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US2322608A - Engine starting mechanism - Google Patents

Engine starting mechanism Download PDF

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Publication number
US2322608A
US2322608A US403214A US40321441A US2322608A US 2322608 A US2322608 A US 2322608A US 403214 A US403214 A US 403214A US 40321441 A US40321441 A US 40321441A US 2322608 A US2322608 A US 2322608A
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United States
Prior art keywords
engine
rollers
motor
levers
engine starting
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Expired - Lifetime
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US403214A
Inventor
Sidney H Webster
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Bendix Aviation Corp
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Bendix Aviation Corp
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
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Priority to US403214A priority Critical patent/US2322608A/en
Application granted granted Critical
Publication of US2322608A publication Critical patent/US2322608A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N19/00Starting aids for combustion engines, not otherwise provided for
    • F02N19/001Arrangements thereof
    • 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
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D41/00Freewheels or freewheel clutches
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/13Machine starters
    • Y10T74/131Automatic
    • Y10T74/134Clutch connection

Definitions

  • starting mechanism and particularly to starting mechanism of the type adapted to impart initial rotary movement to the crank-shaft of an internal combustion engine.
  • One of the objects of the invention is to provide powerful, positive starting means embodied in a unit that is attachable to the engine housing in such a manner as to constitute an integrated component of the engine, with the major por tion of the starter assembly actually disposed within the bounds of the engine crank-case.
  • Another object is t render possible such an internal disposition of the major'portion of the starter, whether the installation be on a radial or on a rectilinear engine.
  • Another object is to provide, in an engine starter, novel engine-engaging mechanism adapted to permit overrun of the engaged engine. member in response to the impetus resulting from fuel combustion in the engine itself.
  • Another object is to provide, in an engine engine engaging mechanism adapted to permit overrun of the engaged engipe member in response to any reversely directed impetus, such as'is sometimes caused by pre-' mature combustion as on the compression stroke (ones-2s)
  • This invention relates to engine starting elements 6 and I, and a starting motor (electric or non-electric, but shown as electric) provided with a flanged casing II is mounted so that its power shaft l2 aligns with said common axis.
  • Bolts i3 pass through flanges ll of the motor in continuous mesh with a plurality of, preferably three, equally spaced identical planetary gears, one of which is shown at 32.
  • the planetary gears 32 are encircled by and in mesh with the accompanyingdrawing wherein is illustrated drawing is for the purpose of illustration only,
  • Fig. 1 is a longitudinal sectional view of, a device embodying the invention
  • Fig. 2 is a view along line 22 of Fig. 1;
  • Figs. 3 and 4 show the parts of Fig. 2 in dif- .ferent relationships.
  • the crank-case 5 is provided with a circular opening whose center is on the common axis of a non-rotable internal gear member 33 preferably provided with an integral flange 34 clamped in place (as by bolts l3 and I1) between the 32, and concentric therewith, are planetary gears 35; said gears 35 having a smaller diameter and fewer teeth, which are in mesh with a rotatable internal gear 36, the latter also having a somewhat smaller diameter and fewer teeth than internal gear 33.
  • the internal gear 36 is preferably an integral part of a cup-shaped element 31 whose central portion 23 is centrally recessed toreceive a fraction-reducing bushing 33, and also to receive the hub 39 of engine member 6.
  • the plurality of planetary gears may be assembled in a spider construction comprising centrally perforated sections 40 and II on 23 constitutes the inner race of my novel selfreleasing clutch assembly; the outer race being constituted by the engine member 6.
  • a roller-bearing cage composed of annular rings ii and 52, and a plurality of rollers 53, each having reduced ends for reception in the holes of the rings 5
  • a plurality of levers 56 are pivotally mounted in pockets cut in the member 23, and springs 53 yieldably urge the levers 56 toward the peripheries of rollers 63 wherefore driving relationship is established (see Fig.
  • rollers 53 I When such speed predominance occurs rollers 53 I will be carried forward sufliciently (see Fig. 2) to. .permit free rolling action, as in conventional overrunning clutches.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transmission Devices (AREA)

