. 8. A rotor for a high speed centrifugal machine I or the like comprising a hub, a web, blades carried by the web, a shroud for the blades and re- I inforoing means for the shroud comprising a ring ugal bursting stresses in operation, reinforcing means for said Well comprising a ring structure having inner and outer portions tightly engaging the wall at radially spaced locations to relieve centrifugal stresses in thewall and an intermediate portion connecting the radially outer portion, to the radially inner portion'sothat the latter helps to support the forces set up in the former by centrifugal force.

-5. In combination with a high speed rotor subiect to centrifugal brusting stresses in operation and having a wall with radially and axially spaced cylindrical shoulders, a reinforcing structure for the wall comprising a ring substantially S-shaped in cross section and having radially and axially spaced inner and outer portions tightly engaging the respective shoulders to reiieve centrifugal stresses in the wall, the cross section of said ring being so shaped that when operating at high speed the forces acting on a certain part of the ring tending to move the radially outer portion from engagement with the outer shoulder are substantially balanced by forces acting on another part of the ring tendin to move the outer portion into tighter engagement with said shoulder.

6. In a high speed rotor having a wall requiring support at both inner and outer radially spaced portions to withstand centrifugal stresses, a-reinforcing ring for said wall having a. curved cross section with radially spaced inner and outer end portions and an interconnecting portion arranged to transmit forces set up during operation from one end portion to the-other, the inner end portion tightly engaging the outer surface of an annular shoulder formed on a radially inward portion of the wall and the outer end portion tightly engaging the outer surface of an annular shoulder formed on a radially outer portion of the wall, the cross section of the ring being so shaped that at high speeds the centrifugal forces acting on a certain portion of the ring tending to cause the outer portion to deflect away from the outer shoulder on the wall are substantially equalized by" the forces acting on another portion of the ring tending to cause the outer portion to deflect towards said shoulder.

"I. In a high speed rotor having a wall requiring support at both inner and outer radially spaced portions to withstand centrifugal stresses,

, radially spaced inner and outer annular shoultion fromone end portion to the-other, the inner end portion tightly engaging the outer surface of the annular shoulder formed on a radially inward portion of the wall and the outer end portion tightly enga ing the outer o! the annular shoulder formed on a radially outer portion of the wall, at least one of said shoulders having a "substantially cylindrical outer surface tapering slightly to a smaller diameter in the direction toward the walland the ring having a cross section so shaped that at high speeds the centrifugal forces acting on a certain portion of the ring tending to disengage the outer aeoasss end portions and eninterconnecting portion arranged to transmit forces set up during operation from one end portion to the other. the inner end portion tightly engaging the outer suriace of an annular shoulder formed one radially inward portion of the wall and the outer end portion tightly engaging the outer surface of an annular shoulder formed on a radially outer portion of the wall. the cross section of the ring being so shaped that the integral of the moments produced by centrifugal iorcesacting on a certain portion of the ring tending to rotate the cross section 01 the ring counterclockwise is substantially balanced by the integral oi the moments of the forces acting on the other portions of the ring tending to deflect the cross section clockwise. I

KENTON D. McMAHaN.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2438867 *Jun 1, 1945Mar 30, 1948United Aircraft CorpMethod of assembling shrouds on impellers
US2441432 *Dec 14, 1945May 11, 1948Gen ElectricHigh-speed rotor
US2556676 *Jun 9, 1944Jun 12, 1951Gen Motors CorpRotor blade construction
US2860827 *Jun 8, 1953Nov 18, 1958Garrett CorpTurbosupercharger
US3107627 *Jun 27, 1958Oct 22, 1963Stalker CorpRotor for radial flow pumping means
US3175804 *Apr 1, 1963Mar 30, 1965Bendix CorpRadial-flow turbine safety
US4795311 *Jun 20, 1986Jan 3, 1989Proizvodstvennoe Obiedinenie "Nevsky Zavod" Imeni V.I. LeninaCentrifugal compressor impeller
US4806078 *Jan 21, 1988Feb 21, 1989Klein, Schanzlin & Becker AktiengesellschaftDevice for transmitting torque to brittle impellers of fluid flow machines
US4863349 *Nov 28, 1986Sep 5, 1989Proizvodstvennoe Obiedinenie Nevsky Zavod Imeni V.I. LeninaImpeller of centrifugal compressor
US6599084Jan 20, 2000Jul 29, 2003Leybold Vakuum GmbhRotor fixture for a friction vacuum pump
US7147433 *Nov 19, 2003Dec 12, 2006Honeywell International, Inc.Profiled blades for turbocharger turbines, compressors, and the like
US8469669 *Mar 10, 2009Jun 25, 2013Man Diesel & Turbo SeCover disk for a closed impeller
US20110008160 *Mar 10, 2009Jan 13, 2011Man Diesel & Turbo SeCover disk for a closed impeller
DE3002585A1 *Jan 25, 1980Aug 7, 1980Mercantile Ab OyKreiselgeblaese-laufrad
WO2000060241A1 *Jan 20, 2000Oct 12, 2000Ralf AdamietzRotor fixture for a friction vacuum pump
Classifications
U.S. Classification416/186.00R, 416/244.00R, 416/194, 416/244.00A
International ClassificationF04D29/28
Cooperative ClassificationF04D29/284
European ClassificationF04D29/28C