US2791185A - Hydraulic rotary transmission device - Google Patents

Hydraulic rotary transmission device Download PDF

Info

Publication number
US2791185A
US2791185A US444042A US44404254A US2791185A US 2791185 A US2791185 A US 2791185A US 444042 A US444042 A US 444042A US 44404254 A US44404254 A US 44404254A US 2791185 A US2791185 A US 2791185A
Authority
US
United States
Prior art keywords
ring
contour
curve
transmission device
rise
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US444042A
Inventor
Arthur F Bohnhoff
Toschkoff Dimitar
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to US444042A priority Critical patent/US2791185A/en
Application granted granted Critical
Publication of US2791185A publication Critical patent/US2791185A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 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 groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 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 groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C2/3446Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 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 groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface

Definitions

  • This invention relates to hydraulic rotary transmission devices and more particularly pertains to rotary pumpsand-motorsof the .type comprising a circulan rotor adapted to turn within a ring engaged by the outer endsof-a plurality of radially movable vanesU carried., by the rotor, the
  • the principal object of our invention is implicit from the foregoing, i. e., our main purpose is to reduce ring wear, thereby to lengthen the life of the pump or other device and render it maximally eflicient over a longer period.
  • a further and more specific object is to provide a ring for rotary vane hydraulic transmission devices in which the inner contouring is such as to avoid high frequency impingement of the vanes and to substantially lessen variations in the load imposed thereby.
  • a corollary object is the provi-sion of a ring contour whereby (a) Centrifugal force alone will be nearly suticient to maintain vane contac-t at the speeds contemplated.
  • Still another object of the invention is to provide such a contour which is easily land accurately reproduced and which is based on a curve capable of definition by an algebraic equation to the end that for any given applica- Patent/ed May 7, 1,957
  • Fig. l is a side View of a pump conforming to the invention, the pump-cover being removed to showithe principal. parts; Y
  • Figs. 2 and 2A show the development of? the equation'v denitive ofV the cycloidal curve on which tlie infernal contour of the pump -ring is basedyand y
  • Figs. 3-5 are graphs affording@ comparison of' the performance of the pumpf with that of a prior' art pump heretofore used for the particular prposenamelfy, power. steering. 'Phe velocity and' acceleration curves (Figs. 4 ⁇
  • the illus trated pump is ofthe general'type disclosed for instance, in U. S. Patent 2,544,987 to Gardiner etal.
  • the principalparts are-the ring 10,', the rotor 1 ⁇ 2 and the vanes 14, the outer ends of which are maintained against the inner surfaces of the ring ⁇ by centrifugal forcel plus a hydraulic force developed atrk 16, thesecharnbersy 1'6, with the'pump iny operation, being filled withI tluidI under rlisy charge pressure.
  • accumulator or other source,. may v enterthe system
  • FIG. 3-5 The advantage of the cycloidal curve as a basis for the inner contour of the ⁇ ring 10 is demonstrated graphically by Figures 3-5 wherein the symbol P refers to the old contour, and the symbolC to the contour 22.
  • Figure 3 shows the displacement, i. e., the linear distance, expressed in inches, between the contour 22 and the base circle for each'degree. of rotation of the latter through the arc indicated by the arrow (Fig. 1). that the C contour provides for the displacement of substantially more uid in the filling area than the P contour (note thev spread .between the ⁇ curves through the distance 42"--72), a substantial advantage in many ap plications.
  • a hydraulic transmission device of the type includ ing a rotor mounting radially movable vane means and a ring member surrounding and contacting the vane means so as to determine the radial positioning of the latter for each increment of rotation of the rotor, the inner contour of said ring member comprising two rise portions and two fall portions connected by dwell portions of predetermined length, the contour of said rise and fall portions being substantially set by application of the following equation:
  • ⁇ 0o total angular distance from start to end of contour H :total rise (or fall) of contour in angular distance 0o, the units of linear measurement as to S and H being the same, the units of angular measurement as to 0 and 0o likewise being the same.
  • a hydraulic transmission device of the type including a rotor mounting radially movable vane and a ring member surrounding and contacting the vane means so as to determine the radial positioning of the latter for each increment of rotation of the rotor, the inner con tour of said ring member comprising two rise portions and two fall portions connected by dwell portions of predetermined length, said inner contour being based on a curve representing an algebraic summation of an i Archimedes spiral and a sine curve having its generating radius equal to the total rise divided by 21r.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

