US2861557A - Hydraulic timer - Google Patents

Hydraulic timer Download PDF

Info

Publication number
US2861557A
US2861557A US627799A US62779956A US2861557A US 2861557 A US2861557 A US 2861557A US 627799 A US627799 A US 627799A US 62779956 A US62779956 A US 62779956A US 2861557 A US2861557 A US 2861557A
Authority
US
United States
Prior art keywords
vanes
hub
cover
chamber
driven
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
US627799A
Inventor
Richard C Stolte
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation 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 Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to US627799A priority Critical patent/US2861557A/en
Application granted granted Critical
Publication of US2861557A publication Critical patent/US2861557A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L1/00Valve-gear or valve arrangements, e.g. lift-valve gear
    • F01L1/34Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
    • F01L1/344Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear
    • F01L1/3442Valve-gear or valve arrangements, e.g. lift-valve gear characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift changing the angular relationship between crankshaft and camshaft, e.g. using helicoidal gear using hydraulic chambers with variable volume to transmit the rotating force

Definitions

  • the inventio-n relates to a hydraulic advance and retard mechanism and more particularly to such a mechanism which automatically advances and retards the cam shaft of an internal combustion engine in relation to the speed of the engine.
  • the invention is also applicable to other mechanisms in which one member is to be rotated relative to a second member while torque is being continuously transmitted between the two members.
  • the invention includes a hydraulic advance and retard mechanism which is hydraulically actuated and connects two members through a uid drive while a mechanical linkage is maintained in reserve which will continue to drive the controlled member should the hydraulic system become inoperative.
  • the hydraulic actuation system is controlled by a governor sensitive to the speed of the engine, and this governor is preferably formed as an integral part of the advance and retard mechanism.
  • Figure 1 illustrates an advance and retard mechanism embodying the invention and having parts broken away and in section.
  • Figure 2 is a partial view taken in the direction of arrows 2-2 of Figure l and having parts in section.
  • Figure 3 is a partial view taken in the direction of arrows 3 3 of Figure l and having parts in section.
  • Figure 4 is a partial view taken in the direction of arrows 4-4 of Figure 1 and having parts in section.
  • Figure 5 is a fragmentary view of a portion of the governor included in the mechanism of Figure 1 and taken in the direction of arrows 5-5 of Figure l.
  • the advance and retard mechanism may be hydraulically actuated to advance a member from normally retarded position or to retard a member from a normally advanced position.
  • the device shown in the drawing advances one member from a normally retarded position relative to a second member as the engine speed increases.
  • a drive gear 10, which maybe driven by the timing gears or equivalent linkage in timed relation to the engine crank shaft, may be formed with a radially extending web 12 and a cylindrical hub 14.
  • Hub 14 is preferably .i 2,861,557 Patented Nov. 25, 1958 ice formed with an axially located cavity or chamber 16 which is defined by a radial wall 18 and the cylinder formed by hub 14.
  • Web 12 and wall 18 are axially spaced and positioned adjacent either end of the cavity 16, web 12 extending radially outward from the cavity and wall 18 providing an end cover for the cavity.
  • Wall 1S may be provided with a boss 20 which is axially drilled and reamed to form a bearing surface 22.
  • a driven member 24, which may be the cam shaft of an internal combustion engine, is rotatably received within hub 14 and is in contact with bearing surface 22 for support by boss 20.
  • a pluraiity of equi-spaced driving vanes may be integrally formed with cylindrical hub 14 and extend radially inward in cavity 16. While two or more vanes may be used, only two vanes 26, 28 are illustrated for simplicity. Vanes 26 and 28 extend axially within cavity 16 from radial wall 18 to a transverse plane defined by the outer edge 36 of web 12. These vanes also extend inwardly from cylindrical hub 14 to a point radially spaced intermediate bearing surface 22 and hub 14.
