US2540208A - Friction holding and sealing means for direct cranking engine starters and the like - Google Patents
Friction holding and sealing means for direct cranking engine starters and the like Download PDFInfo
- Publication number
- US2540208A US2540208A US709271A US70927146A US2540208A US 2540208 A US2540208 A US 2540208A US 709271 A US709271 A US 709271A US 70927146 A US70927146 A US 70927146A US 2540208 A US2540208 A US 2540208A
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- Prior art keywords
- jaw
- nut
- starter
- axially
- shank
- Prior art date
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- Expired - Lifetime
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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
- F02N15/00—Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00 - F02N13/00
- F02N15/02—Gearing between starting-engines and started engines; Engagement or disengagement thereof
- F02N15/021—Gearing between starting-engines and started engines; Engagement or disengagement thereof the gearing including disengaging starter jaws
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/13—Machine starters
- Y10T74/131—Automatic
- Y10T74/134—Clutch connection
Definitions
- the invention hereof relates to friction holding and sealing means for direct cranking engine starters and the like, and particularly to means for frictionally holding the starter jaw for axial movement by a screw shaft and for sealing the starter about the jaw without axial rubbing on the seal.
- a ring seal subject to rotative rubbing only is considerably more efiective in excluding oil or any other fluid or liquid mixture, such as gasoline and oil or water, than a similiar seal which is also subject to axial rubbing.
- Another object is to entirely eliminate a sliding jaw seal, and to provide non-sealing friction holding means in combination with a seal which is subject to rotative rubbing only.
- Another object is to utilize a combined sliding seal and friction means in combination with a seal which is subj ect to rotative rubbing only.
- Another object is to provide a single ring having axially offset parts, one of which constitutes a combined friction means and sliding seal, and the other of which is subject to rotative rubbing only.
- Another object is to provide means of the above indicated character which are simple and durable in construction, economical to manufacture, and efiective in their operation.
- Figure 1 is a side view, partially in section and partially in elevation, of a portion of a directcranking starter structure embodying the invention in one form;
- Figure 2 is a view similar to a portion of Figure 1, of a modification of the invention.
- Figure 3 is a View similar to Figure 2 of a further modification of the invention.
- the device comprises a starter rotor member it having jaws l2 and adapted for axial movement, from its retracted position shown, to a position of engagement with an engine rotor jaw or load element M.
- the member I 0 is also adapted for rotative movement to rotate the element It to start the engine.
- a hollow shank portion it of the member ID is surrounded by a unit 18 of the invention, to be later more fully described, and has an inner spline connection 20 to a hollow screw shaft 22 having long-lead screw thread connection to a hollow axially stationary rotative nut 24.
- a member 32 held by a nut 34 in an opening in a central wall portion of the member I9, has a sealing ring 36, compressed by the nut between the members I9 and 32, and is provided with a flange 38 behind a flange 30 of the screw shaft 22.
- the spring 39 extends between the flange 38 and a backing ring 42 held to the shaft 22, as by a lock ring 44 in a groove of the shaft.
- a barrel 49 rotatively journaled in a housing portion 48, has a closed end wall 59, from which project trunnions 52 carrying planet gears 59 held in place, as by a ring 59, and engaging an orbital gear 58, fixed to the housing portion 48, and a sun gear 99 fixed to a shaft 62 journaled, as by needle bearings 85, in a tubular portion 66 of an annular plate-like member 98 positioned axially between the shaft 22 and the nut 24 at one side, and the wall 59, at the other side.
- the tubular portion 65 is closed at its left hand end, as by a wall 19.
- the shaft 62 further carries a portion 78 on which planet gears are also carried for engagement with the orbital gear 58 and another sun gear, and connected to other elements completing a gear train for reducing the speed of a driving or motor shaft, to the right of the structure shown, to the speed desired of the barrel 45.
- a feature of the invention resides in providing a cylindrical extension 89 of the nut 29 adapted to closely embrace the shank It of the member I9, and to extend axially to a position, short of the outer end of the shank in the retracted position of the member I9, leaving a length L of the shank between the jaws I2 and the adjacent end of the extension 89 constituting, in effect, a radially inward step from the radially outer surface of the extension 89 to the radially outer surface of the shank 18.
- An end housing portion 82 having a radial flange 84 secured to a radial flange 88 of the housing portion 48, as by screws 88, is mounted with the portion 48, as by studs 99 extending through the flanges 89 and 89 and into a portion 92 of an engine crank casing.
