US2660367A

US2660367A - Compressor sealing arrangement

Info

Publication number: US2660367A
Application number: US254155A
Authority: US
Inventors: Arnold H Ehlinger
Original assignee: Allis Chalmers Corp
Current assignee: Allis Chalmers Corp
Priority date: 1951-10-31
Filing date: 1951-10-31
Publication date: 1953-11-24
Anticipated expiration: 1970-11-24

Description

NOV. 24, 1953 A. HQE-HLINGER 2,660,367

COMPRESSOR SEALING ARRANGEMENT Filed Oct. 31, 1951 a/VVU MAX/O/v MM. 3%. awa 43m Momma Patented Nov. 24, 1953 COMPRESSOR SEALING ARRANGEMENT Arnold H. Ehlinger, Milwaukee, Wis., assignor to Allis-Chalmers Manufacturing Company, Milwaukee, Wis.

Application October 31, 1951, Serial No. 254,155

12 Claims. 1

The present invention relates to sealing arrangements for elastic fluid compressors of the type utilized in wind tunnels or other elastic fluid conveying systems.

In the operation of wind tunnels or like apparatus for conveying elastic fluids it is often a rigid requirement that oil vapor from the lubricating system of the compressor serving the tunnel and air from the atmosphere surrounding the tunnel should not be permitted to enter and become admixed with the air or other elastic fluid being circulated. A reason for this requirement in wind'tunnel operation, for example, is that the velocity of the elastic fluid circulated is extremely high and the presence of oil vapor, dust or an excessive amount of moisture in the circulated fluid has an adverse effect on objects placed in the tunnel for test purposes. To obtain high velocities in wind tunnel operation it is the practice in some instances to operate at subatmospheric pressures such that both the inlet and discharge pressures of the compressor are below atmospheric pressure. As the rotor shaft of the compressor must extend through a shaft opening in the casing of the compressor, so that -it can be coupled to suitable driving means, the opportunity for atmospheric air to enter the wind tunnel through such shaft opening is present.

A sealing device at the junction of the rotor tional view of an axial flow compressor embodying my new and improved sealing arrangement.

Referring to the drawing, a compressor embodying the present invention is shown installed between conduit portions 5 and 6 of an elastic fluid conveying system which, for example,.may be a closed circuit wind tunnel. .The compressor has a casing, completing the circuit between conduit portions 5 and 6, which comprises inlet and discharge portions 1 and B and a generally cylindrical central portion 9 defining the.

interior of the casing. Formed or mounted respectively in casing portions 1 and 8, inaxially spaced and axially aligned relation, are two hub members II and I2 which form, respectively with casing portions 1 and 8, an annular inlet passage l3 and an annular discharge passage l4 Hub members I l and [2 are each formed with a generally annular portion adjacent the interior of the casing and an enclosing end wall portions, l5 and I6 respectively, at the opposite end from the interior of the casing. Rotatably disposed in the casing is a rotor I! having a blade carrying portion I 1a which extends axially between hub members II and I2, a shaft portion l'lb which extends into the bore" of the annular portion of hub member H and through a shaft opening I 8 in end wall portion I5, and a shaft portion llc which extends into the.annular portion of hub member 12 but terminates short of end wall portion [6. Shaft portion IIb maybe coupled with any suitable driving means (not shown) for rotating rotor H. A plurality of blades l9 extend in a generally radial direction from the periphery of blade carrying portion l'la of rotor; I! for cooperation in elastic compressor which, upon installation of the compressor in an elastic fluid conveying system, will prevent atmospheric air as well as oil vapor from the compressor bearings from entering such system when the pressure of the fluid circulated in the system is below atmospheric pressure.

Other objects will appear hereinafter as th description of the invention proceeds. 1

In the drawing, the flgure'is -a.- vertical secfluid compressing relation with a plurality of f a blades" 20 mounted to the internal surface of easing portion 9.

The internal surface or bore of the annular portion of hub member H is provided, adjacent the blade carrying portion Ila of rotor H, with a pair of axially spaced labyrinth sealing surfaces 2| and 22 which cooperate respectively, in elastic fluid sealing relation, with cylindrical surfaces 23 and 24 on shaft portion Nb of rotor l1. Positioned axially between sealing surface 22 and end wall portion I5 is a hear annular chamber 29 between bearing 25 and V 3? to chamber 35.