  • a cover 32 may be suitably secured to web 12 and extend axially in a direction opposite hub 14 and be provided with an inwardly extending hub 34.
  • An internal bearing surface 36 is formed in hub 34 and is adapted to rotatably receive driven shaft 24. Bearing surfaces 22 and 36 therefore provide axially spaced supports for the shaft 24.
  • the portion o-f shaft 24 which passes through cavity 16 may have an annular hub 38 secured thereto by any convenient means such as key 40.
  • integrally formed with or secured to hub 38 are two or more equi-spaced driven vanes, the number o-f such vanes being equal to the number of driving vanes formed with cylindrical hub 14.
  • Two such driven vanes 42 and 44 are illustrated.
  • the external diameter of hub 38 is substantially equal to the internal diameter formed by the inwardly extend ing ends of vanes 26 and 28.
  • the outer ends of vanes 42 and 44 are substantially equal Vto the internal diameter of that portion of hub 14 which defines cylindrical cavity 16. Vanes 42 and 44 are therefore circumferentially spaced from and coaxial with vanes 26 and 28 and are comparable to rotary pistons within arcuate chambers.
  • Cavity 16 is provided with a cover 46 which is axially positioned adjacent the outer surface 30 of web 12 and extends inwardly into rotatable engagement with shaft 24.
  • Cover 46 may be positioned adjacent the edges of driven vanes 42 and 44 and be rotatable with respect to these vanes, web 12 and shaft 24.
  • the surface of cover 46 opposite the surface adjoining vanes 42 and 44 may be provided with two or more depressions which are preferably each formed with an arcuate cross section and are adapted to receive a governor ball-type weight within each depression.
  • Two depressions 48 and Sti which are adapted to respectivelyY receive governor ball weights 52 and 54, are illustrated.
  • the depressions 48 and 5t? extend radially outward from circumferentially spaced positions intermediate shaft 24 and cover 32 and are inclined in the radial transverse plane so that their extended center lines do not pass through the axis of shaft 24.
  • the depressions are inclined in the same circumferential direction as is best illustratedY in Figure 3.
  • Hub 34 of cover 32 may be provided with an external spline or key 56 which is adapted to receive a governor driving plate 5S on which an internal spline or a keyway is formed to cooperate with external spline or key 56.V
  • Plate 5S is therefore non-rotatably mounted on hub 34 and may be axially slidable on spline or key 56.
  • a compression spring 66 may be providedbetween plate y58 and cover 32 to urge plate 58 axially toward cover 46.
  • the side of plate 58 adjacent cover 46 is provided with depressions 62 and 64 which are similar to depressions 48 and-56, but are oppositely inclined in the radialV transverse plane. The opposite inclinations are best illustrated in Figure 2.
  • the outer ends 66 and 68 of depressions 62 and 64 are axially spaced from the inner ends of these .depressions in a direction toward cover 46, thuscausing the bottom of depressions 62 and 64 to form an acute angle with the bottom ofdepressions 48 and 5t).
  • the apex of the angleso formed is radially outward of the depressions as is best shown in Figure l.
  • plate '58 is driven at the same angular velocity, driving 52 and 54 and cover 46.
  • ecntrifugalrorces acting on the ball weights 52 and S4overco-methe relatively inclined planes presentedby the bottoms of depressions 62 and 64 and the force exerted byspring 69.
  • the Weights move radially outward in the depressions formed in cover 46 and plate S8 in response to these forces. Since the depressions are oppositely inclined, this radialmovement of the weights causes rotational movement of cover 46 relative to plate 58.
  • Cover 46 is providedwith a plurality of vane positioning ports which are equal in number to the vanes 26 and 28, two such ports 70 and 72 being illustrated. While these ports are shown as having arectangular cross section, vthey may beformcd with variable areas to obtain advance and retard actuation of the shaft 24 at rates other than that obtained by rectangular ports or orifices. Oil and air-escape orifices are also provided in cover and are so circumferentially spaced from ports 70 and 72 that any of the vanes 26, 28, 42 and 44 may be positioned between any two adjacentports and orifices without covering either. Two such voicess 74 and 76 are shown.