*May 7, 1957 A. F. BoHNHoFF ET AL 2,791,185
HYDRAULIC ROTARY TRANSMISSION DEVICE 2 Sheets-Sheet 1 Filed July 19, 1954 May `7, 1957 A, F. BoHNHor-'F x-:T AL
HYDRAULIC ROTARY TRANSMISSION DEVICE 2 Sheets-Sheet 2 Filed July 19, 1954 HYDAULIC ROTARY TR AN 'SlVISSllI DEVICE rthnr' F. Bolinhoft and D'iinitar Toscliliolf, Saginaw, Mc'h'., a's'signrs to'f General Motors; Corporation, Dc-
tr'ot, Micha; a corporation of' Delaware- Application Jul-y 1'9', 1954, S'erialb'. 444,042 zr Clarins. (armar-136)@ This invention relates to hydraulic rotary transmission devices and more particularly pertains to rotary pumpsand-motorsof the .type comprising a circulan rotor adapted to turn within a ring engaged by the outer endsof-a plurality of radially movable vanesU carried., by the rotor, the
surface of the ringy in which the rotorl turns a condition-i, which in time is` boundtobe reflected in; the operating efficiency. of the pump.
T'he. present invention iSv-based on the-disfcovery thatlthel wearing qualities of the pump ring aredeterxninedfby the internalcontouring thereof'. Moref specifically, we have found` that the pump `ring-.wear inthe-case of thefpreviousy designs owes to .the fact that the vanes do not contact the ring inthe essentially evenV anduniform manner supposed. Rathenthecontact- (especially at high speeds) is marked in certain areas byhigh frequency impingement ori tle'vane'slag-ains-tthe ring surfaces and in other areas variationsin the load applied: against: the ring surfaces bythe vaines: f v
@onside'riigtheforegoing, itshould? bel clearfthat ring wear isa f'ri'ctionof shock and that* the 'degree' of' shock relates to the radial acceleration characteristics of the vanes as set by the ring contour. Obviously the shock will be greater the greater the value of (F) in the formula (F) =Ma, where M equals the mass of the vane and a its radial acceleration.
The principal object of our invention is implicit from the foregoing, i. e., our main purpose is to reduce ring wear, thereby to lengthen the life of the pump or other device and render it maximally eflicient over a longer period. A further and more specific object is to provide a ring for rotary vane hydraulic transmission devices in which the inner contouring is such as to avoid high frequency impingement of the vanes and to substantially lessen variations in the load imposed thereby. A corollary object is the provi-sion of a ring contour whereby (a) Centrifugal force alone will be nearly suticient to maintain vane contac-t at the speeds contemplated.
(b) Vane acceleration is zero lat the beginning and at the end of rise.
(c) Though retaining features (a) and (b), displacement in the intake areas is greater than in the case of conventional devices of similar design.
Still another object of the invention is to provide such a contour which is easily land accurately reproduced and which is based on a curve capable of definition by an algebraic equation to the end that for any given applica- Patent/ed May 7, 1,957
tion the radial velocity and acceleration of.v thevanes and" the physical dimensions and properties of' the contour can be readily determined, regardless ofV the amount of rise and the travel used to achieve it. l
In the accompanying drawings which will be referred tofin thev further description: Y
Fig. l is a side View of a pump conforming to the invention, the pump-cover being removed to showithe principal. parts; Y
Figs. 2 and 2A show the development of? the equation'v denitive ofV the cycloidal curve on which tlie infernal contour of the pump -ring is basedyand y Figs. 3-5 are graphs affording@ comparison of' the performance of the pumpf with that of a prior' art pump heretofore used for the particular prposenamelfy, power. steering. 'Phe velocity and' acceleration curves (Figs. 4`
and 5) are for nf=1000 R. P. M; v
Referring. rst to Figi 1it willbe seen. that the illus trated pump is ofthe general'type disclosed for instance, in U. S. Patent 2,544,987 to Gardiner etal. Thus, the principalparts are-the ring 10,', the rotor 1`2 and the vanes 14, the outer ends of which are maintained against the inner surfaces of the ring` by centrifugal forcel plus a hydraulic force developed atrk 16, thesecharnbersy 1'6, with the'pump iny operation, being filled withI tluidI under rlisy charge pressure. As well understood: on turningY ofthe rotor 12 counterclocloiviseI (clockwise rotationmay be provided for by means of the expedient of'an interchangeable cover piece altering. the porting. as'required) the inner vane chambers become-lledwith oil inthe vicinity ofthe inletports 1S and discharge oil in the vicinity of the outletports 20, the vanes 1'4A mov-ingin or out as determined by the lring contour 22.- y
It shouldbe, evident that the construction shown is adapted for use as ahydraulic' motor. as'well.v as a pinp. WhenV so appliedt1he pressure fluid,.supplied from. apump,