3 end wall portion [5. During normal operation of the compressor a partial vacuum exists in chamber 29 and, to impede the flow of atmospheric air into chamber 29, a suitable sealing device 30 is provided between end wall portion 15 and shaft portion ill); the sealing device is shown by way of example as an axial contact type seal which abuts a collar 30a on shaft portion llb. A plurality of ports 3| circumferentially surrounding bearing 25 provide for communication between chambers '28 and 28 for a reason appearing hereinafter.

The internal surface of hub member I 2 is provided, adjacent the blade carrying portion Ha of rotor with a labyrinth sealing surface 32 which cooperates, in elastic fluid sealing relation, with cylindrical surface 33 on shaft portion ilc of rotor l3. Positioned axially between sealing surface 32 and end wall portion 55 is a bearing 34 which cooperates with a journal surface 35 on shaft portion l'ic. Hub member I2 further defines, in conjunction with shaft portion ilc, an annular chamber 36 between sealing surface 32 and bearing 3t and an annular chamber 37 between bearing 34 and end wall portion 16. A suitable thrust bearing 38, which cooperates in axial thrust bearing relation with a collar 38a. on shaft portion tie, is housed in chamber 3?. A plurality of ports 39 circumferentially surrounding bearing 34 provide for communication between chambers 36 and Si for a reason appearing hereinafter.

Communication between annular discharge passage is and annular chamber 2? may be provided by way of conduits to in rotor H.

An arrangement for supplying lubricating oil to bearings 25 and as includes a pneumatically sealed tank a conduit 42 having at one end thereof a trunk extending into the tank and at the other end thereof

branches

42a and 42?) leading to bearings 25 and 34 respectively, and an oil pump. in conduit 42 for supplying oil from the tank to the bearings.

, It was mentioned hereinabove that a main object of the present invention is to provide a sealing arrangement which prevents atmospheric air, as well as oil vapor from the lubricating system, from entering the compressing chamber of the compressor when the pressure of the elastic fluid in inlet and discharge passages 83 and i4 is below atmospheric pressure, during operation of the compressor. To accomplish this object annular chambers 28' and 3'? are operatively connected to a fluid exhausting device, shown herein .as a vacuum pump 55, for maintaining a predetermined subatrnospheric pressure in chambers 28 and 36. Conduit means for connecting chambers 28 and as to pump 45 may comprise, for example: an intermediate conduit portion 44 communicating at one end thereof with an upper portion Me of the interior of tank M and at the other end thereof with branches 434a and i-ib leading to annular chambers 28 and 31 respectively,

. and a conduitportion d5 cperatively connecting vacuum pump 5 with the upper portion 41a of the interior of tank 4!; ports 39, circumferentially surrounding bearing t l, connect chamber A quantity of lubricating oil is normally maintained in tank d! at a level low enough to permit air to be drawn from the intermediate conduit portion dl; to conduit portion 58 and at a level high enough to submerge the inlet to conduit The oil level indicated' by gauge 51 in the drawing would be suitable for example. a The mode of operation of a compressor pro- 4 vided with a sealing arrangement according to the present invention will be explained, for the sake of convenience, with the aid of assumed fluid pressures in various parts of the system described hercinabove. It will be understood, however, that the particular pressures referred to hereinafter are not intended to limit the present invention but are referred to merely by way of example to facilitate an explanation of its mode of operation,

When a compressor embodying the present invention is installed in a close-:1 circuit wind tunnel, represented by conduit portions 5 and 6 in the drawing, the quantity of air in the wind tunnel and the speed of rotor i? may be selected such that the pressure in the inlet passage l3 will be 2 p. s. i. a. (pounds per square inch absolute) and the pressure in the discharge passage M will be 6 p. s. i. a. Atmospheric air pressure is about 14.7 p. s. i. a. and the sealing arrangement of the present invention functions to prevent atmospheric air from leaking through seal 38 into the wind tunnel in the following manner.

Vacuum pump 55 may be operated to maintain a pressure of 5.8 p. s. i. a. in chambers 28, 29, 8B and 37. As the air pressure in discharge passage 14 is 6 p. s, i. a., air will flow therefrom through seal 32 to chamber 35, where vacuum pump 45 maintains a pressure at 5.8 p. s. i. a., and from passage id through conduits as to chamber 2'! where, because of the pressure drop occurring in conduits -39, the air pressure will be 5.9 p. s. i. a. Air will flow from chamber 27 through seal 2| to inlet passage i3, where the pressure is only 2 p. s. i. a., and from chamber 2? through seal 22 to chamber 28 where vacuum pump @5 maintains the, pressure at 5.8 p. s, i. a. It is thus seen that the sealing arrangement of the present invention causes atmospheric at 14.7 p. s. i. a. to flow through seal 3:} to chamber '29 and from there through ports 3! to chamber 2% from which it is exhausted to the atmosphere by exhaust pump 45.

