US2665588A - Starter jaw advancing mechanism - Google Patents

Starter jaw advancing mechanism Download PDF

Info

Publication number
US2665588A
US2665588A US273021A US27302152A US2665588A US 2665588 A US2665588 A US 2665588A US 273021 A US273021 A US 273021A US 27302152 A US27302152 A US 27302152A US 2665588 A US2665588 A US 2665588A
Authority
US
United States
Prior art keywords
jaw
starter
shaft
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 - Lifetime
Application number
US273021A
Inventor
Gilbert Samuel
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
Priority to US273021A priority Critical patent/US2665588A/en
Application granted granted Critical
Publication of US2665588A publication Critical patent/US2665588A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F02N15/021Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging starter jaws
    • 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
    • Y10T74/139Cam operated

Definitions

  • the present invention relates to engine starters and particularly to starter jaw advancing mechanism.
  • I In'engine starters it is desirable to have some method of automatically advancing the starter jaw into mesh with the engine jaw.
  • One method which has been used comprises a nut, driven by a clutch and reduction gearing, which engages a screw shaft drivably connected to the starter jaw.
  • a rotational restraint is required to hold the jaw to cause the screw shaft to advance the nut thereby to move the starter jaw axially to the engaged position.
  • One method of providing rotational restrain is a friction ring. The friction ring results in a loss of efficiency and a decrease'of effectiveness of the jaw advance mechanism as the friction reduces due to wear in service.
  • nut and screw shaft are located after th reduction gearing which requires that they be large enough to have sufiicient strength for handling the high torque required for starting.
  • the purpose of the screw shaft is to advance the jaw which requires a relatively small force. Hence, it could be'a smaller mechanism if located in a more-favorable position.
  • rotational restrain is provided for the reduction'gearing. Inasmuch as the restrain is in the low torque portion-of the gearing, less restraint is required than if located on the starter jaw'where the output torque is high.
  • An object of the present invention is to provide an improved starter.
  • Another object of the invention is to provide improved jaw meshing mechanism.
  • Another object of the invention is to provide novel positive jawactuating mechanism.
  • Another object is to provide a jaw-advancing mechanism in which'fewer, smaller-and-simpler parts are required.
  • Another object of the'invention is to provide novel rotational restraining means- *2
  • Another object of the invention i to provide a relatively low cost engine starter.
  • Figure 1 of the drawing is a partial section view of an engine starter embodying one form of the'invention. I 1
  • Figure 2 is an enlarged view of the'rest'raining means of Figure l. i
  • the device therein shown comprises a starter assembly including, in general, a motor I having a driving shaft 2 rotatably supported by a'bearing 3 mounted in end wall 4' of motor housing 5;
  • the shaft 2' has a counterbore portion 6 adapted to receive an "enlarged portion 1 of a shaft 8.
  • a helical cam' 9 is formed in the enlarged portion 1 of'the shaft 8.
  • a pin l secured to the driving shaft 2 ex-. tends into the helical cam 9;
  • the shaft'8 has a pinion gear H integral therewith.
  • the gear ll meshes with'planetary ear 12."
  • the gear I2 is carried by a shaft 13 mounted. in planetary cage 14.
  • the shaft I3 is secured in the cage [4 by a pin l or in any other suitable manner.
  • a wall It of gear housing H has a circumferential flange it for positioning the cage 14';
  • a bearing member I9 may be positioned be-. tween the cage is and the flange 18.
  • the gear 12 is adapted to mesh with a ring gear secured against rotation to the housing H in any'suitabl'e manner. 1 f
  • Integral with th gear l2 is'a gear 2
  • the barrel 23 is rotatably mounted in the housing IT.
