US2156340A - Vacuum pump - Google Patents
Vacuum pump Download PDFInfo
- Publication number
- US2156340A US2156340A US82760A US8276036A US2156340A US 2156340 A US2156340 A US 2156340A US 82760 A US82760 A US 82760A US 8276036 A US8276036 A US 8276036A US 2156340 A US2156340 A US 2156340A
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- Prior art keywords
- rotor
- blades
- opening
- slots
- 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
Links
- 230000002093 peripheral effect Effects 0.000 description 18
- 238000010276 construction Methods 0.000 description 5
- 239000000314 lubricant Substances 0.000 description 5
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010411 cooking Methods 0.000 description 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 1
- 238000002425 crystallisation Methods 0.000 description 1
- 230000008025 crystallization Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000003562 lightweight material Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/344—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
Definitions
- the opposite endof the rotor 22 is also provided with an axial extension 3d, preferably formed integral therewith, and which is also rotatably mounted in an anti-friction bearing 35 secured in a recessed portion 36 provided upon the inner side of the cover plate i8.
- This euxtension 3d has an axial opening therein for a purpose to be later described.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Description
May 2,- 1939.
J. P. JOHNSON VACUUM PUMP 2 Sheets-Sheet l A Filed June 1, 19:56
May 2, 1939. J. P. JOHNSON v 2,156,340
Y VACUUM PUMP Filed June 1, 1956 2 sheets-sheet `2 INVENTOR l A ORNEY.
Patented May 2, 1939 UNITED STATES PATENT OFFICE VACUUM PUMP James P. Johnson, Shaker Heights, hio
Application June l, 1936, Serial No. 82,760V
Claims. (Cl. 230-153) Theabove attributes are of essential importance in connection with the design and manufacture of pumps for use on aircraft, as is the primary purpose of the pump embodying the pres- 10 ent invention, although it will be obvious that it may be employed for many other purposes thereby not being so restricted.
The purpose of such a vacuum pump is to operate flight instruments accurately at. all plane speeds, any time of the day or night, and in all kinds of weather. have to be made to operate at a temperature and at speeds up to 4500 R.. P. M. without sticking or scoring, for periods of 500 continuous 2'0 hours of flying. All of these requirements are according to specication and pumps which fail lto perform in this manner are rejected with the result that such rejection necessarily involves loss of money as it is very seldom that these imperfections can be later corrected in a manner to pass inspection. While the pumps disclosed in my prior Patent No. 2,070,662, granted February 16, 1937, and No. 2,068,803, granted January 26, 1937, operated successfully and came within the heretofore mentioned requirements, certain objectionable structural features were embodied therein and the present invention resides in providing an improved pump structure in which these structural objections have been eliminated and by such .'15 elimination the efllciency of the present pump has been greatly increased.
It is therefore a further object of the present invention to provide an entirely new type of blade assembly and operation in which it is possible to obtain a uniform running clearance between the ends of the blades and the inner peripheral surface of the rotor chamber and wherein there is a minimum of blade area exposed to the pressure side.
., A further object is to provide through blades supported in such a manner in the rotor that a minimum of friction is obtained between the ends of the blades and the inner peripheral surface of the rotor chamber and relatively thin blades thus so producing a small area resulting in a reduction of braking effect and consequent friction.
A still further object of the invention is to provide a new type of rotor and the method by which the rotor is formed. Y
.55 A still further object of the invention resides in Furthermore', these pumps A so arranging the blades in the rotor that they are properly balanced thus wear.
With the objects above indicated and other objects hereinafter explained in view, my invention consists in the construction and combination 5 of elements hereinafter described and claimed.
v Referring to the drawings:
Figure 1 is a top plan view of a pump embodying the present invention illustrated in full sire.
Figure 2 is a longitudinal sectional view taken 10 substantially on line 2--2 in Figure 3- and showe ing in detail the features embodying the invention. Y
Figure 3 is a transverse sectional view taken on line 3-3 in Figure 2. 15
Figure 4 is a longitudinal sectional view of the rotor taken on line 4.4 in Figure 5. Figure 5 is an end view of the rotor illustrate in Figure 4 and looking at the left side thereof.
