GB341715A - Improvements in engine starting apparatus - Google Patents

Improvements in engine starting apparatus

Info

Publication number
GB341715A
GB341715A GB1965/30A GB196530A GB341715A GB 341715 A GB341715 A GB 341715A GB 1965/30 A GB1965/30 A GB 1965/30A GB 196530 A GB196530 A GB 196530A GB 341715 A GB341715 A GB 341715A
Authority
GB
United Kingdom
Prior art keywords
casing
sleeve
engaging
engine
spring
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
GB1965/30A
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.)
Eclipse Aviation Corp
Original Assignee
Eclipse 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 Eclipse Aviation Corp filed Critical Eclipse Aviation Corp
Publication of GB341715A publication Critical patent/GB341715A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N19/00—Starting aids for combustion engines, not otherwise provided for
    • F02N19/001—Arrangements thereof
    • E—FIXED CONSTRUCTIONS
    • E02—HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02D—FOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D29/00—Independent underground or underwater structures; Retaining walls
    • E02D29/063—Tunnels submerged into, or built in, open water
    • E02D29/077—Tunnels at least partially built beneath the water-bed characterised by being made by methods involving disturbance thereof all along the location line, e.g. by cut-and-cover or caisson methods

Abstract

341,715. Turning gear. ECLIPSE AVIATION CORPORATION, 545, North Arling- ton Avenue, East Orange, New Jersey, U.S.A. Jan. 20, 1930, No. 1965. Convention date, Jan. 30, 1929. [Class 7 (v).] In hand- or motor-operated starting- mechanism for aeroplane engines &c., a casing 10 is secured with rotary adjustment upon the engine casing 14 and is closed by a cover 16, lateral oblique extensions 20 on the casing and cover carrying a pinion 23 with inclined teeth engaging a wheel 36 on a barrel 34 mounted concentrically in the casing. The barrel is frictionally connected by a coupling 45, 46, adjustable between a screwed sleeve 49 and springs 47, to a sleeve 44 carrying lugs 51 for engaging the engine and normally retracted by a spring 58. A spring collar 52, Fig. 3, frictionally engages the sleeve 44 and has an inclined slot 53 engaging a screw 54 in the casing, so that when the pinion 23 is rotated in the forward direction, by the engagement of hand-crank or motor driving-means with its end 26, the sleeve 44 is projected to engage with the engine, returning automatically when the engine starts. Damage to the operator when backfiring occurs is prevented by the use of a spring- pressed non-rotatable ratchet ring 42 engaging a similar ring 40 on the side of the wheel 36, the coupling 45, 46 slipping during such action.
GB1965/30A 1929-01-30 1930-01-20 Improvements in engine starting apparatus Expired GB341715A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US341715XA 1929-01-30 1929-01-30

Publications (1)

Publication Number Publication Date
GB341715A true GB341715A (en) 1931-01-22

Family

ID=21874745

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1965/30A Expired GB341715A (en) 1929-01-30 1930-01-20 Improvements in engine starting apparatus

Country Status (2)

Country Link
FR (1) FR341715A (en)
GB (1) GB341715A (en)

Also Published As

Publication number Publication date
FR341715A (en) 1904-08-18

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