  • the inner surface of the housing I1 and outer surface of the barrel 23 are finished to provide bearing surfaces. It is understood, however, that the barrel 23 could be mounted in the housing" ill by other bearing means.
  • the barrel 23 is connected to starter jaw 24 by a clutch pack 25.
  • the clutch pack 25 has one set of discs 26 splined to the barrel 23 and. another set of discs 21 slidably splined to the 'jaw 24. Pressure isapplied to the clutch pack .25 by means of a spring 28 which may be a belleyille washer.
  • a backing plate 29 is secured in position by a snap ring 3! placed-in a groove 3! in the barrel 23.
  • a bearing support 32 is held against a shoulder 33 in the barrel 23 by the reaction of the spring 28.
  • the bearing support 32 has a cylindrical portion 34 extending into a counterbore portion 35 of jaw 24.
  • a bearing 36 is piloted by and is free to move axially in the cylindrical portion 34.
  • a shank portion of shaft 8 is secured to the bearing 35 by a shoulder 31 on the shaft 8 and a lock ring 38.
  • a mesh rod 139 extends axially of the counterbore portion 35 and extends through the jaw 24.
  • a nut 40 retains the jaw 24 in operative relationship with the mesh rod 39.
  • the other end of the rod 39 terminates in a flanged portion 7 4! which pilots in the cylindrical portion 34.
  • a spring 42 positioned between the flange 4 and the jaw 24 urges the jaw 24 into” engagement with an engine jaw (not shown) upon being com pressed by movement of the mesh rod 39.
  • a spring 43 positioned between the flange 4! and a radially extending flange 44 on tliecylindrical portion 35 serves to return the jaw 24 to a retracted position.
  • the housings 5 and i! are secured together by bolts 45.
  • the housing I! has an outward extending flange 46 adapted to be secured to an engine housing 41 in a conventional manner, for example, by studs 48.
  • An end cover 49 is secured to the housing I! by the bolts 45.
  • the present invention providesnovel means for restraining rotation of the starter jaw 24 until it has been cammed into mesh by the action of the pin Ill in the slot 9.
  • a spring washer 50 is positioned on the shaft I3 between a brass washer 5i and a head 52 of the shaft l3.
  • a steel washer 53 is positioned between the washer 5i and the gear i2.
  • Corresponding brass and steel washers 54 and 55 are positioned on the shaft I3 between the gear 2
  • An engine starter comprising driving means, a pinion shaft, means including a cam connection for connecting said shaft for rotation with and axial movement relative to said driving means, a rotatable barrel member; reduction gearing interconnecting said barrel member and said pinion shaft, a starter 'jaw member, a splined clutch pack for connecting said starter jaw for rotation with and axial movement relative to said barrel member, means responsive to axial movementof said shaft for urging said starter jaw to an exte'ned position; and means including a spring washer for restraining said reduction gearing from rotation to cause said axial movement.
  • driving means having a driving member, a pinion shaft having a pinion gear integral therewith, earn means for connecting said pinion gear integra l therewith, cam means for connecting said pinion shaft for rotation with and axial move ment relative to said driving member, said cam means being responsive to initial rotation of said driving means to cause said axial movement, a rotatable barrel membenreduction gearing conmeeting said pinion gear and said barrel member, a starter jaw member, a spring biased clutch pack connecting said starter jaw to said barrel memher for rotation with and axial movement relative thereto, yieldable inans responsive to axial movement of said pinion shaft for urging said starter jaw to an engine engaging position, and.
  • a driving shaft for use in an engine starter, the combina tion: of a driving shaft, an axially movable pinion shaft, a pin and cam slot connection between said shafts, said connection being adapted to impart axial movement to said pinion shaft to position said pin and slotfor a positive driving connection between said shafts, a starter jaw member, means responsive to said axial movement for moving said jaw member axiallyto' an engine engaging position. and means for yieldably restraining said pinion shaft to cause said axial movement.