Figure 6 is an end view of the rotor illustrated 20 in Figure 4 and looking at the right side thereof.
Figure 7 is a perspective view of the blades better illustrating their construction and arrangement.
In the drawings I have illustrated a vacuum 26 pump embodying the present invention for use on aircraft but it should be understood that its use is not so restricted although it possesses features particularly essential in pumps of that type.
Referring particularly to Figures 1 to 3, the 30 pump comprises a housing I 0 preferably of aluminum or lsome similar light-Weight material cast in the usual manner, and which is open at one end and closed at its opposite end. At the closed end of the housing I0 there is an integral angular cir- 35 cumferential flange Il which terminates in a laterally extending flange I2 having openings I3 therein by which the housing is adapted to be removably connected to its supporting structure I4. The housing I0 is provided with a circular 40 bore Ii extending inwardly from the open end thereof which is terminated by the end wall I1 of the housing I0. The open end of the housing Il is closed by a cover plate I8 detachably connected 45 thereto by a plurality of machine screws t9 and the cover plate is provided with a circular extension 20 which lits into the adjacent end of the bore I6 to provide the opposite end wall of the bore.
-A tubular sleeve 2 I, preferably of hard nitralloy, is secured within the circular bore I6 and extends throughout the distance betiiveen the end wall l1 and the extension 20 on the cover plate Il, the latter engaging the adjacent end of the sleeve 2| and holdingI it against longitudinal movement within the bore i5.
' The housing i@ is provided with passageways 22 of identical area disposed on diametrically opposite sides thereof, the lower ends terminating in a transversely extending partition 23 and the upper ends communicating respectively with screwthreaded openings'24 which are adapted for connection with the instrument line depending upon the direction of operation of the pump.
The sleeve 2l is provided with transverse openings 25 positioned upon opposite sides thereof adjacent the upper portion which provide means of communication between the respective passageways 22 and the interior of the sleeve 2|.A These openings 25 function as inlet and outlet openings for the passage of iiuid through thel pump and. as before stated, their respective function is de- ,pendent upon the direction of operation of the The rotor 28, of course, is coextensive with thev sleeve 2l as more clearly shown in Figure 2. One end of the rotor 28 has an integral axial extension 30 which is rotatably mounted in an antifriction bearing 2i enclosed in a metal sleeve 32 secured in an opening in the end wall il of the housing iii, the free end of the extension 3d projecting beyond the end Wall il. 'I'he rotor 2B is also provided with an oiset portion 33 between the end oi the rotor and the extension 30, of a diameter enabling it to iit freely within the ad- `lacent end of the sleeve 32 so as to prevent displacement of the bearing 3i.
The opposite endof the rotor 22 is also provided with an axial extension 3d, preferably formed integral therewith, and which is also rotatably mounted in an anti-friction bearing 35 secured in a recessed portion 36 provided upon the inner side of the cover plate i8. This euxtension 3d has an axial opening therein for a purpose to be later described.
'Ihe rotor 28 is provided with pairs of radially disposed slots 3l and 36 on diametrically opposite sides, the slots of each pair" being in alignment and extending longitudinally throughout the length of the rotor 28. Ribs 39 are formed on the interior of the rotor 2t and extend longitudinally, for reinforcing the latter and by reason of the fact that the slots extend through the ribs 29 throughout their lengths, additional bear-A ing surface is provided for vthe blades. Unitary through blades are provided which have many advantages over the type of short blade and roller arrangement disclosed in my referred to copending applications. One Vblade lll is rectangular in shape and has a rectangular opening il! centrally positioned therein as more clearly shown in Figure 7. This blade l@ is relatively thin and preferably made of nitralloy, having its long edges rounded on an arc struck from a small axis while its short edges or sides are at. This blade is slidably mounted within the slots 33 as shown in Figure 3 and when the rotor is rotatedthe outer ends of the blade engage or have a running engagement with the inner pe ripheral surface of the sleeve 2|. The other blade 42 comprises two hal! sections of identical form, preferably 'of I-shape and made of nitralloy. These sections are arranged with the flanges in abutting relation and with the Webs extending in parallelism and when so arrangedare substantially the same size as the blade 40. 'I'he blade 42 is relatively thin and has its long edges rounded on an arc struck from a small axis while its short edges or sides are flat. This blade t2 is Aslidably mounted within the slots 31 as shown in Figure 3 and when the rotor is rotated the outer ends of the blade engage or have a running engagement with the inner peripheral surfaceof the sleeve v2li in the same manner as the blade 40. The blades 40 and 42 are readily assembled in the rotor by first placing the blade 40 centrally within the slots 38 and then moving the sections of the blade 42 transversely with respect to one another so that' the engaging iianges are positioned in alternate relation thus foreshortening the blade. When in this position the blade d2 is inserted in the slots 31 with portions of the blade extending through the opening di in the blade 40. The sections lcanthen be joggled around until they assume their normal position shown in Figure '7.