- the portion 82 constituting a portion of the unit 48, in this instance, has an axially extending annular flange 94 provided with radial apertures, around and about which flange, and through which apertures, a single ring body 99 of the unit I8 extends.
- the body 96 is constructed, as of neoprene or the like, molded to have flexible radially inner axially offset portions 99 and H39 substantially corresponding in inner diameter to the outer diameters of the shank I6 and the nut 29, respectively.
- Each of the portions 99 and 299 is of substantially C-section forming annular grooves opening to the left, as shown, with at least the portion 98 provided, in this instance, with a labyrinth i823 of annular inner surface grooves facilitating wiping of oil from the shank in its movement to the right from its extended position to its retracted position shown.
- the body 98 is locally vulcanized around and about the flange 94, and in the apertures of the flange, to strongly and rigidly anchor the body at these positions, and to leave the remainder of the body resilient, the body 96 thereby being positively interlocked with the housing portion 82 both axially and annularly and having effective yieldability for radially inward compression of the portions 98 and I99 against the shank I8 and the nut 24, respectively.
- a garter spring I94 in the groove of the portion 98, has its radially inward pressing force chosen not only to provide an elfective seal, but to effect sufiicient friction on the member 19 for holding the latter for axial movement by the screw shaft 22 through the intermediary of the spring 39, as hereinabove mentioned.
- a garter spring I96, in the groove of the portion I99 has its radially inward pressing force chosen to provide an effective seal against rotation of the nut 24 only.
- Both of the portions I99 and 98, before assembly, with the nut extension 89 and the member I9, respectively, are formed with the radially inner surfaces thereofconvergingly tapered from right to left, in which condition, with neither the extension 89 nor the member I9 in position, the grooves of the portions I89 and 99 are more open than they are as shown. Also, in this condition, the free edge tips, of the grooves may be bent counterclockwise, as viewed at the top of the ring in Figure 1, relative to the more solid parts of the body 98, to further open the grooves for the reception of the springs 186 and it.
- the groove walls in the portion I99 close to a position as shown around the spring I86 from which the latter, or parts thereof, cannot escape from the unit it.
- the body 96 has an annular surface 133 diverging to the left from a position near the spring I89, the shortest distance between which surface I98 and the free edge tip of the groove in the portion 98, is substantially less than the section diameter of the rim of the spring I99, in operative position as shown.
- the groove in the portion 98 Prior to assembly, the groove in the portion 98 is more open, for reasons above stated, and may be further opened to admit the spring I94 to the groove.
- the free edge tip of the groove automatically closes around the spring I94 to prevent parts of the spring, in case of breakage, from falling into the engine casing 92.
- the portion I99 is never subjected to any rubbing action except the rotative rubbing of the nut 24, during the first rotation of which nut the portion 98 is subjected to axial rubbing only.
- both portions 98and I99 are subjected to rotative rubbing, in which the rubbing on the portion I99 isslightly faster than that on the portion 98 by reason of the slightly large diameter of the nut 24 relative to the diameter of the member 19.
- FIGs 2 and 3 corresponding parts are designated by corresponding reference characters, in Figure 2 of which the construction and operation are similar to those of the device of Figure l, with the exceptions that the single body 99 is omitted and, in its place, are substituted the portions 98 and I99 as separate bodies.
- the portion or body I99 is vulcanized to the flange 99, extending axially oppositely to its direction of Figure 1, and the portion or body 98 is vulcanized to a similar flange extending, in the direction of the flange 94 of Figure 1, from a separate annular member 99 secured to the end housing portion 82.