  • Shaft 24 is provided with a centrally drilled Huid supply passage 86 which terminates radially inward from hub 3S. Fluid under pressure, which may be engine lubricating oil, is supplied to this passage. Any uid all engine speeds to overcome Since the mechanisms timing action is not a function of the pressureto obtain hydraulic governor actuation, the pressure need not vary with engine speed.
  • Radially extending 88 and 9i) are drilled through shaft 24, hub 38 and vanes 42, 44 and connect at their inner ends with axial passage 86 in shaft 24. Passages 88 and 90 terminate radiallyinward from the outer ends of vanes 42 and 44.
  • Tangentially extending passages 92 and 94 are drilled in vanes 42 and 44 transversely of the axis of hub '38 and respectively connect passages 83 and 90 with-chambers V78 and Sti. Consequentlys 96 and 98 are provided fo-r filling torque damping chambers 82 and 84 and are appreciably smaller in cross section area than passages;92 and 94. Oritces96 and 98 connect passages 88 and 9.0 with torque damping chambers 82 and 84.
  • the mechanism for hydraulically adjusting the camshaft timing may be readily substituted in the space normally occupied by the camshaft drive gear with a minimum amount of changes. Oil under ⁇ pressure is normally supplied to a passage in the camshaft corresponding to passage S6 in order to lubricate the cams, eliminating the new uid supply system.
  • the mechanism will cifectively control the camshaft timing through an engine speed sensitive hydraulically adjustable drive. Should the Huid pressure supply be interrupted, the drive and driven vanes will engage and continue to drive the camshaft in the position normally assumed at engine idle. This mechanical safety feature permits the engine to be operated as necessary Without undue strain on the system.
  • Means for advancing and retarding an engine camshaft with respect to an engine crankshaft said means includingy a drive member and a driven member forming a fluid pressure chamber therebetween, said drive member being operatively connected for rotation with said crankshaft and said driven member being operatively and drivingly connected with said camshaft, and crankshaft speed responsive means for controlling the pressure of fluid in said chamber to advance and retard said camshaft with respect to said crankshaft.
  • a speed responsive device having drive and driven elements, said drive element being secured for rotation with said drive member, means: hydraulically connecting said drive member with said driven member, a source of hydraulic pressure and control-means actuated by said speed responsive device for controlling said. pressure in said hydraulic connecting means whereby said driven member is arcuately displaced relative to said driving member.
  • An advanceand retard mechanism for a camshaft in an internal combustion engine including a camshaft drive gear adapted to be driven by the crankshaft of said engine, said gear having a hub with a variable volume arcuate chamber formed therein, said camshaft extending coaxially through said hub and having a piston secured thereto, said piston being adapted to move in said chamber, means for supplying fluid under pressure to said chamber, a chamber cover having a chamber exhaust control orifice, said cover being coaxial with and rotatable relative to said gear and said camshaft, and means responsive to the speed of'said drive gear for arcuately positioning said cover and said orifice relative to said chamber whereby the volume of said chamber is varied in ⁇ accordance with drive. gear speed.
  • variable volume chamber adaptedto contain. hydraulicuid for transmitting torque hydraulically to said driven member from said drive member and control means responsive to the speed of said driving member for controlling said hydraulic fluid in said chamber.
  • a hydraulically actuated positioning mechanism for arcuately positioning a driven member relative to a drive member, said mechanism including a trst variable volume hydraulic chamber having iluid therein for transmitting torque from said drive member to said driven member and a seco-nd variable volume hydraulic chamber having fluid therein for damping torque fluctuations between said drive member and said driven member and means for controlling the volumes of said chambers whereby said driven member is arcuately positioned relative to said drive member in accordance with the speed of said drive member.