As the rotor rotates in a clockwise direction as viewed in Figure 3 the blades 40 and 42 will assume different angular positions due to the fact that they are rotating about an eccentric axis.
The inner peripheral surface of the sleeve 2| being in the nature of a limaon curve causes the ends of tlie blades to engage the surface with a minimum area exposed to the pressure side of the blades. Furthermore, by employing through blades it is possible to obtain a uniform running clearance between the ends of the blades andthe inner peripheral surface of the sleeve 28. An additional advantage of through blades resides in the fact that they are supported at opposite sides while sliding in the rotor thus avoiding cooking as is found to occur in the blade and roller type heretofore referred to with the result that the frictional resistance is reduced to a minimum To. provide proper and suitable lubrication for the relatively movable parts of the high speed rotor, itis desirable that the lubricant be supplied substantially continuously under pressure. This is eiectively obtainedin the present instance by providing a circumferential groove 43 on the inner surface of the opening in the wall I7 as shown in Figure 2. This groove is turned in any suitable manner before the sleeve 32 is secured in position and the latter cooperates therewith to provide an endless circular passageway. A laterally extending passageway 4t is provided in the extension' il and has its inner' end communicating with the groove 43, the outer end being adapted to communicate with the pressure oiling system of the engine through the medium of the engine pad to which the pump is connected by the iiange l2. `A plurality of such passageways are providedin the extension Il so that the pump housing may be angularly adjusted about its axis to properly 'align one .of the passageways itl with the opening in the engine pad, the latter being in engagement with the end surface of the ange when assembled which thereby closes the outer ends of the other passageways notin use.
An opening 45 extends upwardly from the groove 43 through the housing I0 and terminates in connection with a screw-threaded opening 46 vnormally closed by a removable screw threaded the vertical opening 45. Extending downwardly from the screw-threaded opening 48 in the cover I8 is an opening 5| which communicates with a circumferential groove provided in a hardened steel discharge member 53. This discharge member has its outer end iitting snugly in an axial opening provided in the cover plate I8 and is secured against accidental displacement by means of a removable cotter pin 54. A pair of angularly disposed communicating openings are drilled in the discharge member to provide a passageway 55 communicating with the circumferential groove and the outer surface of the inner end of the discharge member through which a lubricant may pass.
A bronze sleeve 56 is positioned loosely within the axial opening in the extension 34 and is secured to rotate with the rotor by means of a 'pin 51 having a drop 'fit in aligned openings in the extension 34 and the sleeve 56. 'Ihe pin 51 is positioned so as to underlie the inner race of the bearing 35 which prevents accidental disengagement. The sleeve 56 further encircles the inner end of the discharge member 53 and is provided with a predetermined clearance which controls the amount of lubricant discharged from the inner end of the passageway 55. By varying the clearance between the outer surface of the discharge member 53 and the adjacent inner peripheral surface of the sleeve 56 or=by varying the size of the passageway 55, or both, the rate at which the lubricant can be discharged is controlled and therefore the amount of lubricant reaching the relatively movable parts.
For further information as to the detailed operation of the oiling system reference should be had to my copending application Serial No. 10,994.