accumulator, or other source,. may v enterthe system;
through. either the ports, 1S or ZO The rotary motionof the rotor shaft' induced by the impact'ofA the lluidagainstl the vanesimay be translated by knowny means iiito'an'y othervv type of motion which may be` dsi`re'd. l
We' have broughtl out' in therforepart hereof the' ini# portance: of the inner contoin`` 22' of thering' 102 In acl cordancewith our invention; we bas' this" co' 1"itoir"on'v a' ey'e'lo'idally'l formed crve StichI4 a curve as illustrated by' of a point on the straight line (or spiral) OA minus the displacement (-H sine 2 21r 7F00 of a point on the circumference of the generating circle of radius whose center moves along the line (or spiral) OA while it rotates through the angle senting an algebraic summation of an Archimedes spiral and a sine curve having its generating radius equal to thctotal risc divided by 21r.
The advantage of the cycloidal curve as a basis for the inner contour of the` ring 10 is demonstrated graphically by Figures 3-5 wherein the symbol P refers to the old contour, and the symbolC to the contour 22. Figure 3 shows the displacement, i. e., the linear distance, expressed in inches, between the contour 22 and the base circle for each'degree. of rotation of the latter through the arc indicated by the arrow (Fig. 1). that the C contour provides for the displacement of substantially more uid in the filling area than the P contour (note thev spread .between the `curves through the distance 42"--72), a substantial advantage in many ap plications.
ly sufficient to maintain contact between the vanes and ring in the instance of curve C, an infinite acceleration is demanded in the case of curve P to effect the contact at the beginningA of the rise. As a consequence, using curve P, there is no contact on initiation of the rise and when contact does occur it is so abrupt as to cause dcformation of the ring surfaces. Similar contact with similar eects, occurs (curve P) at the end of the rise, on the abrupt reversal in the direction of radial movement of the vanes without a dwell. In other words, this sharp reversal results in momentary loss of contact, followed by a quick, hard rebound of the vanes against the ring, spelling obvious adverse effects on the ring surfaces involved. Continuing with reference to curve P, it should be clear that the stepping of this curve between the rise and fall retiects changes in acceleration which are also adverse from a wear standpoint, even though vane contact may be maintained through the area. In practical effect the symmetry of curve C means that such wearing The figure demonstrates i of theiring surfaces as may occur is substantially uniform,
4without pitting orl indentation.- VSignificantly the vanes have zero acceleration both at the beginning and at the end of the rise.
Having thus described and illustrated our invention what we claim is:
1. A hydraulic transmission device of the type includ ing a rotor mounting radially movable vane means and a ring member surrounding and contacting the vane means so as to determine the radial positioning of the latter for each increment of rotation of the rotor, the inner contour of said ring member comprising two rise portions and two fall portions connected by dwell portions of predetermined length, the contour of said rise and fall portions being substantially set by application of the following equation:
`0o=total angular distance from start to end of contour H :total rise (or fall) of contour in angular distance 0o, the units of linear measurement as to S and H being the same, the units of angular measurement as to 0 and 0o likewise being the same.
2. A hydraulic transmission device of the type including a rotor mounting radially movable vane and a ring member surrounding and contacting the vane means so as to determine the radial positioning of the latter for each increment of rotation of the rotor, the inner con tour of said ring member comprising two rise portions and two fall portions connected by dwell portions of predetermined length, said inner contour being based on a curve representing an algebraic summation of an i Archimedes spiral and a sine curve having its generating radius equal to the total rise divided by 21r.
References Cited in the tile of this patent UNITED STATES PATENTS 2,165,963 Curtis July 11, 1939 2,272,635 Davis Feb. 10, 1942 2,321,190 Ellinwood June 8, 1943 2,470,987 Johnson May 24, 1949 2,588,430 Svenson Mar. 1l, 1952
US444042A 1954-07-19 1954-07-19 Hydraulic rotary transmission device Expired - Lifetime US2791185A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US444042A US2791185A (en) 1954-07-19 1954-07-19 Hydraulic rotary transmission device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US444042A US2791185A (en) 1954-07-19 1954-07-19 Hydraulic rotary transmission device