Landscapes

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

Description

Jan. 12, 1954 s, GlLBERT 2,665,588
STARTER JAW ADVANCING MECHANISM Filed Feb. 23, 1952 INVENTOR.
SAMUEL GILBERT BY Patented Jan. 12, 1954 STARTER JAW ADVANCING MECHANISM Samuel Gilbert, Cedar Grove, N. J., *assignor to Bendix Aviation Corporation, Teterboro, N. J., a corporation of Delaware 1 V 7 Application February 23, 1952, Serial No. 273,021
4 Claims.
. 1 e The present invention relates to engine starters and particularly to starter jaw advancing mechanism. I In'engine starters it is desirable to have some method of automatically advancing the starter jaw into mesh with the engine jaw. One method which has been used comprises a nut, driven by a clutch and reduction gearing, which engages a screw shaft drivably connected to the starter jaw. A rotational restraint is required to hold the jaw to cause the screw shaft to advance the nut thereby to move the starter jaw axially to the engaged position. One method of providing rotational restrain is a friction ring. The friction ring results in a loss of efficiency and a decrease'of effectiveness of the jaw advance mechanism as the friction reduces due to wear in service. Another disadvantage is that the nut and screw shaft are located after th reduction gearing which requires that they be large enough to have sufiicient strength for handling the high torque required for starting. The purpose of the screw shaft is to advance the jaw which requires a relatively small force. Hence, it could be'a smaller mechanism if located in a more-favorable position.
In copending application Serial No. 223.305, filed April 27, 1951, by Henry Troeger, the starter jaw is meshed by a cam action ahead of the reduction gearing. High starting torques cannot be applied until the jaw teeth are fully meshed. Also, the advancement of the starter jaw is rapid, thus preventing high impact loads due to high armature speeds as are obtained in other methods. It has been found, however, that to insure the advancement of the starter jaw into mesh with the engin jaw some means of rotational restraint is necessary. e I
In the present invention, rotational restrain is provided for the reduction'gearing. Inasmuch as the restrain is in the low torque portion-of the gearing, less restraint is required than if located on the starter jaw'where the output torque is high.
An object of the present invention is to provide an improved starter.
Another object of the invention is to provide improved jaw meshing mechanism.
Another object of the invention is to provide novel positive jawactuating mechanism.
' Another object is to provide a jaw-advancing mechanism in which'fewer, smaller-and-simpler parts are required.
' Another object of the'invention is to provide novel rotational restraining means- *2 Another object of the invention i to provide a relatively low cost engine starter.
'The above and other objects and features of th invention will appear more fully hereinafter from a consideration of the following description taken in connection with the accompanying drawings wherein-one embodiment of theinv'ention is illustrated by way of example.
In the drawing: I 3
Figure 1 of the drawing is a partial section view of an engine starter embodying one form of the'invention. I 1
Figure 2 is an enlarged view of the'rest'raining means of Figure l. i
Referring to the drawing, the device therein shown comprises a starter assembly including, in general, a motor I having a driving shaft 2 rotatably supported by a'bearing 3 mounted in end wall 4' of motor housing 5; The shaft 2'has a counterbore portion 6 adapted to receive an "enlarged portion 1 of a shaft 8. A helical cam' 9 is formed in the enlarged portion 1 of'the shaft 8. A pin l secured to the driving shaft 2 ex-. tends into the helical cam 9;
The shaft'8 has a pinion gear H integral therewith. The gear ll meshes with'planetary ear 12." The gear I2 is carried by a shaft 13 mounted. in planetary cage 14. The shaft I3 is secured in the cage [4 by a pin l or in any other suitable manner. A wall It of gear housing H has a circumferential flange it for positioning the cage 14'; A bearing member I9 may be positioned be-. tween the cage is and the flange 18. The gear 12 is adapted to mesh with a ring gear secured against rotation to the housing H in any'suitabl'e manner. 1 f
Integral with th gear l2 is'a gear 2| adapted to mesh with splines 22 of barrel 23'. The barrel 23 is rotatably mounted in the housing IT. The inner surface of the housing I1 and outer surface of the barrel 23 are finished to provide bearing surfaces. It is understood, however, that the barrel 23 could be mounted in the housing" ill by other bearing means.
The barrel 23 is connected to starter jaw 24 by a clutch pack 25. The clutch pack 25 has one set of discs 26 splined to the barrel 23 and. another set of discs 21 slidably splined to the 'jaw 24. Pressure isapplied to the clutch pack .25 by means of a spring 28 which may be a belleyille washer. A backing plate 29 is secured in position by a snap ring 3!! placed-in a groove 3! in the barrel 23. l
A bearing support 32 is held against a shoulder 33 in the barrel 23 by the reaction of the spring 28. The bearing support 32 has a cylindrical portion 34 extending into a counterbore portion 35 of jaw 24. A bearing 36 is piloted by and is free to move axially in the cylindrical portion 34. A shank portion of shaft 8 is secured to the bearing 35 by a shoulder 31 on the shaft 8 and a lock ring 38.
A mesh rod 139 extends axially of the counterbore portion 35 and extends through the jaw 24. A nut 40 retains the jaw 24 in operative relationship with the mesh rod 39. The other end of the rod 39 terminates in a flanged portion 7 4! which pilots in the cylindrical portion 34. A spring 42 positioned between the flange 4 and the jaw 24 urges the jaw 24 into" engagement with an engine jaw (not shown) upon being com pressed by movement of the mesh rod 39. V
A spring 43 positioned between the flange 4! and a radially extending flange 44 on tliecylindrical portion 35 serves to return the jaw 24 to a retracted position. v
The housings 5 and i! are secured together by bolts 45. The housing I! has an outward extending flange 46 adapted to be secured to an engine housing 41 in a conventional manner, for example, by studs 48. An end cover 49 is secured to the housing I! by the bolts 45.