The rotor extension 30 is adapted for connection with a driving means such as the motor of the aircraft and due to the impulses set up during operation it has been found that where this driving connection is directly and rigidly made fatigue and breakage of thel parts occur from crystallization. A means of eliminating this condition has been proposed in my copending application which broadly contemplates a resilient or iiexible coupling between the rotor and driving means. In the present constrution a coupling is used embodying lthe sam'e principle but of slightly diiferent construction and-the details of which constitute an application being led of even date. The coupling comprises a body portion 58 having an axial opening extending inwardly from one end thereof and a resilient member 59 having its opposite ends mounted in said body portion and its intermediate portion extending across the axial opening. The extension 38 has a transverse slot in its end arid when the extension is inserted iinto the axial opening in the body portion 58 the resilient member 59 is disposed within the slot. As the extension and body portion are mounted so as to have a limited amount of relatively angular movement the impulses are1 absorbed by the resilient memand a retainer cap 6| encircles the body portion and prevents the resilient member from becoming disengaged. The body portion has` an axial extension terminating in a splined end 62 adapted for connecting with the motor drive. t As previously stated, the rotor 28 is of special construction having features entirely new in this art and reference should be had to Figures 4, 5 and 6 for a clear understanding. The body of the rotor is made of cast iron molded in any well known manner and is of circular cross ,section having a circumferential wall 63 and end walls 64 and 65 formed integral therewith thus producing a hollow rotor body more clearly shown in Figure 4. The end wall 64 has an axial extension 34 a hardened end for connection with the drive means thus improving the eflciency of the pump. This -steel insert 61 has at its inner end a laterally extending circular flange 68 terminating in an axially extending marginal flange 69 which tends to prevent relative movement and separation after the body of the rotor has been cast.
The rotor 28 as previously explained has inwardly projecting ribs 39, four of such ribs being shown positioned on diametrically opposite sides of the rotor and extending longitudinally throughout the length of the wall 63 and terminating as part of the end Walls 64 and 65. The rotor 28 as originally cast does not have the slots 31 and 38 provided therein but said `slots are cut in a manner later to be described, therefore the position of -the ribs on the inside of the rotor body are not ordinarily visible to the eye. The steel insert 61 has an additional important function and that is, it provides a locating means which, when the insert is properlyplaced within the mold, receives and supperts an axial extension on the end of the core. The opposite end of the core has an axial extension adapted to' provide the opening 66and the outer surfaceof the core is, of course, provided with grooves which provide the ribs 39.
In order that the position of the ribs may be positively and accurately determined, the core is provided with radial projections of the de' Vsired size and th end opposite to the insert 61 so as to provide openings 1i which when the rotor is machined extend through the end wall 64. There are four of such openings illustrated which are positioned directly beneath each rib 39 and the outer ends extend slightly beyond the outer peripheral surface of the extension 34 after the end walls are turned down, as more clearly shown in Figure 5. By thus providing these locating openings the position of the ribs 39 are definitely ascertained and therefore the slots 31 and 38 can be cut in any well known manner with the assurance that each slot will extend operate in both directions without the necessity of changing arrv'operating parts thereof, the only change required being the instrument line connection to the proper opening 24 depending upon the direction of rotation of the rotor. In Figure'3 ,for example if the rotor operates in a.
clockwise direction. the vacuum side or instrument line is connected with the opening 2t at the left hand.side and the othe1l opening 2t becomes the outlet opening.
In the operation, with the rotor rotating in a clockwise direction, the blades and t2 as they pass the inlet.opening 25 create a suction thus drawing the air out of the instrument line and thereby maintaining the proper vacuum therein for' operating the ight instruments. As the blades pass the outlet opening 25 the air is forced out and passes through the screwthreaded opening 241 on the right side of the pump as viewed in Figure 3. The openings 25 are so spaced with respect to the blades 40 and d2 that the ends of adjacent blades at vall times prevent connection between said openings. discharged air should become trapped ahead of any blade after the latter has passed the discharge opening 25 it is exhausted through the openings 26 and 2l into the associated passageway 22 and out through the screwthreaded opening 2li as before explained thus illuminating any possible breakage of the pump parts by reason of the extreme pressure which would otherwise be present. B y using solid through blades in the construction it is possible to plot'the contour of the )inner peripheral surface of the-sleeve 2i so that a uniform running clearance is maintained i thus increasing the eiiiciency of the pump.
