US2665122A - Hydraulic power means and seal for pressure vessel agitators - Google Patents

Hydraulic power means and seal for pressure vessel agitators Download PDF

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US2665122A
US2665122A US293019A US29301952A US2665122A US 2665122 A US2665122 A US 2665122A US 293019 A US293019 A US 293019A US 29301952 A US29301952 A US 29301952A US 2665122 A US2665122 A US 2665122A
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shaft
pressure
chamber
motor
seal
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US293019A
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Ernest E Rowland
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B21/00Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/40Sealings between relatively-moving surfaces by means of fluid
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S366/00Agitating
    • Y10S366/601Motor control

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Hydraulic Motors (AREA)

Description

Jan. 5, 1954 E. ROWLAND 2,665,122 HYDRAUL C POWER MEANS AND SEAL FOR PRESSURE VESSEL AGITATORS Filed June 11, 1952 IN VEN TOR.
r new) E. Row/and BY 7 yy am $947 W ATTOR/VfXf' Patented Jan. 5, 1954 UNITED STATES PATENT QFFICE' Ernest E. Rowland, Akron; Ohio Application June 11, 1952,. Serial No.- 293,019
g 2 Claims. 1
An object of the present invention is to provide improved hydraulic power means and sealing means for pressure vessel agitator shafts.
One of the objects of the present invention is to provide an efficient driving and sealing means for an agitator shaft in a pressure reaction vessel so arranged that no part of the shaft ever extends in the atmosphere.
Another object of the present invention is to provide in combination, a pressure reaction vessel containing liquid and subject to a predetermined pressure, a rotatable shaft in th vessel and projecting through the wall thereof, a selfcontained motor for rotating the shaft and connected to the shaft spaced from the wall of the pressure vessel, this motor running in. hydraulic oil or other hydraulic fluid, together with sealing means embracing the shaft where it passes through the wall of the pressure vessel an enclosed chamber surrounding the agitator shaft and sealing means, with a seal between the chamber and. the motor housing together with means maintaining a pressure liquid in the chamber at a pressure above the predetermined pressure in the agitator vessel. In this way any leakage from the chamber along the shaft toward the vessel win be into the vessel and any leakage from the chamber along the shaft in the op o ite direct o will be into the motor housing.
Another object of the present invention is to provide in the combination of the preceding paragraph, a single hydraulic system providing hydraulic liquid under pressure which isconnected to the sealing chamber through pressure regulating means maintaining a substantially constant pressure in the chamber at all times higher than the predetermined pressure in the agitator, and so arranged thatany leakage is always back into the hydraulic system.
A further object of the present invention is to provide a self-contained motor of the hydraulic type having a shaft aligned with the agitator vessel shaft and a single hydraulic system for operating the motor and for providing a pressure liquid seal along the agitator shaft. In such a combination the agitator driving shaft terminates at one end inside of the agitator vessel and at the other end terminates inside of the hydraulic system so that no leakage can ever occur to atmosphere.
Other objects and advantages of my invention will be apparent from the accompanyin drawlugs and description and the essential features thereof will be set forth in the appended claims.
The drawing shows somewhat cliagrammatically an hydraulic system embodying my invention with parts of the sealing means broken away central sectional view to more clearly show the construction.
In operating chemical reaction vessels wherein liquids are treated under developing pressure, it is sometimes undesirable, and other times dangero us to have liquid leak outwardly from the reaction vessel along the agitator shaft which extends into the vessel. lit is an object of the present invention to prevent such leakage along the agitator shaft. Difficulty has been found in the past in drives for such pressure vessel agitators where they exert a side thrust on the agitating shaft rendering it difficult to maintain a good seal to prevent leakage along the shaft out of the vesscl. My invention is Well adapted to solve this problem also.
On form of m invention is illustrated in the drawing wherein a reaction vessel is shown at I!) having a shaft l l passing through the upper wall of the reaction vessel to the interior thereof for operating an agitator or the like. Immediately above the top wall of the reaction vessel I0 I provide a pressure hydraulic seal l2 and above this is mounted a self-contained driving motor l3.
