US3876344A - Counterbalance for rotary engine - Google Patents

Counterbalance for rotary engine Download PDF

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Publication number
US3876344A
US3876344A US358307A US35830773A US3876344A US 3876344 A US3876344 A US 3876344A US 358307 A US358307 A US 358307A US 35830773 A US35830773 A US 35830773A US 3876344 A US3876344 A US 3876344A
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counterbalance
rotor
disc
shaft
rotation
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US358307A
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Leonard R Nestor
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/22Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/003Systems for the equilibration of forces acting on the elements of the machine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005Wankel engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines

Definitions

  • FIGS. I, 2 and 3 are fragmentary views primarily in section of three modifications of my novel counterbalance as installed in modified forms of the engine of FIGS. l and 2 of said Ser. No. 203,211;
  • FIG. 4 is a partial sectional elevation taken approximately at line 44 of FIG. 2, showing the counterbalance unit in front elevation and as installed, and
  • FIGS. 5 and 6 are front elevations of the counterbalance units of FIGS. 1 and 3 respectively.
  • the rotary engine 10 includes a stator side wall ll, rotor side wall 12, shaft 13, and counterbalance unit 14.
  • the latter includes a guide disc disposed within the circular central opening 16 in the rotor wall, a ring 17 disposed within the circular central opening 18 in the stator wall. and a counterbalance weight 19 extending from said ring in a plane parallel to said disc and enclosed within a casing 20 fastened to the stator side wall.
  • a hub opening extends through disc, ring and weight to receive a tubu lar support member 21 within which the shaft 13 rotates.
  • the support member here serves to support a fixed spur gear, not shown, located within the rotor as part of the constraining mechanism therefor, as shown in my application Ser. No, 203,211, but in other forms of rotary engines may be omitted.
  • the counterbalance unit then being rotatively mounted directly on the shaft 13.
  • the rotary engine of FIGS. 2 and 4 similarly include stator side wall 31, rotor side wall 32, shaft 33, and counterbalance unit 34.
  • the balance weight 39 is attached directly to the guide disc and rotates directly adjacent the rotor side wall, the stator wall 31 extending inwardly only to the rim of the outer casing 40.
  • the disc 35 is here seen as perforated throughout the portion lying opposite the balance weight 39, the perforations 42 serving to reduce the weight of that portion of the disc and thereby permitting a reduction in the weight of the counterbalance and making possible the cooling of the rotor by forced air flow if desired.
  • the perforated disc fails to isolate the interior of the rotor, which isolation may in some instances be desirable, e.g. in obtaining improved lubrication.
  • the counterbalance unit 54 of FIGS. 3 and 6 again, as in FIG. 2, has the weight 59 joined directly to the disc 55.
  • the latter is extended out wardly around the central opening to form a wide lip 56, and the disc 55 is made to similar width.
  • the unbalanced portion of the disc is then reduced in thickness to provide a thin web portion 63, the structure effectively isolating the interior of the rotor while reducing unbalanced weight in the sealing disc.
  • the invention has been here presented primarily in terms of a single counterbalance unit applied to a rotary engine of a particular type.
  • the invention is not to be construed as limited to such structure, since the same counterbalance unit and method may be applied at ei ther or both sides of rotary engines, pumps, or other analogous rotary devices of analogous structure and operating characteristics.
  • a counterbalance unit for a rotary device having a drive shaft and a rotor disposed for oscillative rota tion about said shaft and having side plates with circular central openings, said unit comprising a guide disc fitting within a said rotor plate opening for rotation therein and having an off-center circular hub opening for rotation of said shaft, and a counterbalance weight integral with said disc and extending from one side of said disc to oscillative rotation outside of said rotor plate.
  • a rotary engine comprising a stator having side plates each with an axial opening; a drive shaft extending through the stator side plate openings; a rotor, having side plates each with an axial circular opening, for oscillative rotation within said stator and about said shaft; and, at least at one side of said engine, a counterbalance unit rotating about said shaft and comprising a guide disc rotating within the rotor side plate opening and having an offcenter circular hub opening for rotation of said shaft therein, and a counterbalance weight integral with said disc and disposed outwardly of said rotor side plate.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

A counterbalance for a rotary engine, e.g. of the type described in application Ser. No. 203,211 now U.S. Pat. No. 3,744,941, includes a disc rotating about the drive shaft and within the rotor side wall opening, and a counterbalance weight suspended therefrom.