Description

' June 22, 1943. Q s H EBS 2,322,608 V ENGINE STARTING MECHANISJM I Filed J l 19, 1941 1e 1e V Fpg.1.
56 INVENTOR 6 Patented June 22, 1943 s PATENT OFFICE starter, novel UNITED STATE ENGINE STARTING MECHANISM Sidney H. Webster. Bogota, N. J., assignor to. Bendix Aviation Corporation, South Bend, Ind.,
a corporation of Delaware Application July 19, 1941, Serial No. 403,214
2 Claims.
mechanism, and particularly to starting mechanism of the type adapted to impart initial rotary movement to the crank-shaft of an internal combustion engine.
One of the objects of the invention is to provide powerful, positive starting means embodied in a unit that is attachable to the engine housing in such a manner as to constitute an integrated component of the engine, with the major por tion of the starter assembly actually disposed within the bounds of the engine crank-case.
Another object is t render possible such an internal disposition of the major'portion of the starter, whether the installation be on a radial or on a rectilinear engine.
Another object is to provide, in an engine starter, novel engine-engaging mechanism adapted to permit overrun of the engaged engine. member in response to the impetus resulting from fuel combustion in the engine itself.
Another object is to provide, in an engine engine engaging mechanism adapted to permit overrun of the engaged engipe member in response to any reversely directed impetus, such as'is sometimes caused by pre-' mature combustion as on the compression stroke (ones-2s) This invention relates to engine starting elements 6 and I, and a starting motor (electric or non-electric, but shown as electric) provided with a flanged casing II is mounted so that its power shaft l2 aligns with said common axis.
Bolts i3 pass through flanges ll of the motor in continuous mesh with a plurality of, preferably three, equally spaced identical planetary gears, one of which is shown at 32. The planetary gears 32 are encircled by and in mesh with the accompanyingdrawing wherein is illustrated drawing is for the purpose of illustration only,
and is not designed as a definition of the limits of the invention, reference being had to the appended claims for this purpose.
In the drawing:
Fig. 1 is a longitudinal sectional view of, a device embodying the invention;
Fig. 2 is a view along line 22 of Fig. 1; and
Figs. 3 and 4 show the parts of Fig. 2 in dif- .ferent relationships.
In the drawing reference character 5 designates a portion of a crank-case which encloses the rotatable elements 3 and I of the engine crank-shaft assembly; the said elements 6 and I being journaled in suitable bearings (not shown) supported on the crank-case 5, and said elements being preferably in splined inter-engagement, as indicated at 8, wherefore unitary rotation is assured.
The crank-case 5 is provided with a circular opening whose center is on the common axis of a non-rotable internal gear member 33 preferably provided with an integral flange 34 clamped in place (as by bolts l3 and I1) between the 32, and concentric therewith, are planetary gears 35; said gears 35 having a smaller diameter and fewer teeth, which are in mesh with a rotatable internal gear 36, the latter also having a somewhat smaller diameter and fewer teeth than internal gear 33. The internal gear 36 is preferably an integral part of a cup-shaped element 31 whose central portion 23 is centrally recessed toreceive a fraction-reducing bushing 33, and also to receive the hub 39 of engine member 6.
If desired, the plurality of planetary gears may be assembled in a spider construction comprising centrally perforated sections 40 and II on 23 constitutes the inner race of my novel selfreleasing clutch assembly; the outer race being constituted by the engine member 6. Interposed between 23 and 6 is a roller-bearing cage composed of annular rings ii and 52, and a plurality of rollers 53, each having reduced ends for reception in the holes of the rings 5| and 52. A plurality of levers 56 are pivotally mounted in pockets cut in the member 23, and springs 53 yieldably urge the levers 56 toward the peripheries of rollers 63 wherefore driving relationship is established (see Fig. 3) for transmission of torque from part 23 to engine member 6, by way of elements 56 and 53, upon rotation of member 23 in the direction indicated by the'arrows in Fig. 2. Inthis manner initial rotation or the engine crankshaft is brought about; and if there is no backfire to interrupt the cranking" action, the engine's own fuel combustion cycle will eventually cause member 6 to acquire a speed in excess of that of element 23 of the starter.
When such speed predominance occurs rollers 53 I will be carried forward sufliciently (see Fig. 2) to. .permit free rolling action, as in conventional overrunning clutches.
If, on the other hand, there shouldoccur, during the cranking process, a reverse rotational impulse (backfire") applied to member 6, such impulse will tend to throw rollers 53 to the rear, in relation to the direction of rotation of levers 56 and'member 23 (see Fig. 4) wherefore said rollers will ride off the high points 6! of levers 58, and then roll freely on their individual axes until such time as the reverse rotation of mem'- her 6 ceases. When such cessation occurs the levers 56 will again operatively connect the forwardly rotating driving member 23 with said member 8, to resume the cranking process.
Should any occasion arise wherein the 0pposing inertia of the engine is too great to be overcome by the driving pressure exerted on rollers 53 by spring-pressed levers 56, the said levers will slip past the rollers," into the positionindicated in Fig. 4, precisely as in the case of a backfire." In this manner, the starter parts, including the motor, are protected against overload.
What is claimed is: 1. The combination, with anengine member having an inner cylindrical surface, of a roller cage having a plurality of rollers engageable with said inner surface, to rotate the latter and to subsequently roll freely thereon, a driving motor,'means responsive to rotation of said motor to transmit driving torque to said engine member, by way of said rollers, said means comprising a motor-driven member rotatable with in said roller cage, and means carried by said motor driven member for yielding engagement with the rollers of said cage, to exert upon said rollers a radially directed pressure suflicient to rotate said engine member, said means comprising pivoted levers having highf points from which said rollers may ride off in either direction, according-to the torque conditions encountered.
2; The combination, with a driven member having an inner cylindrical surface, of a plurality of rollers engageable with said inner surface, to rotate the driven member and to subsequently roll freely thereon, a driving motor, means responsive to rotation of said motor to transmit driving torque to said driven member, by way of said rollers, said means comprising a motor-driven member, and means carried by said motor-driven member for yielding engagement with the said rollers, to exert upon said rollers a radially directed pressure suiflcient to rotate-said -driven member, said means comprising pivoted levers having high"-points from which said rollers may ride ofi in either direction, according to the torque conditions encountered.
' SIDNEY H. WEBSTER.
US403214A 1941-07-19 1941-07-19 Engine starting mechanism Expired - Lifetime US2322608A (en)