The seal l2 comprises a base plate l4 surmounted by a tubular body Hi, th interior of which provides a chamber surrounding the shaft in which liquid under pressure is provided for sealing purposes. The body I5 is provided with a bottom flange I6 and a top flange ll. Bolts 18 pass through flange l6 and base member l4 into the top wall of the reaction vessel l 0 so as to hold the parts assembled. A carbon sealing ring it! of known construction tightly embraces shaft ll almost immediately above the top wall of the reaction vessel ill, there being just enough clearance to permit rotation of shaft l l in the carbon ring IS. The external diameter of the carbon ring is just sufficient for a press fit into a recess 14a in the base member 14. Immediately above the carbon ring is a sealing collar 26 which is cup-shape opening upwardly and which holds two annular sealing rings 2| of compressible sealing material. A packing gland 22 presses the sealing rings 2| inside of the cup-shape member 29 so as to tightly hug the shaft l l. A compression ring 23 is secured to shaft l I by means of a plurality of set screws 24. A plurality of short helical springs 25 are seated in recesses in ring 23 and press downwardly against the packing gland. 22. Each of these springs surrounds a guide pin 26 which seats in ring 23 and gland 22 so that parts 23, 22 and 20 turn with shaft I I.
3 The lower face of the member is hardened where it rubs against the carbon ring I9. This provides a very effective sealing means between the pressure reaction vessel III and the sealing chamber I2.
Means is provided in the sealing chamber construction to support the shaft I I by means of twobearings 21 spaced apart along the shaft I I so as to support it firmly against lateral movement. Each of these bearings fits on one side againsta shoulder 28 in member I5 and is held on the opposite side by means of a snap ring 29 seating in the member I5.
It is commonly the practice to provide shaft I I extending into the atmosphere and there pro-- vided with a drive means extending laterally to some driving mechanism. This causes a side thrust on shaft II which is disadvantageous to the seal where the shaft II passes through the wall of the reaction vessel It and sometimes causes the carbon ring I9 to lift out of place. I avoid this objectionable arrangement by providing a self-contained motor I3 having a driving shaft 30 which is either integral with or at leastaligned with the shaft I I. In the present instance: I have shown the two shafts in alignment and connected together for uniform rotation by a coupling 3|. In this way, I provide torque without side thrust in the driving motor I3. To complete the effective sealing of shaft II against leakage therealong, in an upward direction, I prefer to use a self-contained motor running in hydraulic oil or other hydraulic fluid. Specifically, I have shown motor I3 as a positive displacement hydraulic motor of the type specifically shown in Fig. l of United States Patent No. 2,480,069, granted August 23, 1949, to Fred J. Wright. The housing of motor I3 has a bottom flange I3a which is secured by means of bolts 34 to flange I! of the member I5. The seal 35 seals shaft 3!] between chamber 36 and the interior of the housing for motor I3. This seal 35 is the sole dividing means between the hollow of motor housing I3 and chamber 36.
Means is provided for supplying hydraulic pressure fluid to chamber 36 for sealing purposes and through conduit 32 to drive motor I3. Preferably, but not necessarily, I use a single hydraulic system for this purpose. A reservoir 3'! is supplied with hydraulic fluid which is moved by means of pump 38 through line 39 and control valve 40 to line 32 leading to motor I3. The discharge from motor 33 passes through a rotameter M which is a device for measuring the flow through line 33 and line 42 back to the reservoir 37. The pressure and temperature of this hydraulic fluid are held substantially constant and, therefore, the viscosity is substantially constant. Therefore, the rate of flow through the positive displacement motor I3 can be translated into revolutions per minute of shafts 30 and II and the calibration scale on the rotameter 4| can be read directly in revolutions per minute. In one form of my invention, a flow of 0.42 gallons of oil per minute is equivalent to 100 R. P. M. of the hydraulic motor I3, and tests show that this motor would deliver about 2 H. P. at 1500 R. P. M. when the oil pressure is 600 pounds per square inch. I prefer to use an oil having a viscosity of about 2 5 seconds on a Saybolt Universal viscosimeter at the temperature of the hydraulic system which is preferably held not greatly differing from the temperature within the reaction vessel I ll. Quite commonly a lubricating oil of this viscosity is used. Some oil will leak by the pistons and rotor of the hydraulic motor I3. A drain line 43 conducts this leakage back through a by-pass in the rotameter M to the line 42. This leakage oil has no effect on the movements of the rotameter M and does not effect the R. P. M. registered there.
Another connection from line 39 leads through a pressure regulating valve 44 and line 45, through a control valve 46 to the lower end of 'chamber 36. The discharge from chamber 36 is through line 41 and relief valve 48 to rotameter 49 and thence through line 59 back to line 42 for return to the reservoir 31. The flow through the sealing chamber 36 may be regulated by valve 46 and in one form of my invention is adjusted to about of a gallon per minute. To insure that no leakage will occur from the reaction vessel I0 outwardly along shaft II, the pressure in chamber 35 is constantly held at pressure greater than that in the reaction vessel I I]. In one form of my invention, the regulating valve 44 is set to hold a "constant pressure in line 45 approximately pounds per square inch higher than the highest pressure expected in the vessel II]. The relief valve 48 is then set for 25 to 50 pounds higher than the pressure in vessel It) so as to constantly hold a pressure in chamber 33 greater than the pressure inside of vessel I I].