Publications (1)

Publication Number Publication Date
US2791185A true US2791185A (en) 1957-05-07

Family

ID=23763245

Family Applications (1)

Application Number Title Priority Date Filing Date
US444042A Expired - Lifetime US2791185A (en) 1954-07-19 1954-07-19 Hydraulic rotary transmission device

Country Status (1)

Country Link
US (1) US2791185A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3076415A (en) * 1960-01-08 1963-02-05 Bendix Corp Reversible vane fluid power device such as a pump or motor
US3096932A (en) * 1960-11-22 1963-07-09 Jr Samuel W Traylor Air pump
US3191853A (en) * 1964-11-16 1965-06-29 Worthington Corp Rotary compressor
DE1224150B (en) * 1958-05-30 1966-09-01 Gunnar Axel Wahlmark Rotary piston machine
US3374943A (en) * 1966-08-15 1968-03-26 Kenneth G Cervenka Rotary gas compressor
US3549289A (en) * 1969-04-03 1970-12-22 David G Skagen Fluid motor
US4556372A (en) * 1983-06-16 1985-12-03 Robert Bosch Gmbh Positive displacement machine having improved displacement curve
US4616984A (en) * 1984-03-14 1986-10-14 Nippondenso Co., Ltd. Sliding-vane rotary compressor with specific cylinder bore profile
US4712987A (en) * 1985-05-22 1987-12-15 Diesel Kiki Co., Ltd. Vane compressor provided with endless camming surface minimizing torque fluctuations
US4738603A (en) * 1983-03-08 1988-04-19 Kabushiki Kaisha Toyota Chuo Kenkyusho Hydraulic vane pump
US5702242A (en) * 1994-04-26 1997-12-30 Luk Fahrzeug-Hydraulik Gmbh & Co. Vane pump
CN103807092A (en) * 2014-02-26 2014-05-21 上海交通大学 Cam rotor of cam rotor blade type hydraulic servo motor
DE102013110351A1 (en) * 2013-09-19 2015-03-19 Hella Kgaa Hueck & Co. Vane pump

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2165963A (en) * 1938-04-25 1939-07-11 Curtis Pump Co Constant flow nonpulsating pump
US2272635A (en) * 1939-11-03 1942-02-10 Walwin L Davis Balanced rotary pump
US2321190A (en) * 1940-03-30 1943-06-08 Adel Prec Products Corp Rotary pump
US2470987A (en) * 1947-09-03 1949-05-24 James P Johnson Rotary pump stator
US2588430A (en) * 1945-10-15 1952-03-11 Odin Corp Rotary blade pump