v While I have described the preferred embodiment of the invention it is to be understood that extending slots, the slots of each pair being disposed on diametrically opposite sides of said rotor and in longitudinal alignment, the pairs of slots being arranged in dilerent relative angular positions, and a pair of non-extensible blades, each of which is'slidably mounted in a d iierent pair of slots and having their opposite ends adapted for uniform running engagement with the peripheral surface of said chamber, one of said blades being of rectangular shape and having an L opening extending therethrough, and the other 0f said blades being of freely cooperating I sectionsvfor the purpose of assembly and disassembly and adapted to extend through the opening in said rst mentioned blade in angular relation 2. A rotary pump comprising a housing having a chamber therein the inner peripheral surfaceof which conforms to a l-imaon curve and iiuid inlet and outlet openings communicating with said chamben, a rotor eccentrically positioned 'in said'chamber and rotatably mounted in said housing, said rotor having two pairs of radially extending slots, the slots of each pair being disposed on diametrically opposite sides of said rotor and in longitudinal alignment, the pairs of slots` being arranged in dierent relative angular positions, and a pair of Inon-extenl sible blades, each of which is slidably mounted in a dilerent pair ofslots and havingv their opposite ends adapted for uniform running engagement In the event any of the area-,eco
with the peripheral surface of said chamber, one of said blades being of rectangular shape and having an opening therethrough, and the other of said blades'consisting of two I sections normally arranged side by side with the adjacent edges of the flanges touching and the webs in parallelism and adapted to extend through the opening in said first mentioned blade in angular relation thereto,- the sections of said blade being adapted for relative movement longitudinally into a foreshortened position in which the'adjacent iianges are in alternate relation thereby enabling assembly and ldisassembly of said blade.
3. The method of producing a rotor for rotary pumps and the like which comprises casting as a unit a cylindrical body portion with end walls and one or more radially extending ribs upon the inside thereof, the end walls having axial extensions and one or more openings in atleast one of said end walls in alignment with said rib or ribs and extendingv outwardly beyond the peripheral surface of the adjacent extension to denitely predetermine the location of the rib or ribs-and subsequently cutting a radial slot or slots in the cylindrical body portionin alignment with the opening or openings whereby said slot or slots will extend substantially centrally through said rib or ribs.
4. A rotary pump comprising a housing having a bore therein and iuid inlet and outlet openings communicating with said bore, a sleeve secured y sleeve being provided with openings extending through the wall thereof and communicating respectively with the fluid inlet and outlet openings in saidhousing, a rotor eccentrically positioned in said sleeve and rotatably mounted in said housing,` said rotor having two pairs of radially extending slots, the slots of each pair being disposed on diametrically opposite sides'of said rotor and in longitudinal alignment, the pairs of slots being arranged in diierent relative angular positions, and a pair of non-extensible blades, each of which is slidably mounted in a diierent pair of slots and having their opposite ends adapted for uniform running engagement with the peripheral surface of said sleeve, one of said blades being of rectangular shape and having an opening extending therethrough, and the other of said blades being of freely cooperating I sections for the purpose of assembly and disassembly and adapted to extend through the a bore therein and fluid inlet and outlet openings communicating with said bore, a sleeve secured Within saidbore and having its inner peripheral surface conforming to a limaon curve, said sleeve.