Since valve 44 is a regulating valve and opens only to permit flow in the direction of the arrows when the pressure in line 45 is less than that in line 39; and since valve 48 is a relief valve and opens to permit flow in the direction of the arrow only when the pressure in line 4? is above a predetermined minimum, valves 44- and 48 serve to hold liquid under pressure in sealing chamber I2 if for any reason the pressure should fail in the system 3'I--3839.
In one form of my invention the pump 38 delivers hydraulic fluid at a pressure of about 600 pounds per square inch through line 33, valve 48 and line 32 for the operation of motor I3. By regulating valve 40, the speed of motor I3 may be controlled. Excess oil moving through the pump 38 may flow through line 5i and relief valve 52 back into reservoir 31'.
In cases where even small quantities of oil used in sealing chamber 36 might have a deleterious effect on the chemical reaction of the charge in the vessel Ill, the sealing chamber 36 may be provided with a separate pressure liquid supply system using silicone oil or grease, a medicinal grade of white oil, specially refined petrolatum, or any other lubricant which is chemically inert.
It will be noted that any leakage from the pressure sealing chamber 33 toward the reaction vessel will in any case be very slight and no deleterious chemical can escape from the reaction vessel. The seal 35 creates barrier against free flow between chamber 35 and the interior of the motor I3. However, if any leakage does occur in this direction along shaft 33 upwardly, such leakage returns to the hydraulic system and cannot escape into the room.
Prior constructions known to me have utilized an agitator drive shaft such as that shoWn in United States Patent No. 2,398,944, granted April 23, 1946, to George E. Kopetz. This Kopetz construction provides a sealing chamber somewhat similar to my sealing chamber 38 for preventing leakage from the reaction vessel outwardly along shaft I I. However, the Kopetz shaft extends into atmosphere and any leakage from chamber 36 will cause a messy or even dangerous condition. In contrast to this, it will be noted that my drive shaft I I, 30 ends within the hydraulic system itself and no leakage outside to atmosphere is possible.
What I claim is:
1. In combination, a pressure reaction vessel containing liquid and subject to a predetermined pressure, a rotatable shaft in said vessel and projecting through the wall thereof, a self-contained motor for rotating said shaft and connected to said shaft spaced from said wall, said motor being a hydraulic motor having a shaft aligned with said first-named shaft, sealing means embracing said shaft where it passes through said wall, and an enclosed chamber surrounding said shaft and sealing means, a seal between said chamber and said motor and providing the only dividing means between them, an hydraulic system including a; source of hydraulic pressure fluid connected with said motor for operating it, and means connecting said hydraulic pressure fluid in said chamber, said last named means providing means maintaining pressure in said chamber above said predetermined pressure, whereby said shaft termi- 6 nates at one end inside of said vessel and at the other end inside of said hydraulic system.
2. The combination of claim 1 including valves in said hydrauliic system isolating said chamber from the rest of said system when pressure in the rest of said system falls below said predetermined pressure, whereby if said system falls below said predetermined pressure or if said hydraulic motor fails to maintain rotation of said shaft in said reaction vessel, the pressure liquid in said chamber maintains a seal there.
ERNEST E. ROWLAND.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,855,274 Arutunoff Apr. 26, 1932 2,101,541 Hait Dec. 7, 1937 2,250,714 LaBour July 29, 1941 2,398,944 Kopetz Apr. 23, 1946
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2834619A (en) * 1955-04-15 1958-05-13 United Aircraft Corp Fluid seal means for rotating shafts
US3018628A (en) * 1957-12-27 1962-01-30 Sigma Remote control installations for the valves of marine tankers
US3023580A (en) * 1959-10-28 1962-03-06 Max Isaacson Mixer
US3174405A (en) * 1962-05-23 1965-03-23 Sinclair Research Inc Positive displacement fluid motor
US3191621A (en) * 1963-02-21 1965-06-29 Donkin And Company Ltd Hydraulically-operated valves
US3536302A (en) * 1968-11-21 1970-10-27 King Of Prussia Research & Dev Bearing lubrication for mixer shaft
US3596565A (en) * 1969-07-25 1971-08-03 Duane Edward Atkinson Remotely controlled hydraulic system
US4062269A (en) * 1975-04-21 1977-12-13 Clark Equipment Company Hydraulic cylinder extension control
US4120234A (en) * 1974-07-01 1978-10-17 Ab Vabyma Device for distributing a fluid flow in fixed proportions
US4167171A (en) * 1976-07-06 1979-09-11 Robert Bosch Gmbh Positively lubricated distributor construction for internal combustion engines
US4565453A (en) * 1983-11-21 1986-01-21 Ekato Industrieanlagen Verwaltungsgesellschaft Mbh & Co. Agitator
US20130051906A1 (en) * 2010-04-26 2013-02-28 Itt Manufacturing Enterprises Inc Lead through for digestion tank
US20170071140A1 (en) * 2015-09-10 2017-03-16 Komatsu Ltd. Work vehicle
US10470380B2 (en) * 2016-10-28 2019-11-12 Deere & Company Lubrication system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1855274A (en) * 1929-01-14 1932-04-26 Arutunoff Armais Oil filled submergible electric motor
US2101541A (en) * 1935-04-29 1937-12-07 Fmc Corp Lubricating system for vertical pump shafts
US2250714A (en) * 1937-11-15 1941-07-29 Bour Harry E La Centrifugal pump
US2398944A (en) * 1942-07-21 1946-04-23 Blaw Knox Co Lubricated shaft bearing

