GB643727A - Engine starting means - Google Patents

Engine starting means

Info

Publication number
GB643727A
GB643727A GB20652/47A GB2065247A GB643727A GB 643727 A GB643727 A GB 643727A GB 20652/47 A GB20652/47 A GB 20652/47A GB 2065247 A GB2065247 A GB 2065247A GB 643727 A GB643727 A GB 643727A
Authority
GB
United Kingdom
Prior art keywords
gear
clutch
shaft
motor
jaw
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
GB20652/47A
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 GB643727A publication Critical patent/GB643727A/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
    • F02N15/00Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00 - F02N13/00

Abstract

643,727. Turning gear. BENDIX AVIATION CORPORATION. July 30, 1947, No. 20652. Convention date, Aug. 28, 1946. [Class 7 (v)] In an engine starter comprising a starter clutch-jaw member 16, a motor 36 having a shaft 38 for rotating the member 16 and a reduction gear train for transmitting the rotation of the shaft to the member 16 at a reduced speed, a rotative gear member 32 meshes with a gear 28 at the higher speed end of the train and is rotatable by driving-element receiving means 52 when the motor is de-energized and disconhected therefrom when the motor is energized, the means 52 being located at a position spaced from member 16 and operatively connected with the gear member 32 through a flexible shaft 54. A rotatable barrel 2, supports planet gears 26 operating between a stationary orbitalgear 24 and a sun gear 30, the latter being fixed to the internal gear 28 the teeth of which are engaged by a pinion 34 that is part of gear 32. The gear 32 is in mesh with another pinion 40 on the shaft 38 which shaft has attached thereto a flywheel 42. The barrel 20 is connected by a multi-plate, friction clutch 22 to an axially-stationary nut 12 threaded to a screwshaft 14 to which is splined the jaw-member 16, whilst a spring 18 is interposed between the shaft 14 and the jaw-member 16, the spring surrounding the front end of a mesh rod 122 and a shoulder on the rod being in engagement with the rear of the screwshaft. A hollow pinion 48 is in permanent engagement with the gear 32 and an overrunning free-wheel clutch 50 is located inside the pinion 48, the clutch being connected by the flexible shaft 54 to the receiving means 52. The hollow pinion and clutch 50 could be replaced by a screw-and-nut mechanism such as that described above for operating the jaw-member 16. The element 52 is connected to a step-up gear-train 172 which is either operated manually or by a portable electric motor (not shown). The mesh rod is either moved manually by a ring 178, cable 182 and lever 128 or by a solenoid (not shown), whilst another ring 186 and cable 188 is used to lift the motor brushes 102 when the alternative drive through clutch 50 is to be used. A ball 126 is provided on the cable 188 to lock the brushes in the lifted position. When the motor 36 is operated and the flywheel 42 is brought up to speed, the ring 178 is pulled to move the mesh rod 122 axially until the shoulder of the latter pushes against the screwshaft 14 and causes it to turn in the nut 12 and so through the spring 18 to move the member 16 into engagement with the engine jaw-clutch 46 whereupon the shoulders 116 and 118 on the shaft and nut respectively abut so that member 16 is rotated and cranks the engine. To effect starting independently of the motor 36 the ring 186 is pulled to lift the brushes, and the gear train 172 is operated to rotate the flywheel through clutch 50. Oil seals 130 and 126' are provided, respectively, at the rear of the screwshaft and the member 16 whilst the latter has a seal 112 around its periphery.
GB20652/47A 1946-08-28 1947-07-30 Engine starting means Expired GB643727A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US693469A US2508833A (en) 1946-08-28 1946-08-28 Engine starting means

Publications (1)

Publication Number Publication Date
GB643727A true GB643727A (en) 1950-09-27

Family

ID=24784778

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20652/47A Expired GB643727A (en) 1946-08-28 1947-07-30 Engine starting means

Country Status (2)

Country Link
US (1) US2508833A (en)
GB (1) GB643727A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0649898Y2 (en) * 1987-11-11 1994-12-14 株式会社共立 Internal combustion engine starter
JPH0649899Y2 (en) * 1987-11-25 1994-12-14 株式会社共立 Internal combustion engine for portable work machine with automatic starter

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1424987A (en) * 1920-11-05 1922-08-08 Clark Albert Hawkins Clutch
US2030882A (en) * 1929-01-08 1936-02-18 Eclipse Machine Co Engine starting apparatus
US2095236A (en) * 1934-11-23 1937-10-12 Eclipse Aviat Corp Engine starting mechanism
US2261402A (en) * 1939-05-05 1941-11-04 Bendix Aviat Corp Engine starting mechanism
US2349867A (en) * 1942-07-07 1944-05-30 Jack & Heintz Inc Starter
US2346303A (en) * 1942-09-24 1944-04-11 Jack & Heiatz Inc Engine starting system

Also Published As

Publication number Publication date
US2508833A (en) 1950-05-23

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