- a direct-cranking engine starter compriing a housing, a screw shaft, a starter jaw member adapted for movement axially outwardly of the housing for engaging and rotative movement for rotating an engine jaw element and having a hollow shank portion providing for axial relative movement between the shaft and the jaw member, spring means axially compressible by and between said jaw member and said shaft, the combination of an axially stationary rotatably driven hollow nut having long-lead screw connection to said shaft thereabout and including a cylindrical extension adapted to closely axially and rotatively embrace said shank portion throughout the axial movement of the jaw member and in retracted position having its outer end short of the outer end of said shank portion leavin a length of the latter between the jaws of the jaw member and said outer nut extension end, a onepiece ring of rubber or the like around the axis of said shank having radially outer portions vulcanized to said housing and radially inner axially ofiset first and second portions of different
- a direct-cranking engine starter comprising a housing, a screw shaft, a starter jaw member adapted for movement axially outwardly of the housing for engaging and rotative movement for rotating an engine jaw element and having a, hollow shank portion providing for axial relative movement between the shaft and the jaw member, spring means axially compressible by and between said jaw member and said shaft, the combination of an axially stationary rotatably driven hollow nut having long-lead screw connection to said shaft thereabout and including a cylindrical extension adapted to closely axially and: rotatively embrace said shank portion throughout the axial movement of the jaw member and in retracted position having its outer end short'of the outer end of said shank portion leaving a length of the latter between the jaws of the jaw member and said outer nut extension end, a ring seal supported by said housing around said nut adjacent to said outer nut extension end, and a combined seal and friction ring supported by said housing and frictionally engaging and sealing said shank length in the retracted position of the jaw member and
- a direct-cranking engine starter comprising a housing, a screw shaft, a starter jaw member adapted for movement axially outward- -1y of the housing for engaging and rotative movement for rotating an engine jaw element and having a hollow shank portion providing for axial relative movement between the shaft and the jaw member, resilient means axially compressible by and between said jaw member and said shaft,
Description
Feb. 6, 1951 c s METSGER 2,540,208
FRICTION HOLDING AND SEALING MEANS FOR DIRECT CRANKING ENGINE STARTERS AND THE LIKE Filed Nov. 12, 1946 Z QafI 90 I2 7 38 so I iNVENTOR [H /"K55 5 M57555? ATTORNEY Patented Feb. 6, 1951 FRICTION HOLDING AND SEALING MEANS FOR DIRECT CRANKING ENGINE START- ERS AND THE LIKE Charles S. Metsger, Lodi, N. 3., assignor to Bendix Aviation Corporation, Teterboro, N. J a corporation of Delaware Application November 12, 1946, Serial No. 709,271
3 Claims. 1
The invention hereof relates to friction holding and sealing means for direct cranking engine starters and the like, and particularly to means for frictionally holding the starter jaw for axial movement by a screw shaft and for sealing the starter about the jaw without axial rubbing on the seal.
In a starter of the general type indicated, as formerly constructed, especially in aircraft practice, it has been usual to insert a smallportion of one end of the starter housing into the crank casing of the engine through an opening of the casing, and to have a clutch rotor or jaw member in an aperture of the starter housing adapted for axial movement between a position in which the jaw is mostly in the starter housing and spaced from an engine rotor or jaw element, and a position in which the starter jaw engages the engine In such arrangement, the jaw end of the starter is naturally subject to a strong tendency of the crank casing oil to enter the starter housing about the starter jaw, and this tendency has long presented a difficult and perplexing problem, resulting in many suggestions for its solution.
It is extremely undesirable to have any appreciable amount of such oil enter the starter housing, or to have any oil at all between the discs of a torque-limit ng friction disc pack 01' between friction elements of torque limiting means of any type.
In direct cranking starters, it has been exclusively the practice, irrespective of the many improvements heretofore suggested, so far as applicant is aware, to retain a ring seal between the starter housing and the jaw, which seal is subjected not only to rotative rubbing by the jaw, but to the axial sliding rubbing by the jaw as well.
A ring seal subject to rotative rubbing only, is considerably more efiective in excluding oil or any other fluid or liquid mixture, such as gasoline and oil or water, than a similiar seal which is also subject to axial rubbing.
Another objection to the axially sliding rotative seal directly on a jaw, is that it is subject to greater adverse effects from radial vibration of the jaw resulting from the necessary radial or rotative clearances of the jaw added to the cumulative radial clearances of other elements in the starter leading to the jaw.
Accordingly, among the objects of the present invention are to avoid all of the former objections to a starter jaw or like member, in connection with which a seal is subject to both rotative and axial rubbing, and to effect such results by novel effective means.
Another object, for certain applications, is to entirely eliminate a sliding jaw seal, and to provide non-sealing friction holding means in combination with a seal which is subject to rotative rubbing only.
Another object, for certain other applications, is to utilize a combined sliding seal and friction means in combination with a seal which is subj ect to rotative rubbing only.
Another object, for certain further applications, is to provide a single ring having axially offset parts, one of which constitutes a combined friction means and sliding seal, and the other of which is subject to rotative rubbing only.
Another object is to provide means of the above indicated character which are simple and durable in construction, economical to manufacture, and efiective in their operation.
