US1390464A - Propeller-shaft mounting - Google Patents

Propeller-shaft mounting Download PDF

Info

Publication number
US1390464A
US1390464A US263780A US26378018A US1390464A US 1390464 A US1390464 A US 1390464A US 263780 A US263780 A US 263780A US 26378018 A US26378018 A US 26378018A US 1390464 A US1390464 A US 1390464A
Authority
US
United States
Prior art keywords
propeller shaft
bearings
casing
shaft
propeller
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
US263780A
Inventor
Antoine G Senstius
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.)
Jeep Corp
Original Assignee
Willys Overland Co
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 Willys Overland Co filed Critical Willys Overland Co
Priority to US263780A priority Critical patent/US1390464A/en
Application granted granted Critical
Publication of US1390464A publication Critical patent/US1390464A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K17/00Arrangement or mounting of transmissions in vehicles
    • B60K17/22Arrangement or mounting of transmissions in vehicles characterised by arrangement, location, or type of main drive shafting, e.g. cardan shaft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10Suppression of vibrations in rotating systems by making use of members moving with the system
    • 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
    • Y10T74/21Elements
    • Y10T74/2173Cranks and wrist pins
    • Y10T74/2183Counterbalanced
    • Y10T74/2184Vibration dampers

Definitions

  • My invention relates to propeller shaft mounting, and more particularly to a form of propeller shaft mounting designed for preventing Whipping or vibrating of the propeller shaft, when a heavy load is being carried thereby, or when the propeller shaft is subjected toa sudden shock, such as may be occasioned by a sudden change in the amount of the load.
  • ()ne object of my invention is to provide a device of this character, which will prevent the whipping or vibrating of that portion of a propeller shaft which is intermediate the bearings, and which has a tendency to buckle or vibrate when suddenly subjected to a heavy strain thereon.
  • a further object of In invention is to provide a device of this 0 aracter whichis simple in construction and eflicient in operation, under varying conditions of use.
  • Figure I is a horizontal sectional view of a propeller shaft casing, showing my improved mounting as applied to the propeller shaft therein.
  • Fig. II is an'enlarged view of that portion of the structure shown in Fig. I, showing the mounting as applied to the propeller shaft.
  • Fig. III is a vertical sectional view of the propeller shaft casin along the line III-III of Figs. I and II;
  • Fig. IV is an enlargedhorizontal sectional view of a portion of a propellershaft casing
  • Fig. V is a vertical sectional view of a pro eller shaft casing taken alon-g the line V- of Fig. IV.
  • My invention comprises generally devices of the character set forth designed to be ap-' plied to a rotating shaft passing through a caslng, at a point intermediate the bearing portions thereof, for'thepurposes set forth above.
  • the propeller shaft housing 12 comprises a portion 13 attached to the-rear axle housing in any suitable manner, to which is securely attached the main 'propeller shaft casing 14, which is in turn connected by a slip joint 15 to that portion 16 of the uniyersal joint casing which extends rearwardly from the transmission casing.
  • Extending from the transmission easing into the universal joint housing 17 is a main transmission shaft 18, connected by means of a universaljoint 19 and aslip joint 20 to the usual propeller shaft 21.
  • the propeller shaft 21 is mounted for rotation at 'a point near its forward end in a bearing member 21 carried by the main portion 14 of the propeller casing.
  • the propeller shaft 21 carries a bevel driving pinion 22 securely attached thereto at a point near the rear end of the propeller shaft, which bevel driving pinion meshes with a bevel driving ring 24, to drive the rear axle sections (not shown) in the usual manner.
  • a point near its rear extremity the propeller shaft 21 is mounted in a bearing 25 supported by the section 13 of the housing.
  • a ring 26 which is firmly attached to the casing in any suitable manner, and is provided at one end with an inturned flange 27.
  • This flange portion lies in proximity to the outer circumferential surface of the propeller shaft, the diameter of the circular opening formed by the flange being a little larger than the diameter of the propeller shaft, so that normally the propeller shaft runs freely between the two bearings. Any whipping or vibrating of the propeller shaft between the bearings, such as might be occasioned by a heavy load upon the propeller shaft, or by a sudden increase in load, will be prevented by the flanged collar positioned as shown intermediate of the two bearings.
  • FIGs. IV and V A modified form of my invention is shown in Figs. IV and V, wherein a plurality of set screws 28 are fitted into interiorally threaded openings 29 in the propeller shaft casing 14 at diametrically opposed points thereof, and held in adjusted position by clamping nuts 30.
  • the set screws 28 are provided with angular end portions 81 for securing the proper adjustment of the set screwsrelative to the propeller shaft.
  • the set screws 28 may be positioned in a common vertical plane in the casing and their inner ends, when properly adjusted, may be separated from the propeller shaft by slight clearance space, which permits the propeller shaft to normally run freely in the bearings without touching th ends of the set screws.
  • a propeller shaft in combination, a propeller shaft, bearings near the ends thereof, and means su ported inde pendently of the shaft'intermec iate the bearings for preventing whipping of the propeller shaft. 4
  • a propeller shaft in combination, a propeller shaft, bearings therefor, and means supported independently of the shaft intermediate the bearings providing a slight clearance space for the propeller shaft for preventing whipping of the same.
  • a propeller shaft in combination, a propeller shaft, a dasing therefor, propeller shaft bearings supported by the casing, and means carried by the casing for preventing undue vibration of the propeller shaft.
  • a propeller shaft in combination, a propeller shaft, a casing therefor, propeller shaft bearings supported by the casing, and a plurality of means carried by the casing for preventing vibration of the propeller shaft.
  • a propeller shaft in combination, a propeller shaft, a' casing therefor, propeller shaft bearings, and a plurality of set screws carried b the casing intermediate the said bearings or preventing vibration of the propeller shaft.
  • a propeller shaft in combination, a propeller shaft, a casing therefor, propeller shaft bearings, the casing and bearings being rigidly supported with respect to each other, and means carried by the casing intermediate the bearings and normally free of the shaft for preventing vibration of the shaft.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Support Of The Bearing (AREA)
  • Motor Power Transmission Devices (AREA)