Excess oil which flows out of bearings 25 and 34 into chambers 28, 29, 35 and 3? returns by gravity through conduit branches Mia and 44b to tank M. Oil vapors emerging from bearings 25 and 34 into chambers 28 and 38 are of course prevented from entering the wind tunnel in that air which seeps into chambers 23 and 36 is continuously exhausted to the atmosphere as explained above.

It will be understood that the present invention is applicable to elastic fluid compressors generally and is not limited partcularly to an axial flow type compressor. Also, that a compressor embodying the present invention may be utilized in various elastic fluid conveying systems, other than wind tunnels, when it is desirable to prevent atmospheric air or other elastic fluids from leaking into such systems.

While one embodiment of the invention has been described for the purpose of illustration, it

should be understood that the invention is not limited to the exact apparatus illustrated in the modifications thereof, within the scope of the appended claims, may be suggested by those skilled in the art without departure from the essence of the invention.

It is claimed and desired to secure by Letters Patent:

1. An elastic fluid compressor comprising: a rotor; a casing enclosing said rotor in a manner providing fluid inlet, compressing and discharge sections disposed in series flow relation, said casaccess? ins including a hub portion at its inlet end presenting a continuous interior surface surround ing the corresponding end portion of ,said rotor and including a pair of axially spaced-continuous cylindrical surfaces having a sealing coaction with said end portion of said rotor; a bearing structure carried by said interior surface in spaced axially outward relation with respect to the outer one of said pair of surf c s, and rtatably supporting the :adjacent end of said rotor; a first :means placing said discharge section in communication with the space between said pair of surfaces; and a second means for exhausting .gas entering the space between said bearingstructure and the outer one of said pair of surfaces.

2. An elastic fluid compressor comprising: a rotor; a 'casing enclosing said rotor in a manner providing fiuid inlet, compressing and discharge sections disposed in series flow relation, said casing including a first :hub portion at its inlet end and a second hub portion at its discharge end each presenting a continuous interior surface surrounding first and second end portions of said rotor respectively, said surface of said first :hub member including a pair of axially spaced continuous cylindrical surfaces having a sealing c.0- action with said first end portion of said rotor and said surface of said second hub member including a continuous cylindrical surface coacting with said second end portion of said rotor; at first bearing structure carried by said interior surface of said first hub member inspacedaxially outward relation with respect to the outer one of said pair .of surfaces and a second hearin structure carried by said -interior surface of said second hub member in spaced axially outward relation to said cylindrical surface of said second hub member for rotatably supporting the respective ends of said rotor; a "first means placing said discharge section incommunication with the space between said pair of surfaces; second means for exhausting gas entering the space between said first bearingstructure and the outer one of said pair ofsurfaces; and thirdrmeans for exhausting gas entering thespace :between said second bearing structure and said cy1indrical surface of said second "hub member.

3. An elastic fluid compressor comprising: ;.a casing; first and second axially spaced and axially aligned hub members mounted with respect to said casing so as to form inlet and discharge passages respectively therewith .and :an interior space between saidhub members, said Lhub :members each having a shaft receiving portion; :a rotor mounted. in said casing shaving a sblade carrying portion extending axially :between. said huhmembers, a first shaft port-iorrextending into said shaft receiving portionof said firstthub member, and a second shaft :portionzextending into said shaft receiving portion .of said second hub member; said shaft receiving portion of said first hub member having an interior surface procooperation with said first shaft portion -1a first annular chamber between said sealingsurfaces and a second annular chamber between 5.8 161 bearing and the adjacent one of :said, pair of sealing surfaces; conduit 'means connecting, said discha ge pass ge w th said first a nular c ain be t; and conduit means for conne ting said o! ,ond annular chamber to fluid pumping means for maintaining a predetermined pressure therein. 1