  • a hydraulically actuated timing mechanism including driving vanes and driven vanes and a source for delivering hydraulic uid under pressure intermediate said vanes and means for automatically controlling the application of said fluid under pressure intermediate said vanes to relatively displace said driving vanes and said driven vanes.
  • a driving member having an arcuate chamber formed therein
  • a driven member having a rotary piston positioned for arcuate movement within said chamber and means for moving said piston in said chamber in relation to the speed of said driving member.

Description

Nov. 25, 1958 R. c. s'roLTE HYDRAULIC TIMER Filed Deo. 12, 1956 A TTOPN Y aired tats 8 Claims. (Cl. 123-90) Birmingham, Mich., assigner to Gen- Detroit, Mich., a corporation The inventio-n relates to a hydraulic advance and retard mechanism and more particularly to such a mechanism which automatically advances and retards the cam shaft of an internal combustion engine in relation to the speed of the engine. The invention is also applicable to other mechanisms in which one member is to be rotated relative to a second member while torque is being continuously transmitted between the two members.
Advance and retard mechanisms previously proposed have inciuded mechanical linkages between the two members which may be either hydraulically, mechanically or otherwise actuated. There are several inherent advantages in the use of a hydraulically actuated mechanism, however the mechanical advance and retard devices which are remotely actuated by fluid pressure do not utilize these advantages to the fullest extent. When the mechanical linkage is replaced by a hydraulic linkage, for example, shock loads are materially reduced and the complexity of the entire mechanism is decreased.
The invention includes a hydraulic advance and retard mechanism which is hydraulically actuated and connects two members through a uid drive while a mechanical linkage is maintained in reserve which will continue to drive the controlled member should the hydraulic system become inoperative. The hydraulic actuation system is controlled by a governor sensitive to the speed of the engine, and this governor is preferably formed as an integral part of the advance and retard mechanism.
in the drawing:
Figure 1 illustrates an advance and retard mechanism embodying the invention and having parts broken away and in section.
Figure 2 is a partial view taken in the direction of arrows 2-2 of Figure l and having parts in section.
Figure 3 is a partial view taken in the direction of arrows 3 3 ofFigure l and having parts in section.
Figure 4 is a partial view taken in the direction of arrows 4-4 of Figure 1 and having parts in section.
Figure 5 is a fragmentary view of a portion of the governor included in the mechanism of Figure 1 and taken in the direction of arrows 5-5 of Figure l.
The advance and retard mechanism may be hydraulically actuated to advance a member from normally retarded position or to retard a member from a normally advanced position. The device shown in the drawing advances one member from a normally retarded position relative to a second member as the engine speed increases. Some engines, due to design and operating characteristics, give more satisfactory performance results by having the camshaft in a normally advanced position at idle speeds and retarding it as the engine speed increases. The mechanism embracing the invention may be readily modified to obtain this result while remaining within the scope of the invention.
A drive gear 10, which maybe driven by the timing gears or equivalent linkage in timed relation to the engine crank shaft, may be formed with a radially extending web 12 and a cylindrical hub 14. Hub 14 is preferably .i 2,861,557 Patented Nov. 25, 1958 ice formed with an axially located cavity or chamber 16 which is defined by a radial wall 18 and the cylinder formed by hub 14. Web 12 and wall 18 are axially spaced and positioned adjacent either end of the cavity 16, web 12 extending radially outward from the cavity and wall 18 providing an end cover for the cavity. Wall 1S may be provided with a boss 20 which is axially drilled and reamed to form a bearing surface 22. A driven member 24, which may be the cam shaft of an internal combustion engine, is rotatably received within hub 14 and is in contact with bearing surface 22 for support by boss 20.