These and other objects and features of the invention are pointed out in the following description in terms of the embodiment thereof which is shown in the accompanying drawing. It is to be understood, however, that the drawing is for the purpose of illustration only, and is not designed as a definition of the limits of the invention, reference being had to the appended claims for this purpose.
In the drawing:
Figure 1 is a side view, partially in section and partially in elevation, of a portion of a directcranking starter structure embodying the invention in one form;
Figure 2 is a view similar to a portion of Figure 1, of a modification of the invention; and
Figure 3 is a View similar to Figure 2 of a further modification of the invention.
In Figure 1, which shows only so much of a direct-cranking starter sufficient for an understanding of the invention, the device comprises a starter rotor member it having jaws l2 and adapted for axial movement, from its retracted position shown, to a position of engagement with an engine rotor jaw or load element M. The member I 0 is also adapted for rotative movement to rotate the element It to start the engine.
A hollow shank portion it of the member ID is surrounded by a unit 18 of the invention, to be later more fully described, and has an inner spline connection 20 to a hollow screw shaft 22 having long-lead screw thread connection to a hollow axially stationary rotative nut 24.
A member 32, held by a nut 34 in an opening in a central wall portion of the member I9, has a sealing ring 36, compressed by the nut between the members I9 and 32, and is provided with a flange 38 behind a flange 30 of the screw shaft 22. The spring 39 extends between the flange 38 and a backing ring 42 held to the shaft 22, as by a lock ring 44 in a groove of the shaft.
A barrel 49, rotatively journaled in a housing portion 48, has a closed end wall 59, from which project trunnions 52 carrying planet gears 59 held in place, as by a ring 59, and engaging an orbital gear 58, fixed to the housing portion 48, and a sun gear 99 fixed to a shaft 62 journaled, as by needle bearings 85, in a tubular portion 66 of an annular plate-like member 98 positioned axially between the shaft 22 and the nut 24 at one side, and the wall 59, at the other side. The tubular portion 65 is closed at its left hand end, as by a wall 19.
A torque limiting disc pack 12, having discs splined to the nut 24 and the barrel 95, respectively, is pressed against the member 98 by springs I4, the degree of pressure of which is regulated by a ring nut 79 in the barrel 46.
The shaft 62 further carries a portion 78 on which planet gears are also carried for engagement with the orbital gear 58 and another sun gear, and connected to other elements completing a gear train for reducing the speed of a driving or motor shaft, to the right of the structure shown, to the speed desired of the barrel 45.
A feature of the invention resides in providing a cylindrical extension 89 of the nut 29 adapted to closely embrace the shank It of the member I9, and to extend axially to a position, short of the outer end of the shank in the retracted position of the member I9, leaving a length L of the shank between the jaws I2 and the adjacent end of the extension 89 constituting, in effect, a radially inward step from the radially outer surface of the extension 89 to the radially outer surface of the shank 18.
An end housing portion 82, having a radial flange 84 secured to a radial flange 88 of the housing portion 48, as by screws 88, is mounted with the portion 48, as by studs 99 extending through the flanges 89 and 89 and into a portion 92 of an engine crank casing.
The portion 82, constituting a portion of the unit 48, in this instance, has an axially extending annular flange 94 provided with radial apertures, around and about which flange, and through which apertures, a single ring body 99 of the unit I8 extends.
The body 96 is constructed, as of neoprene or the like, molded to have flexible radially inner axially offset portions 99 and H39 substantially corresponding in inner diameter to the outer diameters of the shank I6 and the nut 29, respectively. Each of the portions 99 and 299 is of substantially C-section forming annular grooves opening to the left, as shown, with at least the portion 98 provided, in this instance, with a labyrinth i823 of annular inner surface grooves facilitating wiping of oil from the shank in its movement to the right from its extended position to its retracted position shown.
The body 98 is locally vulcanized around and about the flange 94, and in the apertures of the flange, to strongly and rigidly anchor the body at these positions, and to leave the remainder of the body resilient, the body 96 thereby being positively interlocked with the housing portion 82 both axially and annularly and having effective yieldability for radially inward compression of the portions 98 and I99 against the shank I8 and the nut 24, respectively.
A garter spring I94, in the groove of the portion 98, has its radially inward pressing force chosen not only to provide an elfective seal, but to effect sufiicient friction on the member 19 for holding the latter for axial movement by the screw shaft 22 through the intermediary of the spring 39, as hereinabove mentioned.