4. An elastic .fluid compressor comprising: a casing; first and second axially spaced and ex,- ially aligned hub members mounted with respect to said casing so ,as to .form inlet and discharge passage respectively therewith and an interior space between said hub members; said first and second hub members each having an annular shaft receivingportion closed at its furthest end from said interior space by an end wall portion, said wall portion of said first :hubr member ode.- fini g a shaft opening; a rotor mounted said casing having a blade carrying portion extending axial ly between said hub members, a first shaft portion extending into said annular portion of said first hub member and through said shaft opening in sealing arrangement therewith, and a second shaft portion extending into said annular portion of said second hub member; said shaft receiving portion, of said first hub member having an interior surface providing a pair of axiallyspaced sealing portions operativel-y associated with said first shaft portion and a bearing operatively supporting said first shaft portion disposed between said first hub member wall portion and the adjacent one of said pair of surfaces; said first hub member annular por-.- tion defining internally thereof in cooperation with said first shaft portion a first annular chamber between said sealingsurfaces and a second annular chamber between d e g nd the adjacent one of said pair of sealingsurfaces; conduit means in saidrotor connecting said discharge passage with said first annular chamber; nd nduit -.means in said first .hub mem er f nnecting said second annular cham to f id pu pin means for maintainin a pr d termin d p sure herein- .5. v Anelastic uid compressor for :use-in-awind tunne1 or the like, comprising: ;a casing: first and second ax ally p c d nd axi lly lign d hub members mountedwith respect to said casing so a to form inlet and di ch r e pass seszrespectively therewith and :an interior ,space'heween said huh m mb s;.sai.d fir t hub "m mb r having an annular portion with a pair of axial 1 pa d internal se ling surfaces adj cent said interior sp ce, an inte nal bear n surface i spaced axially outward vrelation with respect to the outer one of said pair of sealing surfaces, a first internal recess axially --oetween said sealing surf cesa sec nd internal r s w en said bearin -surf ce and th o ter one of said pair of sea ng surfa s; con it m an for .-co ect ing said second recessto fluid pumping means for maintaining a predetermined pressure therein; arotormount d insaidicas-ing v carry-ins portion extendin axially i-ietween aid hubv members and ,a shaft portion extending into said a nu a p r of sa d first hub mem e and conduit means connecting said discharge passage with said first recess.

' first andsecond ax liy sp ced anda allyi lis ed hn 'niembersmennted i pectt e d'o mg so as to for; inlet and discharg pas a es eesp otlve'lrtherewithand an interior s acerssaid interior space, an end'wall portion at the opposite end from said pair of sealing surfaces having a shaft opening, an internal bearing surface spaced axially between said wall portion and the adjacent one of said pair of sealing surfaces, a first internal recess between said sealing surfaces, a second internal recess between said bearing surf-ace and said pair of sealing surfaces; conduit means for connecting said second recess to fluid pumping means for maintaining a predetermined pressure therein; a rotor mounted in said casing having a blade carrying portion extending axially between said hub members and a shaft portion extending into said annular portion and through said opening in said wall portion; sealing means between said shaft portion and said wall portion; and conduit means in said rotor connectirr said discharge passage with said first recess.

7. An elastic fluid compressor comprising: a casing; first and'second axially spaced and axial iy aligned hub members mounted with respect to said casing so as to form inlet and discharge passages respectively therewith and an interior space between said hub members; said first and second 'hub members each having an annular shaft receiving portion closed at its furthest end from said interior space by an end wall portion, said wall portion of said first hub member defining a shaft opening; a rotor mounted in said casing having a blade carrying portion extending axially between said hub members, a first shaft portion extending into said annular portion of'said first hub member andthrough said shaft opening in sealing arrangement therewith, and a second shaft portion extending into said annular portion of said second hub member; said shaft receiving portion of said first hub member having an interior-surface providing a'pair of axial- 1y spaced sealing portions operatively associated with said first shaft portion an'd'a first bearing operatively supporting said first shaft portion disposed between said first hub member wall portion and the adjacent one'of said pair of sealing portions; said first hub member annular portion defining internally thereof in cooperation with said first shaft portion a first annular chamber between said sealing portions and a second annular chamber between said first bearing and the adjacent one of said pair of sealing portions; said shaft receiving portion of second hub member having an interior surface providing a sealing portion operatively associated with said second shaft portion and a second bearing operatively supporting said second shaft portion disposed between said second hub member wall'portion and said sealing portion; said second hub member annular portion defining internally thereof in cooperation with said second shaft portion a third annular chamber between said second bearing and said sealing portion; conduit means connecting said discharge passage with said first annular chamber; and means for maintaining predetermined pressures in said second and third here, a first shaft portion extending into said annular portion of said first hub member and a second shaft portion extending into said annular portion of said second hub member; said shaft receiving portion of said first hub member having an interior surface providing a pair of axially spaced sealing portions operatively associated with said first shaft portion and a first bearing operatively supporting said first shaft portion disposed in spaced axially outward relation with respect to the outer one of said pair of sealing portions; said first hub member annular portion defining internally thereof in co: operation with said first shaft portion a first annular chamber between said sealing portions and @a second annular chamber between said first hearing and said outer one of said pair of sealing portions; said shaft receiving portion of second hub member having an interior surface providing a sealing portion operatively associated with said second shaft portion and a second bearing operatively supporting said second shaft portion disposed in spaced axially outward relation with respect to said sealing portion; said second hub member annular portion defining internally thereof in cooperation with said second shaft portion a third annular chamber between said second bearing and said sealing portion; conduit means connecting said discharge passage with said first annular chamber; and means for maintaining predetermined pressures in said second and third annular chambers.