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1855274A (en) * 1929-01-14 1932-04-26 Arutunoff Armais Oil filled submergible electric motor
US2101541A (en) * 1935-04-29 1937-12-07 Fmc Corp Lubricating system for vertical pump shafts
US2250714A (en) * 1937-11-15 1941-07-29 Bour Harry E La Centrifugal pump
US2398944A (en) * 1942-07-21 1946-04-23 Blaw Knox Co Lubricated shaft bearing

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2834619A (en) * 1955-04-15 1958-05-13 United Aircraft Corp Fluid seal means for rotating shafts
US3018628A (en) * 1957-12-27 1962-01-30 Sigma Remote control installations for the valves of marine tankers
US3023580A (en) * 1959-10-28 1962-03-06 Max Isaacson Mixer
US3174405A (en) * 1962-05-23 1965-03-23 Sinclair Research Inc Positive displacement fluid motor
US3191621A (en) * 1963-02-21 1965-06-29 Donkin And Company Ltd Hydraulically-operated valves
US3536302A (en) * 1968-11-21 1970-10-27 King Of Prussia Research & Dev Bearing lubrication for mixer shaft
US3596565A (en) * 1969-07-25 1971-08-03 Duane Edward Atkinson Remotely controlled hydraulic system
US4120234A (en) * 1974-07-01 1978-10-17 Ab Vabyma Device for distributing a fluid flow in fixed proportions
US4062269A (en) * 1975-04-21 1977-12-13 Clark Equipment Company Hydraulic cylinder extension control
US4167171A (en) * 1976-07-06 1979-09-11 Robert Bosch Gmbh Positively lubricated distributor construction for internal combustion engines
US4565453A (en) * 1983-11-21 1986-01-21 Ekato Industrieanlagen Verwaltungsgesellschaft Mbh & Co. Agitator
US20130051906A1 (en) * 2010-04-26 2013-02-28 Itt Manufacturing Enterprises Inc Lead through for digestion tank
US8591100B2 (en) * 2010-04-26 2013-11-26 Xylem Ip Holdings Llc Mixer assembly for digestion tank, having a lead through comprising at least three positioning members arranged to determine the mutual position of a first and a second element of the lead through
US20170071140A1 (en) * 2015-09-10 2017-03-16 Komatsu Ltd. Work vehicle
US10362738B2 (en) * 2015-09-10 2019-07-30 Komatsu Ltd. Work vehicle
US10470380B2 (en) * 2016-10-28 2019-11-12 Deere & Company Lubrication system

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