The aforenoted arrangement is described and claimed in copending application Serial No. 223.305.
The present invention providesnovel means for restraining rotation of the starter jaw 24 until it has been cammed into mesh by the action of the pin Ill in the slot 9. A spring washer 50 is positioned on the shaft I3 between a brass washer 5i and a head 52 of the shaft l3. A steel washer 53 is positioned between the washer 5i and the gear i2. Corresponding brass and steel washers 54 and 55 are positioned on the shaft I3 between the gear 2| and the pin [5;
In" operation, upon the motor I being energized, the acceleration of the armature shaft 2 will cause a torque to be applied to the shaft 8 through the pin ID. The spring Washer 50 exerts a force against the washers 5!, 53, gears l2--2l and washers 54 and 55 to restrain the gears 12-21 from rotation thereby causing the pin to exert an axial thrust on the cam surface 9. This axial thrust due to the lead of the cam surface 9 will cause the shaft 8 to move axially and thereby move the bearing 36 axially in the bearing support 32. Movement of the bearing 36 causes a corresponding movement of the mesh rod 39' which compresses the spring 42. The spring 42 upon being compressed urges the starter jaw 24 into engagement with the engine jaw (not shown).
Upon the jaws meshing, the restraining force of the washers will be overcome and the brass and steel washers will slip respective to each other to permit rotation of the gee-rs l22l.
If the starter and engine jaw teeth mesh at partial depth, no appreciable torque can be applied until thecani 9 has fully advanced onthe pin ID. This insures full engagement of starter and engine jaw teeth. Upon cranking an en gins, should the engine jaw accelerate and push thestarter jaw out of mesh; the release of the torque load from the motor will permit the armature to accelerate thus r-engaging the jaws as spring 43 exerts a smaller retraction force on the jaw than is available for jaw advancement when starting, but is suihcient to insure retraction of the jaw regardless of the position in which the starter is mounted.
Another feature of the starter is that the barrel 2 3 is connected to the jaw 24 by the clutch pack 25 thus eliminating the usual splined nut and screw shaft. Also, the gear teeth and spline teeth'of the barrel 23 are the same which simplifies the manufacturing thereof. H 7
Although only one embodiment of the invention has been illustrated and described, various changes in the form and relative arrangements of the parts may be made to suit requirements.
What is claimed is:
1; An engine starter comprising driving means, a pinion shaft, means including a cam connection for connecting said shaft for rotation with and axial movement relative to said driving means, a rotatable barrel member; reduction gearing interconnecting said barrel member and said pinion shaft, a starter 'jaw member, a splined clutch pack for connecting said starter jaw for rotation with and axial movement relative to said barrel member, means responsive to axial movementof said shaft for urging said starter jaw to an exte'ned position; and means including a spring washer for restraining said reduction gearing from rotation to cause said axial movement.
2. In an engine starter, the combination of driving means having a driving member, a pinion shaft having a pinion gear integral therewith, earn means for connecting said pinion gear integra l therewith, cam means for connecting said pinion shaft for rotation with and axial move ment relative to said driving member, said cam means being responsive to initial rotation of said driving means to cause said axial movement, a rotatable barrel membenreduction gearing conmeeting said pinion gear and said barrel member, a starter jaw member, a spring biased clutch pack connecting said starter jaw to said barrel memher for rotation with and axial movement relative thereto, yieldable inans responsive to axial movement of said pinion shaft for urging said starter jaw to an engine engaging position, and.
means for retarding rotation of said reduction gearing to cause said axial movement.
3. For use in an engine starter, the combina tion: of a driving shaft, an axially movable pinion shaft, a pin and cam slot connection between said shafts, said connection being adapted to impart axial movement to said pinion shaft to position said pin and slotfor a positive driving connection between said shafts, a starter jaw member, means responsive to said axial movement for moving said jaw member axiallyto' an engine engaging position. and means for yieldably restraining said pinion shaft to cause said axial movement.
4. In an' engine starter, the combination of driving means, a rotatable axially movable pinion shaft having a spiral cam groove formed in one end thereof, apin member secured to said driving means and adapted for register in said cam groove, a rotatable barrel member, reduction gearing connecting said pinion shaft and said barrel member, a starter jaw member, a spring biased clutch pack for connecting said jaw member for rotation with and splined for axial movement relative to said barrel member, a mesh rod mem ber adapted for axial movement by said pinion shaft, spring means interposed between said mesh rod member and said jaw member for urging said jaw member into an engaging position upon actuation of said mesh rod member, said pin member coacting with said cam groove to move said pinion shaft axially and to provide a driving connection 6 between said driving means and said shaft, and yieldable friction means for restraining rotation of said reduction gearing to cause said pinion shaft to be moved axially.
SAMUEL GILBERT.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,207,652 Berges July 9, 1940 2,280,432 Hodges Apr. 21, 1942
US273021A 1952-02-23 1952-02-23 Starter jaw advancing mechanism Expired - Lifetime US2665588A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US273021A US2665588A (en) 1952-02-23 1952-02-23 Starter jaw advancing mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US273021A US2665588A (en) 1952-02-23 1952-02-23 Starter jaw advancing mechanism