9. An elastic fiuid compressor comprising: a rotor; a casing enclosing said rotor in a manner providing fluid inlet, compressing and discharge sections disposed in series flow relation, said casing including a hub portion at its inlet end presenting a continuous interior surface surrounding the corresponding end portion of said rotor and including a pair of axially spaced continuous cylindrical surfaces having a sealing coaction with said end portion of said rotor; a bearing structure carried by said interior surface in spaced axially outward relation with respect to the outer one of said pair of surfaces, and rotatably supporting the adjacent end of said rotor: said interior surface of said hub portion defining in cooperation withsaid corresponding end portion of said rotor a first annular chamber between said pair of surfaces and a second annular chamber between said bearing structure and the outer one of said pair of surfaces; a passage means placing said discharge section in communication with said first annular chamber; a pneiunatically sealed 'lubricant' confining tank disposed below said second annular chamber, means fordelivering lubricant under pressure from said tank to said 'bearing structure, a gravity return conduit means placing said second chamber in communication with afportion of said tank above the level ing's tructure carried by said interior surface in.

spaced axially outward relation with respect to the outer one of said pair of surfaces, and rotatably supporting the adjacent end of said rotor; said interior surface of said hub portion defining in cooperation with said corresponding end portion of said rotor a first annular chamber between said pair of surfaces and a second annular chamber between said bearing structure and the outer one of said pair of surfaces; a passage means placing said discharge section in communication with said first annular chamber; a lubricant confining tank, means for delivering lubricant under pressure from said tank to said bearing structure, a return conduit means placing said second annular chamber in communication with said tank, and a fluid flow inducing device operatively associated with said return conduit means for effecting a withdrawal of fluids therethrough from said second chamber.

11. An elastic fluid compressor comprising: a rotor; a casing enclosing said rotor in a manner providing fluid inlet, compressing and discharge sections disposed in series flow relation, said casing including a hub portion at its inlet end presenting a continuous interior surface surrounding the corresponding end portion of said rotor and including a pair of axially spaced continuous cylindrical surfaces having a sealing coaction with said end portion of said rotor; a bearing structure carried by said interior surface in spaced axially outward relation with respect to the outer one of said pairof surfaces, and rotat ably supporting the adjacent end of said rotor; said interior surface of said hub portion defining in cooperation with said corresponding end portion of said rotor at first annular chamber between said pair of surfaces and a second annular chamber between said bearing structure and the outer one of said pair of surfaces; a passage means placing said discharge section in communication with said first annular chamber; a lubricant confining tank, means for delivering lubricant under pressure from said tank to said bearing structure, a conduit means having an intermediate portion 10 thereof placing said second chamber in communication with said tank at a point above the level of lubricant confined therein, and a fluid flow inducing device operatively associated with said conduit means at point disposed in downstream relation to said portion thereof.

12. An elastic fluid compressor comprising: a rotor; a casing enclosing said rotor in a manner providing fluid inlet, compressing and discharge sections disposed in series flow relation, said casing including a hub portion at its inlet end presenting a continuous interior surface surrounding the corresponding end portion of said rotor and including a pair of axially spaced continuous cylindrical surfaces having a sealing coaction with said end portion of said rotor; a bearing structure carried by said interior surface in spaced axially outward relation with respect to the outer one of said pair of surfaces, and rotatably supporting the adjacent end of said rotor; said interior surface of said hub portion defining in cooperation with said corresponding end portion of said rotor a first annular chamber between said pair of surfaces and a second annular chamber between said bearing structure and the outer one of said pair of surfaces; a passage means placing said discharge section in communication with said first annular chamber; a lubricant confining tank, means for delivering lubricant under pressure from said tank to said bearing structure, a conduit means having an intermediate portion thereof placing said second chamber in communication with said tank and a fluid flow inducing device operatively associated with said conduit means at a point intermediate the ends thereof.

ARNOLD H. EHLINGER.

References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,000,265 Vickers May 7, 1935 2,064,703 Van De Graaf Dec. 15, 1936