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2165963A (en) * 1938-04-25 1939-07-11 Curtis Pump Co Constant flow nonpulsating pump
US2272635A (en) * 1939-11-03 1942-02-10 Walwin L Davis Balanced rotary pump
US2321190A (en) * 1940-03-30 1943-06-08 Adel Prec Products Corp Rotary pump
US2588430A (en) * 1945-10-15 1952-03-11 Odin Corp Rotary blade pump
US2470987A (en) * 1947-09-03 1949-05-24 James P Johnson Rotary pump stator

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1224150B (en) * 1958-05-30 1966-09-01 Gunnar Axel Wahlmark Rotary piston machine
US3076415A (en) * 1960-01-08 1963-02-05 Bendix Corp Reversible vane fluid power device such as a pump or motor
US3096932A (en) * 1960-11-22 1963-07-09 Jr Samuel W Traylor Air pump
US3191853A (en) * 1964-11-16 1965-06-29 Worthington Corp Rotary compressor
US3374943A (en) * 1966-08-15 1968-03-26 Kenneth G Cervenka Rotary gas compressor
US3549289A (en) * 1969-04-03 1970-12-22 David G Skagen Fluid motor
US4738603A (en) * 1983-03-08 1988-04-19 Kabushiki Kaisha Toyota Chuo Kenkyusho Hydraulic vane pump
US4556372A (en) * 1983-06-16 1985-12-03 Robert Bosch Gmbh Positive displacement machine having improved displacement curve
US4616984A (en) * 1984-03-14 1986-10-14 Nippondenso Co., Ltd. Sliding-vane rotary compressor with specific cylinder bore profile
US4712987A (en) * 1985-05-22 1987-12-15 Diesel Kiki Co., Ltd. Vane compressor provided with endless camming surface minimizing torque fluctuations
AU580872B2 (en) * 1985-05-22 1989-02-02 Zexel Corporation Vane compressor provided with endless camming surface minimizing torque fluctuations
US5702242A (en) * 1994-04-26 1997-12-30 Luk Fahrzeug-Hydraulik Gmbh & Co. Vane pump
DE102013110351A1 (en) * 2013-09-19 2015-03-19 Hella Kgaa Hueck & Co. Vane pump
US9765775B2 (en) 2013-09-19 2017-09-19 Hella Kgaa Hueck & Co. Vane pump
CN103807092A (en) * 2014-02-26 2014-05-21 上海交通大学 Cam rotor of cam rotor blade type hydraulic servo motor

Similar Documents

Publication Publication Date Title
US2791185A (en) Hydraulic rotary transmission device
US3515395A (en) Unidirectional pumping seal
US3246574A (en) Rotor assembly in vane machine with pressure balance devices
US1996875A (en) Fluid motor and pump
US2527536A (en) Rotary screw pump
US1989552A (en) Rotary compressor
US3277833A (en) Hydraulic device
US2891482A (en) Rotary machine adapted to operate as a pump or as a fluid motor
US2985110A (en) Pump construction
US2543603A (en) Fluid operated variable-speed power-transmitting device
US2417568A (en) Rotary vane type pump
US2439668A (en) Pump or compressor
US2377674A (en) Hydraulic shock absorber sealing
US3447476A (en) Rotary fluid device
US3125962A (en) figure
US2278740A (en) Rotary pump
US2318346A (en) Rotary pump
US4021162A (en) Vane-type rotary machines
US2989005A (en) Fluid apparatus
US10012081B2 (en) Multi-vane impeller device
US4772192A (en) Vane-type compressor
US3918859A (en) Valveless rotary piston expansion engine
US2588032A (en) Rotary pump
US1336845A (en) Rotary engine or pump
GB922121A (en) Improvements in or relating to rotary pumps or motors