A garter spring I96, in the groove of the portion I99 has its radially inward pressing force chosen to provide an effective seal against rotation of the nut 24 only.
Both of the portions I99 and 98, before assembly, with the nut extension 89 and the member I9, respectively, are formed with the radially inner surfaces thereofconvergingly tapered from right to left, in which condition, with neither the extension 89 nor the member I9 in position, the grooves of the portions I89 and 99 are more open than they are as shown. Also, in this condition, the free edge tips, of the grooves may be bent counterclockwise, as viewed at the top of the ring in Figure 1, relative to the more solid parts of the body 98, to further open the grooves for the reception of the springs 186 and it.
When the body 96 is axially pressed onto the extension 89 and the member I9, the groove walls in the portion I99 close to a position as shown around the spring I86 from which the latter, or parts thereof, cannot escape from the unit it. The body 96 has an annular surface 133 diverging to the left from a position near the spring I89, the shortest distance between which surface I98 and the free edge tip of the groove in the portion 98, is substantially less than the section diameter of the rim of the spring I99, in operative position as shown. Prior to assembly, the groove in the portion 98 is more open, for reasons above stated, and may be further opened to admit the spring I94 to the groove. When the portion 98 is pressed axially over the member I9, the free edge tip of the groove automatically closes around the spring I94 to prevent parts of the spring, in case of breakage, from falling into the engine casing 92.
In operation, the portion I99 is never subjected to any rubbing action except the rotative rubbing of the nut 24, during the first rotation of which nut the portion 98 is subjected to axial rubbing only. After the shoulder 29 engages the shoulder 28 both portions 98and I99 are subjected to rotative rubbing, in which the rubbing on the portion I99 isslightly faster than that on the portion 98 by reason of the slightly large diameter of the nut 24 relative to the diameter of the member 19.
In Figures 2 and 3 corresponding parts are designated by corresponding reference characters, in Figure 2 of which the construction and operation are similar to those of the device of Figure l, with the exceptions that the single body 99 is omitted and, in its place, are substituted the portions 98 and I99 as separate bodies. The portion or body I99 is vulcanized to the flange 99, extending axially oppositely to its direction of Figure 1, and the portion or body 98 is vulcanized to a similar flange extending, in the direction of the flange 94 of Figure 1, from a separate annular member 99 secured to the end housing portion 82.
In Figure 3, the portion or body Hill is retained, and a, split friction ring H2, as of Phosphor bronze, is substituted for the portion or body 98, and movably held, as by a ring I 14 secured to the end housing portion 82, for spring action against the member 10.
Although only three embodiments of the invention have been illustrated and described, various changes in the form and relative arrange,- ments of the parts, which will now appear to those skilled in the art, may be made without departing from the scope of the invention. Reference is, therefore, to be had to the appended claims for a definition of the limits of the invention.
What is claimed is: 1. In a direct-cranking engine starter compriing a housing, a screw shaft, a starter jaw member adapted for movement axially outwardly of the housing for engaging and rotative movement for rotating an engine jaw element and having a hollow shank portion providing for axial relative movement between the shaft and the jaw member, spring means axially compressible by and between said jaw member and said shaft, the combination of an axially stationary rotatably driven hollow nut having long-lead screw connection to said shaft thereabout and including a cylindrical extension adapted to closely axially and rotatively embrace said shank portion throughout the axial movement of the jaw member and in retracted position having its outer end short of the outer end of said shank portion leavin a length of the latter between the jaws of the jaw member and said outer nut extension end, a onepiece ring of rubber or the like around the axis of said shank having radially outer portions vulcanized to said housing and radially inner axially ofiset first and second portions of different internal diameters around and engaging said shank length and said nut adjacent to said outer nut extension end, respectively, said first and second portions being of substantially C-section forming channels opening toward the jaws of said member, a garter spring in said second channel exerting radially inward sealing pressure against said extension end, and a garter spring in said .first channel exerting radially inward pressure against said shank sealing and frictionally holding said shank length in the retracted position of the jaw member and adapted to continue its friction seal pressure on the shank during axial movement of said jaw member between the retracted and the engine jaw element engaging positions of the starter jaw member.