Description

United States Patent [:91
Nestor 5] Apr. 8, 1975 COUNTERBALANCE FOR ROTARY 2.933.239 4/:900 Blackman 4I8/l5! ENGINE 3.042.009 7/1962 Froede et al 418/6! A 3.377.873 4/1968 Patterson 418/151 Inventor: Leonard Nestor. 2 M g i 3.387.772 6/[968 Wutz 418/15! Ave. St. Paul, Minn. 3.452.643 7/1969 Pratt 418/!5l [22] Filed: May 8, 1973 [211 A I N 358 307 Primary Examiner-John J. Vrablik [57] ABSTRACT [52] U.S.Cl. ..4l8/61A;4l8/i5l A b] r f 511 im. c|...,., FOlc i/02; FOlc 21/00; F040 29/00 Mary 0 type [58] Field of Search H 8/61 A '5] described in application Ser. No. 203,2ll now U.S. Pat. No. 3,744,94l, includes a disc rotating about the [56] References Cited drive shaft and within the rotor side wall opening. and
UNITED STATES PATENTS a counterbalance weight suspended therefrom. 1.890.614 IZ/I932 Klopsteg 4l8/l5l 3 Claims, 6 Drawing Figures COUNTERBALANCE FOR ROTARY ENGINE This inventnion relates to rotary engines and in particular to means for reducing the vibrations associated with their normal operation.
In my copending application Ser. No. 203,21 l filed Nov. 30, l97l, now U.S. Pat. No. 3,744,94l I describe an improved form of rotary engine wherein a multisided rotor, oscillatively revolving within a multi-lobed epitrochoidal stater cavity, is constrained by means of internal supporting mechanism to follow accurately the curved internal stator surface. While the amount of vibration is thereby substantially reduced below that obtained with earlier rotary engines, I have now found it possible to achieve further desirable reduction in vibration of this, as well as significant reduction in the vibration of earlier forms of rotary engines, by counterbalance means now to be described.
In the drawing,
FIGS. I, 2 and 3 are fragmentary views primarily in section of three modifications of my novel counterbalance as installed in modified forms of the engine of FIGS. l and 2 of said Ser. No. 203,211;
FIG. 4 is a partial sectional elevation taken approximately at line 44 of FIG. 2, showing the counterbalance unit in front elevation and as installed, and
FIGS. 5 and 6 are front elevations of the counterbalance units of FIGS. 1 and 3 respectively,
Referring first to FIGS. 1 and 5, the rotary engine 10 includes a stator side wall ll, rotor side wall 12, shaft 13, and counterbalance unit 14. The latter includes a guide disc disposed within the circular central opening 16 in the rotor wall, a ring 17 disposed within the circular central opening 18 in the stator wall. and a counterbalance weight 19 extending from said ring in a plane parallel to said disc and enclosed within a casing 20 fastened to the stator side wall. A hub opening extends through disc, ring and weight to receive a tubu lar support member 21 within which the shaft 13 rotates. The support member here serves to support a fixed spur gear, not shown, located within the rotor as part of the constraining mechanism therefor, as shown in my application Ser. No, 203,211, but in other forms of rotary engines may be omitted. the counterbalance unit then being rotatively mounted directly on the shaft 13.
It will be understood that suitable bushings or bearings are provided between disc and rotor side wall, ring and stator side wall, inner hub surface and outer tubular support surface, and elsewhere as required, but have here been emitted both for clarity of illustration and as forming no part of the present invention.
The rotary engine of FIGS. 2 and 4 similarly include stator side wall 31, rotor side wall 32, shaft 33, and counterbalance unit 34. In this modification the balance weight 39 is attached directly to the guide disc and rotates directly adjacent the rotor side wall, the stator wall 31 extending inwardly only to the rim of the outer casing 40. The disc 35 is here seen as perforated throughout the portion lying opposite the balance weight 39, the perforations 42 serving to reduce the weight of that portion of the disc and thereby permitting a reduction in the weight of the counterbalance and making possible the cooling of the rotor by forced air flow if desired. However, the perforated disc fails to isolate the interior of the rotor, which isolation may in some instances be desirable, e.g. in obtaining improved lubrication.
The counterbalance unit 54 of FIGS. 3 and 6 again, as in FIG. 2, has the weight 59 joined directly to the disc 55. In order to obtain increased bearing surface between disc and rotor wall, the latter is extended out wardly around the central opening to form a wide lip 56, and the disc 55 is made to similar width. The unbalanced portion of the disc is then reduced in thickness to provide a thin web portion 63, the structure effectively isolating the interior of the rotor while reducing unbalanced weight in the sealing disc.
It will be understood that the dimensions of the several components will be selected consistent with the materials of construction employed and with the partic ular engine structure under consideration, with a view to compensating for the inherent imbalance of the rotor assembly. Minor deviations may later be made in the completed device to further reduce any subsequently appearing imbalance, e.g. by drilling or plugging the counterbalance unit at appropriate points. The engine structure will be seen to permit such changes in a simple manner due to the ease of removal of the outer casing.
To facilitate illustration and description, the invention has been here presented primarily in terms of a single counterbalance unit applied to a rotary engine of a particular type. However the invention is not to be construed as limited to such structure, since the same counterbalance unit and method may be applied at ei ther or both sides of rotary engines, pumps, or other analogous rotary devices of analogous structure and operating characteristics.
What is claimed is as follows:
1. A counterbalance unit for a rotary device having a drive shaft and a rotor disposed for oscillative rota tion about said shaft and having side plates with circular central openings, said unit comprising a guide disc fitting within a said rotor plate opening for rotation therein and having an off-center circular hub opening for rotation of said shaft, and a counterbalance weight integral with said disc and extending from one side of said disc to oscillative rotation outside of said rotor plate.
2. A rotary engine comprising a stator having side plates each with an axial opening; a drive shaft extending through the stator side plate openings; a rotor, having side plates each with an axial circular opening, for oscillative rotation within said stator and about said shaft; and, at least at one side of said engine, a counterbalance unit rotating about said shaft and comprising a guide disc rotating within the rotor side plate opening and having an offcenter circular hub opening for rotation of said shaft therein, and a counterbalance weight integral with said disc and disposed outwardly of said rotor side plate.
3. Engine of claim 2 wherein said counterbalance weight is disposed outwardly of said stator side plate. l