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2583829A (en) * 1949-06-03 1952-01-29 Bendix Aviat Corp Wrap spring starter
US2592436A (en) * 1952-04-08 True negative total printing
US2625047A (en) * 1949-06-25 1953-01-13 Garrett Corp Pneumatic engine starter device
US2640359A (en) * 1949-09-26 1953-06-02 Bendix Aviat Corp High-speed starter
US2650060A (en) * 1948-04-27 1953-08-25 Edward A Stalker Gas turbine adapted as a starter
US2754947A (en) * 1951-02-23 1956-07-17 Chicago Nipple Mfg Company Releasable one-way clutch
US2843101A (en) * 1955-01-20 1958-07-15 James H Hubert Adapter type one-way clutch drive means
US2909166A (en) * 1955-10-19 1959-10-20 Garrett Corp Air turbine starter
US3361237A (en) * 1965-03-29 1968-01-02 William K. Mathews Overrunning clutch
US20120252585A1 (en) * 2009-11-06 2012-10-04 Hilti Aktiengesellschaft Torque coupling

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2592436A (en) * 1952-04-08 True negative total printing
US2650060A (en) * 1948-04-27 1953-08-25 Edward A Stalker Gas turbine adapted as a starter
US2583829A (en) * 1949-06-03 1952-01-29 Bendix Aviat Corp Wrap spring starter
US2625047A (en) * 1949-06-25 1953-01-13 Garrett Corp Pneumatic engine starter device
US2640359A (en) * 1949-09-26 1953-06-02 Bendix Aviat Corp High-speed starter
US2754947A (en) * 1951-02-23 1956-07-17 Chicago Nipple Mfg Company Releasable one-way clutch
US2843101A (en) * 1955-01-20 1958-07-15 James H Hubert Adapter type one-way clutch drive means
US2909166A (en) * 1955-10-19 1959-10-20 Garrett Corp Air turbine starter
US3361237A (en) * 1965-03-29 1968-01-02 William K. Mathews Overrunning clutch
US20120252585A1 (en) * 2009-11-06 2012-10-04 Hilti Aktiengesellschaft Torque coupling
US9879734B2 (en) * 2009-11-06 2018-01-30 Hilti Aktiengesellschaft Torque coupling

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