Description

} A. G. SENSTIUS. PROPELLER SHAFT MOUNTING.
APPLICATION FILED NOV. 22. 1918.
Patented Sept.
, INVENTOR. v 14/7/0/l78 6. Sensf/us A TTORNEY OFFICE.
ANTOINE G. SENSTIUS, OF TOLEDO, OHIO, ASSIGNOR TO THE WILLYS-OVERLAND COM- PANY, OF TOLEDO, OHIO, CORPORATION OF OHIO. i
PROPELLER-fiHAFT MOUNTING.
Specification of Letters Patent.
Patented Sept. 13, 1921.
T 0 all 20 ham it may concern Be it known that I, ANTOINE G. SENs'rIUs,
citizen of the United States, residing at Toledo, county of Lucas, and State of Ohio, have invented certain new and useful Improvements in Propeller-Shaft Mountings, of which I declare the following to be a full, clear, and exact description.
My invention relates to propeller shaft mounting, and more particularly to a form of propeller shaft mounting designed for preventing Whipping or vibrating of the propeller shaft, when a heavy load is being carried thereby, or when the propeller shaft is subjected toa sudden shock, such as may be occasioned by a sudden change in the amount of the load.
()ne object of my invention is to provide a device of this character, which will prevent the whipping or vibrating of that portion of a propeller shaft which is intermediate the bearings, and which has a tendency to buckle or vibrate when suddenly subjected to a heavy strain thereon.
A further object of In invention is to provide a device of this 0 aracter whichis simple in construction and eflicient in operation, under varying conditions of use.
Further objects of this invention relate to economics of manufacture and details of construction as will hereinafter appear from the detailed description to follow.
I accomplish the objects of my invention in one instance by the devices and means described in the following specification, but it is evident that the same may be varied widely without departing from the scope of the invention, as pointed out in the appended claims.
- A structure constituting one embodiment of my invention, which may be the preferred,
is illustrated in the accompanying drawing,
forming a part hereof, in which:
Figure I is a horizontal sectional view of a propeller shaft casing, showing my improved mounting as applied to the propeller shaft therein.
Fig. II is an'enlarged view of that portion of the structure shown in Fig. I, showing the mounting as applied to the propeller shaft. Fig. III is a vertical sectional view of the propeller shaft casin along the line III-III of Figs. I and II;
Fig. IV is an enlargedhorizontal sectional view of a portion of a propellershaft casing,
showing a modified form of my propeller shaft mounting.
Fig. V is a vertical sectional view of a pro eller shaft casing taken alon-g the line V- of Fig. IV.
My invention comprises generally devices of the character set forth designed to be ap-' plied to a rotating shaft passing through a caslng, at a point intermediate the bearing portions thereof, for'thepurposes set forth above.
I have illustrated my device as applied to the usual propeller shaft of an automoblle, such as usually have a relatively long portion of the propeller shaft intermediate of the bearings thereof.
Referring to the numbered parts of the drawing, I have shown the usual transmiss1on casing 10 and rear axle housing -11, which are connected by the propeller shaft housing 12. The propeller shaft housing 12 comprises a portion 13 attached to the-rear axle housing in any suitable manner, to which is securely attached the main 'propeller shaft casing 14, which is in turn connected by a slip joint 15 to that portion 16 of the uniyersal joint casing which extends rearwardly from the transmission casing. Extending from the transmission easing into the universal joint housing 17 is a main transmission shaft 18, connected by means of a universaljoint 19 and aslip joint 20 to the usual propeller shaft 21. The propeller shaft 21 is mounted for rotation at 'a point near its forward end in a bearing member 21 carried by the main portion 14 of the propeller casing. The propeller shaft 21 carries a bevel driving pinion 22 securely attached thereto at a point near the rear end of the propeller shaft, which bevel driving pinion meshes with a bevel driving ring 24, to drive the rear axle sections (not shown) in the usual manner. -At a point near its rear extremity the propeller shaft 21 is mounted in a bearing 25 supported by the section 13 of the housing. Intermediate the bearings 21 and 25 is a ring 26, which is firmly attached to the casing in any suitable manner, and is provided at one end with an inturned flange 27. The inner circumferential face of this flange portion lies in proximity to the outer circumferential surface of the propeller shaft, the diameter of the circular opening formed by the flange being a little larger than the diameter of the propeller shaft, so that normally the propeller shaft runs freely between the two bearings. Any whipping or vibrating of the propeller shaft between the bearings, such as might be occasioned by a heavy load upon the propeller shaft, or by a sudden increase in load, will be prevented by the flanged collar positioned as shown intermediate of the two bearings.