Claims (3)

1. A counterbalance unit for a rotary device having a drive shaft and a rotor disposed for oscillative rotation about said shaft and having side plates with circular central openings, said unit comprising a guide disc fitting within a said rotor plate opening for rotation therein and having an off-center circular hub opening for rotation of said shaft, and a counterbalance weight integral with said disc and extending from one side of said disc to oscillative rotation outside of said rotor plate.
2. A rotary engine comprising a stator having side plates each with an axial opening; a drive shaft extending through the stator side plate openings; a rotor, having side plates each with an axial circular opening, for oscillative rotation within said stator and about said shaft; and, at least at one side of said engine, a counterbalance unit rotating about said shaft and comprising a guide disc rotating within the rotor side plate opening and having an offcenter circular hub opening for rotation of said shaft therein, and a counterbalance weight integral with said disc and disposed outwardly of said rotor side plate.
3. Engine of claim 2 wherein said counterbalance weight is disposed outwardly of said stator side plate.
US358307A 1973-05-08 1973-05-08 Counterbalance for rotary engine Expired - Lifetime US3876344A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4278409A (en) * 1977-01-07 1981-07-14 Borsig Gmbh Compressor
US4522574A (en) * 1982-10-27 1985-06-11 Hitachi, Ltd. Balancing weight device for scroll-type fluid machine
IT202100004790A1 (en) * 2021-03-02 2022-09-02 Lonati Spa HANDLING DEVICE.

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1890614A (en) * 1932-12-13 klopsteg
US2933239A (en) * 1957-12-06 1960-04-19 Mcdonald L Stephens Gas compressor
US3042009A (en) * 1958-10-02 1962-07-03 Nsu Motorenwerke Ag Cooling arrangement for rotary mechanisms
US3377873A (en) * 1965-12-08 1968-04-16 Char Lynn Co Counterweight or the like for gerotor gear set
US3387772A (en) * 1965-02-04 1968-06-11 Leybold Heraeus Gmbh & Co Kg Rotary vacuum pump
US3452643A (en) * 1966-08-22 1969-07-01 Harold A Pratt Rotary steam engine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1890614A (en) * 1932-12-13 klopsteg
US2933239A (en) * 1957-12-06 1960-04-19 Mcdonald L Stephens Gas compressor
US3042009A (en) * 1958-10-02 1962-07-03 Nsu Motorenwerke Ag Cooling arrangement for rotary mechanisms
US3387772A (en) * 1965-02-04 1968-06-11 Leybold Heraeus Gmbh & Co Kg Rotary vacuum pump
US3377873A (en) * 1965-12-08 1968-04-16 Char Lynn Co Counterweight or the like for gerotor gear set
US3452643A (en) * 1966-08-22 1969-07-01 Harold A Pratt Rotary steam engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4278409A (en) * 1977-01-07 1981-07-14 Borsig Gmbh Compressor
US4522574A (en) * 1982-10-27 1985-06-11 Hitachi, Ltd. Balancing weight device for scroll-type fluid machine
IT202100004790A1 (en) * 2021-03-02 2022-09-02 Lonati Spa HANDLING DEVICE.
WO2022184347A1 (en) * 2021-03-02 2022-09-09 Lonati S.P.A. Movement device
US12006827B2 (en) 2021-03-02 2024-06-11 Lonati S.P.A. Movement device

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