GB673592A - Improvements in or relating to engine-starter drives - Google Patents

Improvements in or relating to engine-starter drives

Info

Publication number
GB673592A
GB673592A GB18818/50A GB1881850A GB673592A GB 673592 A GB673592 A GB 673592A GB 18818/50 A GB18818/50 A GB 18818/50A GB 1881850 A GB1881850 A GB 1881850A GB 673592 A GB673592 A GB 673592A
Authority
GB
United Kingdom
Prior art keywords
spring
pinion
sleeve
barrel
engine
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
GB18818/50A
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 GB673592A publication Critical patent/GB673592A/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
    • F02N15/02Gearing between starting-engines and started engines; Engagement or disengagement thereof
    • F02N15/04Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears
    • F02N15/06Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging toothed gears the toothed gears being moved by axial displacement
    • F02N15/062Starter drives
    • F02N15/063Starter drives with resilient shock absorbers

Landscapes

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

Abstract

673,592. Turning-gear. BENDIX AVIATION CORPORATION. July 27,1950 [Aug. 8, 1949], No. 18818/50. Class 7(v) In 'an engine starter drive comprising a power shaft 1, a sleeve 4 fixedly mounted thereon having spline grooves at one end and a stop shoulder 6 at the other, a screwshaft 11 having clutch teeth 12 at one end slidably journalled on the intermediate portion of the sleeve 4, a clutch member 9 slidably but non-rotatably mounted on the splined portion of the sleeve 4, an abutment 14 on the sleeve 4 limiting movement of the member 9 away from the sleeve, a spring 13 urging member 9 into driving engagement with the clutch teeth 12 and normally holding the screw-shaft 11 against the stop shoulder 6, a control nut 18 threaded on the screw-shaft 11, a barrel member 21 rigidly mounted at one end on the control nut, a pinion 16 slidably journalled on' the power shaft for longitudinal movement into and out of mesh with a gear 17 on the engine to be started and having a driven coupling member 28 fixed thereon, there is provided a driving coupling member 24 non-rotatably mounted in the other end of the barrel member 21 and yielding means, such as spring discs 31, on the pinion 16 urging the coupling members into driving engagement. The pinion 16 and barrel 21 are normally located in extended relationship by a mesh enforcing spring 34 positioned between a stop in the interior of the barrel and one of the spring discs 31; an anti-drift spring 37 is located between a thimble 38 on the stop shoulder 6 and the nut 18. In operation, the rotation of the power shaft 1 is transmitted through sleeve 4, clutch member 12 to the screw-shaft 11 so that the nut 18 and the associated parts are traversed to the right to mesh the pinion 16 with the engine gear 17 whereupon the nut 18 abuts the shoulder 6 so that the screw-shaft 11 is forced leftward against the compression of spring 13 thereby ensuring firm engagement of the overrunning clutch 9, 12, the clutch member 9 finally contacting the abutment 14; torque is now transmitted,through the coupling members 24, 28 to crank the engine; if, however, the required torque is or should become excessive the coupling members will be forced apart against the bias of the spring discs 31 until the overload ceases. Should tooth abutment occur, the axial movement of the pinion 16 is arrested but the barrel and nut continue to move by virtue of lugs 23 on coupling member 24 travelling in slots 22 in the barrel 21 so that the mesh enforcing spring 34 is compressed until the rotary component of the force transmitted through the screwshaft is sufficient to index the pinion and engine gear, whereupon the spring 34 ensures the initial meshing of the pinion and engine gear.
GB18818/50A 1949-08-08 1950-07-27 Improvements in or relating to engine-starter drives Expired GB673592A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US673592XA 1949-08-08 1949-08-08

Publications (1)

Publication Number Publication Date
GB673592A true GB673592A (en) 1952-06-11

Family

ID=22075481

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18818/50A Expired GB673592A (en) 1949-08-08 1950-07-27 Improvements in or relating to engine-starter drives

Country Status (1)

Country Link
GB (1) GB673592A (en)

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