GB403776A - Starting mechanism for internal combustion engines - Google Patents

Starting mechanism for internal combustion engines

Info

Publication number
GB403776A
GB403776A GB25549/32A GB2554932A GB403776A GB 403776 A GB403776 A GB 403776A GB 25549/32 A GB25549/32 A GB 25549/32A GB 2554932 A GB2554932 A GB 2554932A GB 403776 A GB403776 A GB 403776A
Authority
GB
United Kingdom
Prior art keywords
clutch
engine
shaft
pinion
supercharger
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
Application number
GB25549/32A
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.)
Bendix Aviation Corp
Original Assignee
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
Application filed by Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB403776A publication Critical patent/GB403776A/en
Expired legal-status Critical Current

Links

Classifications

    • 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

Abstract

403,776. Turning-gear. BENDIX AVIATION CORPORATION, 105, West Adams Street, Chicago, U.S.A. Sept. 14, 1932, No. 25549. Convention date, Sept. 15, 1931. [Class 7 (v).] In a starting mechanism for internal-combustion engines which drive a supercharger or other auxiliary unit when operating under their own power, a coupling between the engine shaft and the auxiliary unit is automatically rendered inoperative during the cranking of the engine shaft from the starter. The coupling preferably consists of an overrunning clutch mechanism which couples the starter to the engine shaft during the starting operation and couples the engine to the auxiliary unit during normal running. As shown, the engine starter comprises an electric motor 13 mounted with its axis at right angles to that of the rotary supercharger 4 and driving through bevel gears 16, 17 a shaft 19, on a threaded portion 27 of which a clutch member 26 moves axially into driving engagement with a flywheel 32. The shaft 36 of the flywheel has a threaded portion 62 on which a clutch member 60 moves axially into engagement with a clutch member 61 on a pinion 43 connected to the shaft 6 of the supercharger 4 by a roller clutch 45. The pinion 43 is normally driven from the engine through a clutch 2, gears 106, 102 and a shaft 71 carrying a gear 67 meshing with the pinion 43. The clutch rollers 45, Fig. 2, co-operate with cam surfaces 44 on the inner surface of the pinion, and are guided by a cage 47, Figs. 2 and 3, one end of which carries conical members 49 registering with openings 50 in a control ring 51 rigidly retained in the pinion. The cage 47 is normally urged to the left by a spring 53, allowing sufficient play between the members 49, 51 to allow the rollers 45 to be carried into wedging relation with the cam surfaces 44 and the supercharger to be driven from the engine through the pinion 43. When the starter is in operation, the clutch member 60 moves axially into driving engagement with the pinion 43, while the hub 59 of the member 60 pushes the cage 47 to the right, bringing the conical members 49 into full engagement with the openings 50 of the ring 51. Thus the clutch rollers 45 are held out of engagement with the cam surfaces 44 and the supercharger is not driven, while the engine starter drives the engine through the clutch 60, 61, gears 43, 67, &c. The gear 67 is connected to the shaft 71 by a centrifugally controlled friction clutch comprising a disc 70 on the shaft 71 and a disc member 89, frictional engagement being obtained by means of weighted levers 94 preferably provided with springs 97 and acting through pins 96 on the disc 89. The levers are normally held in clutch-releasing position by a thrust bearing 98 moved to the right in Fig. 1 by a lever 101 and sleeve 99. At starting, when the motor 13 and flywheel 32 have been set in rotation, the thrust bearing 98 is moved to the left to allow the friction clutch to engage and the engine to be driven through the gear train 43,67,102,106.
GB25549/32A 1931-09-15 1932-09-14 Starting mechanism for internal combustion engines Expired GB403776A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US403776XA 1931-09-15 1931-09-15

Publications (1)

Publication Number Publication Date
GB403776A true GB403776A (en) 1934-01-04

Family

ID=21910660

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25549/32A Expired GB403776A (en) 1931-09-15 1932-09-14 Starting mechanism for internal combustion engines

Country Status (1)

Country Link
GB (1) GB403776A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112983709A (en) * 2019-12-18 2021-06-18 重庆隆鑫通航发动机制造有限公司 Centrifugal overload protection starting drive and engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112983709A (en) * 2019-12-18 2021-06-18 重庆隆鑫通航发动机制造有限公司 Centrifugal overload protection starting drive and engine

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