A modified form of my invention is shown in Figs. IV and V, wherein a plurality of set screws 28 are fitted into interiorally threaded openings 29 in the propeller shaft casing 14 at diametrically opposed points thereof, and held in adjusted position by clamping nuts 30. The set screws 28 are provided with angular end portions 81 for securing the proper adjustment of the set screwsrelative to the propeller shaft. The set screws 28 may be positioned in a common vertical plane in the casing and their inner ends, when properly adjusted, may be separated from the propeller shaft by slight clearance space, which permits the propeller shaft to normally run freely in the bearings without touching th ends of the set screws. When, however, a heavy load is suddenly placed upon the propeller shaft, such as would cause a whipping or vibrating of the propeller shaft, such vibration is overcome by the shaft striking the end of the set screws. Thus it will be seen that I have provided a simple and economical means, which is capable of being readily positioned in the casing, for overcoming any excessive vibration of the propeller shaft in a direction transverse thereof, such as is liable to occur when the shaft is suddenly subjected to a considerable strain, as by a sudden increase in the power exerted upon the rear axle sections. It is obvious that such vibrations, when set up in th propeller shaft, tend to place an undue strain thereon if not counteracted, and that by the means shown and described the amplitude of these vibrations will be diminished so as to practically eliminate the same. While it is old to insert a plurality of bearings for supporting the propeller shaft at intervals along its length, my invention obviates the necessity of using an intermediate bearing where a relatively long propeller shaft is employed, by substituting means which normally provides a slight clearance space around the propeller shaft, while extending sufficiently close to the shaft to dampe any vibration which may be set up therein.
While I have shown and. described in considerable detail a specific embodiment of my invention, it is to be understood that this showing and description is illustrated only for the purops of rendering my invention more clear, and that I do not regard the invention as limited to the details of construction illustrated or described, nor to any of them, except in so far as I have included such limitations within the terms of the following claims, i which it is my intention to claim all novelty in my invention broadly, as well as s ecifically.
aving thus described my invention, what I claim as new and desire to secure by Letters Patent is: j
1. In a device of the classdescribed, in combination, a propeller shaft, bearings near the ends thereof, and means su ported inde pendently of the shaft'intermec iate the bearings for preventing whipping of the propeller shaft. 4
2. In a device of the class described, in combination, a propeller shaft, bearings therefor, and means supported independently of the shaft intermediate the bearings providing a slight clearance space for the propeller shaft for preventing whipping of the same.
3. In a device of the class described, in combination, a propeller shaft, bearings therefor, and means supported independently of the shaft intermediate the bearings for preventing vibration of the propeller shaft. J
4. In a device of the class described, in combination, a, propeller shaft, bearings therefor, and means supported independently of the shaft for preventing excessive vibration of that portion of the propeller shaft positioned between the bearings.
5. In a device of the class described, in combination, a propeller shaft, a dasing therefor, propeller shaft bearings supported by the casing, and means carried by the casing for preventing undue vibration of the propeller shaft.
6. In a device of the class described, in combination, a propeller shaft, a casing therefor, propeller shaft bearings supported by the casing, and a plurality of means carried by the casing for preventing vibration of the propeller shaft.
7. In a device of the class described, in combination, a propeller shaft, a' casing therefor, propeller shaft bearings, and a plurality of set screws carried b the casing intermediate the said bearings or preventing vibration of the propeller shaft.
8. In a device of the class described, in combination, a propeller shaft, a casing therefor, propeller shaft bearings, the casing and bearings being rigidly supported with respect to each other, and means carried by the casing intermediate the bearings and normally free of the shaft for preventing vibration of the shaft.
In testimony whereof I aflix mysignature.
' ANTOINE e. SENSTIUS.
US263780A 1918-11-22 1918-11-22 Propeller-shaft mounting Expired - Lifetime US1390464A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US263780A US1390464A (en) 1918-11-22 1918-11-22 Propeller-shaft mounting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US263780A US1390464A (en) 1918-11-22 1918-11-22 Propeller-shaft mounting