Publications (1)

Publication Number Publication Date
US2665588A true US2665588A (en) 1954-01-12

Family

ID=23042211

Family Applications (1)

Application Number Title Priority Date Filing Date
US273021A Expired - Lifetime US2665588A (en) 1952-02-23 1952-02-23 Starter jaw advancing mechanism

Country Status (1)

Country Link
US (1) US2665588A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2728234A (en) * 1954-09-30 1955-12-27 Bendix Aviat Corp Engine starter
FR2554304A1 (en) * 1983-10-27 1985-05-03 Paris & Du Rhone Device for mounting a cap and its application to bearing caps of electrical rotating machines

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2207652A (en) * 1939-06-02 1940-07-09 Bendix Aviat Corp Engine starting mechanism
US2280432A (en) * 1941-07-17 1942-04-21 H P Lester Starter mechanism

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2207652A (en) * 1939-06-02 1940-07-09 Bendix Aviat Corp Engine starting mechanism
US2280432A (en) * 1941-07-17 1942-04-21 H P Lester Starter mechanism

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2728234A (en) * 1954-09-30 1955-12-27 Bendix Aviat Corp Engine starter
FR2554304A1 (en) * 1983-10-27 1985-05-03 Paris & Du Rhone Device for mounting a cap and its application to bearing caps of electrical rotating machines

Similar Documents

Publication Publication Date Title
US2600762A (en) Starter generator
GB1145950A (en) Coupling mechanism
US2665588A (en) Starter jaw advancing mechanism
US2787910A (en) Engine starter drive
US2602335A (en) Engine starter gearing
US2553202A (en) Starter-generator gearing
US2815669A (en) Engine starter gearing
US2841988A (en) Starter gearing for internal combustion engines
US2235076A (en) Starter gearing
US2061161A (en) Engine starter
US2776571A (en) Engine starter clutch
US2571231A (en) Starter jaw actuating device
US2665586A (en) Engine starter apparatus
US2084813A (en) Engine starting mechanism
US2394690A (en) Engine starter gearing
US2593167A (en) Engine starter gearing
US2665587A (en) Starter for internal-combustion engines
US2752023A (en) Jet engine starter clutch with teeth synchronizing means
US2934656A (en) Electric engine-starting motors
US2683990A (en) Engine starter
US2775894A (en) Pneumatic engine starter
US2625826A (en) Automatic premeshing mechanism
US2939324A (en) Engine starter mechanism
USRE23497E (en) Starter jaw actuxtmeimexhanism i
US2345791A (en) Engine starter gearing