being provided with openings extending through the wall thereof and communicating respectively with the uid inlet and outlet openings in said housing, a rotor eccentrically positioned in said sleeve and rotatably mounted in said housing, said rotor having two pairs of radially extending slots, the slots of each pair being disposed on diametrically opposite sides of said rotor and in l surface of'said sleeve, one of said blades being' of rectangular shape and having an opening therethrough, and the other o1' said blades consisting of two I sections normally arranged side by side with the adjacent edges of the anges touching and the webs in parallelism and adapted ing a chamber therein the inner'peripheral surface of which conforms to a limacon curve and 'iiuid inlet andy outlet openings communicating with said chamber, a rotox'- eccentrically positioned in said chamber and rotatably mounted in said housing, said rotor having two pairs of radially extending slots, the slots of each pair being disposed on diametrically opposite sides of said rotor and in longitudinalalignment, the pairs of slots being arranged in different relative angular positions, and al pair of non-extensible blades, each of which is slidably mounted in a different pair of slots and having their opposite ends adapted for uniform running engagement Withthe peripheral surface of said chamber, one of said blades being of rectangular shapeand having an opening extending therethrough, and the other of said blades being of freelyA cooperating abutting' sectionsadapted to efxtend through the opening in said first mentioned blade in angular relation thereto, each of said sections having lateral extensions disposed upon opposite 1 and its respective end wall, the other end wall having an axial bore extending from its inner gside toward its jouter side'and terminating slightly beyond the latter, the diameter of said bore being greater than the diameter of the extension on the opposite end wall, the end wail adjacent the axial opening being provided with transversely extending communicating openings radially of the latter and projecting slightly beyond the peripheral surface of the adjacent extension, said openings being in longitudinal alignment with said ribs whereby the location oi the latter are predetermined for the accurate cutting of slots through the end walls, cylindrical body portian and ribs.
8. A rotor. for rotarypumps and the like comprising a cylindrical body portion having integral end walls closing its opposite ends, radially disposed ribs on. the inside of said body portion and extending longitudinally thereof, said ribs being arranged in diametrically opposite relation,
axiallyd'isposed outwardly projecting extensions von the respective end walls, one of said exten- )sions having an axial opening extending through it and its respective end wall, the other end wall having an axial bore extending from its inner side toward its outer side and terminating' slightly beyond the latter, the diameter of said bore being greater than the diameter of the extension on theopposite end wall, the end wall adjacent the axial opening being provided with transversely extending communicating. openings disposed radially of the latter and projecting slightly beyond the peripheral surface of the adjacent exment with said ribs whereby the location of the latter are predetermined for the accurate cutting of slotsV through the end walls, cylindrical body portion and ribs, the end walls, body portion and ribs having longitudinally extending aligned slots provided therein which communicate with the transverse openings and bore in the respective end walls and which slots are adapted to receive non-extensible through blades coextensive with the body portion and end walls.
9. A pair `of cooperating non-extensible blades for a, rotary pump or the like, one of which is of rectangular shape having an opening extending therethrough, and the other of freely cooperating I sections for the purpose of assembly and disassembly and adapted to extend through the opening in said rst mentioned blade in angular relation thereto.
l0. A pair of cooperating non-extensible blades for a rotary pump on the like, one of which is of rectangular shape having an opening extending therethrough, and the other of ytwo I sections normally arranged side by side with the adjacent edges of the ilanges touching and the webs in parallelism and adapted to extend through the opening in said rst mentioned blade in angular relation thereto, the sections of said blade being adapted for relative movement longitudinally in a foreshortened position in which the adjacent ilanges are in alternate relation thereby enabling assembly and disassembly of said blades.
` JAMES P. JOHNSON.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US82760A US2156340A (en) | 1936-06-01 | 1936-06-01 | Vacuum pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US82760A US2156340A (en) | 1936-06-01 | 1936-06-01 | Vacuum pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2156340A true US2156340A (en) | 1939-05-02 |
Family
ID=22173270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US82760A Expired - Lifetime US2156340A (en) | 1936-06-01 | 1936-06-01 | Vacuum pump |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2156340A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2427606A (en) * | 1942-10-31 | 1947-09-16 | Aro Equipment Corp | Rotary pump with resilient end wall |
| US2448233A (en) * | 1943-11-02 | 1948-08-31 | Mining Engineering Co Ltd | Rotary intersecting vane engine and compressor |
| EP1707816A1 (en) * | 2005-03-31 | 2006-10-04 | Joma-Hydromechanic GmbH | Vacuum pump |
-
1936
- 1936-06-01 US US82760A patent/US2156340A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2427606A (en) * | 1942-10-31 | 1947-09-16 | Aro Equipment Corp | Rotary pump with resilient end wall |
| US2448233A (en) * | 1943-11-02 | 1948-08-31 | Mining Engineering Co Ltd | Rotary intersecting vane engine and compressor |
| EP1707816A1 (en) * | 2005-03-31 | 2006-10-04 | Joma-Hydromechanic GmbH | Vacuum pump |
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