2. In a direct-cranking engine starter comprising a housing, a screw shaft, a starter jaw member adapted for movement axially outwardly of the housing for engaging and rotative movement for rotating an engine jaw element and having a, hollow shank portion providing for axial relative movement between the shaft and the jaw member, spring means axially compressible by and between said jaw member and said shaft, the combination of an axially stationary rotatably driven hollow nut having long-lead screw connection to said shaft thereabout and including a cylindrical extension adapted to closely axially and: rotatively embrace said shank portion throughout the axial movement of the jaw member and in retracted position having its outer end short'of the outer end of said shank portion leaving a length of the latter between the jaws of the jaw member and said outer nut extension end, a ring seal supported by said housing around said nut adjacent to said outer nut extension end, and a combined seal and friction ring supported by said housing and frictionally engaging and sealing said shank length in the retracted position of the jaw member and adapted to continue its friction seal engagement with the shank during axial movement of said jaw member between the retracted and the engine jaw element engaging positions of the starter jaw member.
3. In a direct-cranking engine starter comprising a housing, a screw shaft, a starter jaw member adapted for movement axially outward- -1y of the housing for engaging and rotative movement for rotating an engine jaw element and having a hollow shank portion providing for axial relative movement between the shaft and the jaw member, resilient means axially compressible by and between said jaw member and said shaft,
an axially stationary rotatably driven hollow nut having long-lead screw connection to said shaft thereabout, driving means for the starter jaw member including a barrel surrounding the hollow nut and having a ring-receiving portion, torque-limiting friction disc means having interlayered discs axially-movably non-rotatively splined to the hollow nut and the barrel, respectively, means including spring means for pressing said discs together, and means for backing said spring means including a ring supported by said ring-receiving portion and locked to the barrel, the combination of a cylindrical extension of said nut adapted to closely axially and rotatively embrace said shank portion throughoutthe axial movement of the jaw member and in retracted position having its outer end short of the outer end of said sank portion leaving a length of the latter between the jaws of the jaw member and said outer nut extension end, a ring seal supported by said housing around said nut adjacent to said outer nut extension end, and means supported by said housing and frictionally engaging said shank length in the retracted position of the jaw member and adapted to continue its frictional engagement with the shank during axial move ment of said jaw member between the retracted and the engine jaw element engaging positions of the starter jaw member.
CHARLES S. METSGER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US709271A US2540208A (en) | 1946-11-12 | 1946-11-12 | Friction holding and sealing means for direct cranking engine starters and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US709271A US2540208A (en) | 1946-11-12 | 1946-11-12 | Friction holding and sealing means for direct cranking engine starters and the like |
Publications (1)
Publication Number | Publication Date |
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US2540208A true US2540208A (en) | 1951-02-06 |
Family
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Application Number | Title | Priority Date | Filing Date |
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US709271A Expired - Lifetime US2540208A (en) | 1946-11-12 | 1946-11-12 | Friction holding and sealing means for direct cranking engine starters and the like |
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US (1) | US2540208A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1047533B (en) * | 1953-04-16 | 1958-12-24 | Bendix Aviat Corp | Starting device for internal combustion engines |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1730220A (en) * | 1925-12-11 | 1929-10-01 | Eclipse Machine Co | Combined engine starter and driving means for mechanisms |
US2329929A (en) * | 1942-12-23 | 1943-09-21 | Bendix Aviat Corp | Engine starting mechanism |
US2334657A (en) * | 1942-07-30 | 1943-11-16 | Gen Motors Corp | Engine starting mechanism |
US2349867A (en) * | 1942-07-07 | 1944-05-30 | Jack & Heintz Inc | Starter |
US2412829A (en) * | 1944-06-22 | 1946-12-17 | Bendix Aviat Corp | Engine starting mechanism |
-
1946
- 1946-11-12 US US709271A patent/US2540208A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1730220A (en) * | 1925-12-11 | 1929-10-01 | Eclipse Machine Co | Combined engine starter and driving means for mechanisms |
US2349867A (en) * | 1942-07-07 | 1944-05-30 | Jack & Heintz Inc | Starter |
US2334657A (en) * | 1942-07-30 | 1943-11-16 | Gen Motors Corp | Engine starting mechanism |
US2329929A (en) * | 1942-12-23 | 1943-09-21 | Bendix Aviat Corp | Engine starting mechanism |
US2412829A (en) * | 1944-06-22 | 1946-12-17 | Bendix Aviat Corp | Engine starting mechanism |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1047533B (en) * | 1953-04-16 | 1958-12-24 | Bendix Aviat Corp | Starting device for internal combustion engines |
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