Publications (1)

Publication Number Publication Date
US1390464A true US1390464A (en) 1921-09-13

Family

ID=23003195

Family Applications (1)

Application Number Title Priority Date Filing Date
US263780A Expired - Lifetime US1390464A (en) 1918-11-22 1918-11-22 Propeller-shaft mounting

Country Status (1)

Country Link
US (1) US1390464A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2558623A (en) * 1946-07-31 1951-06-26 Elgin Sweeper Co Side broom assembly and drive
US2838957A (en) * 1954-06-14 1958-06-17 Gen Motors Corp Engine balancing means
US2862453A (en) * 1954-04-01 1958-12-02 Perry I Nagle Adjustable pump support
US2986373A (en) * 1957-01-16 1961-05-30 James Gordon & Co Ltd Butterfly valves
US3291284A (en) * 1964-03-04 1966-12-13 Int Harvester Co Mechanical drive for bale thrower
US4854184A (en) * 1983-11-07 1989-08-08 Jessup Thurman W Support system for shaft
US20080302584A1 (en) * 2007-06-07 2008-12-11 Pleuss Alan E Drive shaft coupling and method, and equipment using same

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2558623A (en) * 1946-07-31 1951-06-26 Elgin Sweeper Co Side broom assembly and drive
US2862453A (en) * 1954-04-01 1958-12-02 Perry I Nagle Adjustable pump support
US2838957A (en) * 1954-06-14 1958-06-17 Gen Motors Corp Engine balancing means
US2986373A (en) * 1957-01-16 1961-05-30 James Gordon & Co Ltd Butterfly valves
US3291284A (en) * 1964-03-04 1966-12-13 Int Harvester Co Mechanical drive for bale thrower
US4854184A (en) * 1983-11-07 1989-08-08 Jessup Thurman W Support system for shaft
US20080302584A1 (en) * 2007-06-07 2008-12-11 Pleuss Alan E Drive shaft coupling and method, and equipment using same

Similar Documents

Publication Publication Date Title
US2041555A (en) Combination fan and vibration damper
US2174010A (en) Coupling device
US1390464A (en) Propeller-shaft mounting
US2450279A (en) Resilient shaft hanger
US2647380A (en) Flexible shaft
US2305454A (en) Bearing for air propeller shafts
US4722707A (en) Transmission for small boat
US3146612A (en) Coupling
US2772547A (en) Universal joint and bushing replacement assembly for a drive shaft assembly
US2270583A (en) Sound insulated drive connection
US2883885A (en) Turbine or compressor rotors
US2772649A (en) Motor mounting system
US2329606A (en) Propeller fairing
US2923460A (en) Blower unit
US2097318A (en) Fan
US2166259A (en) Shaft bearing
US1481024A (en) Flying machine
US3175636A (en) Curved propeller shaft rotatably supported in a plastic sheath
US2595863A (en) Mounting for driving units on motorboats
US1536824A (en) Rear-axle center
US2149122A (en) Shaft mounting
US3597105A (en) Power takeoff centrifugal pump with ring and pinion drive
US1993912A (en) Vehicle motor and rear axle connection
US2727577A (en) Propeller mounting
US2238737A (en) Propeller shaft mounting