A pluraiity of equi-spaced driving vanes may be integrally formed with cylindrical hub 14 and extend radially inward in cavity 16. While two or more vanes may be used, only two vanes 26, 28 are illustrated for simplicity. Vanes 26 and 28 extend axially within cavity 16 from radial wall 18 to a transverse plane defined by the outer edge 36 of web 12. These vanes also extend inwardly from cylindrical hub 14 to a point radially spaced intermediate bearing surface 22 and hub 14. A cover 32 may be suitably secured to web 12 and extend axially in a direction opposite hub 14 and be provided with an inwardly extending hub 34. An internal bearing surface 36 is formed in hub 34 and is adapted to rotatably receive driven shaft 24. Bearing surfaces 22 and 36 therefore provide axially spaced supports for the shaft 24.
The portion o-f shaft 24 which passes through cavity 16 may have an annular hub 38 secured thereto by any convenient means such as key 40. integrally formed with or secured to hub 38 are two or more equi-spaced driven vanes, the number o-f such vanes being equal to the number of driving vanes formed with cylindrical hub 14. Two such driven vanes 42 and 44 are illustrated. The external diameter of hub 38 is substantially equal to the internal diameter formed by the inwardly extend ing ends of vanes 26 and 28. The outer ends of vanes 42 and 44 are substantially equal Vto the internal diameter of that portion of hub 14 which defines cylindrical cavity 16. Vanes 42 and 44 are therefore circumferentially spaced from and coaxial with vanes 26 and 28 and are comparable to rotary pistons within arcuate chambers.
Cavity 16 is provided with a cover 46 which is axially positioned adjacent the outer surface 30 of web 12 and extends inwardly into rotatable engagement with shaft 24. Cover 46 may be positioned adjacent the edges of driven vanes 42 and 44 and be rotatable with respect to these vanes, web 12 and shaft 24.
The surface of cover 46 opposite the surface adjoining vanes 42 and 44 may be provided with two or more depressions which are preferably each formed with an arcuate cross section and are adapted to receive a governor ball-type weight within each depression. Two depressions 48 and Sti, which are adapted to respectivelyY receive governor ball weights 52 and 54, are illustrated. The depressions 48 and 5t? extend radially outward from circumferentially spaced positions intermediate shaft 24 and cover 32 and are inclined in the radial transverse plane so that their extended center lines do not pass through the axis of shaft 24. The depressions are inclined in the same circumferential direction as is best illustratedY in Figure 3.
Hub 34 of cover 32 may be provided with an external spline or key 56 which is adapted to receive a governor driving plate 5S on which an internal spline or a keyway is formed to cooperate with external spline or key 56.V
Plate 5S is therefore non-rotatably mounted on hub 34 and may be axially slidable on spline or key 56. A compression spring 66 may be providedbetween plate y58 and cover 32 to urge plate 58 axially toward cover 46. The side of plate 58 adjacent cover 46 is provided with depressions 62 and 64 which are similar to depressions 48 and-56, but are oppositely inclined in the radialV transverse plane. The opposite inclinations are best illustrated in Figure 2. The outer ends 66 and 68 of depressions 62 and 64 are axially spaced from the inner ends of these .depressions in a direction toward cover 46, thuscausing the bottom of depressions 62 and 64 to form an acute angle with the bottom ofdepressions 48 and 5t). The apex of the angleso formed is radially outward of the depressions as is best shown in Figure l.
Cover 46 and plate 58 in combination with the ball weights y52 and 54, which ride in the respective depressions` formed in thercover andthe plate, constitute a cen- When cover 32 is rotated through gear 10 and web 12, plate '58 is driven at the same angular velocity, driving 52 and 54 and cover 46. As the speed of increases, ecntrifugalrorces acting on the ball weights 52 and S4overco-methe relatively inclined planes presentedby the bottoms of depressions 62 and 64 and the force exerted byspring 69. The Weights move radially outward in the depressions formed in cover 46 and plate S8 in response to these forces. Since the depressions are oppositely inclined, this radialmovement of the weights causes rotational movement of cover 46 relative to plate 58.
Cover 46 is providedwith a plurality of vane positioning ports which are equal in number to the vanes 26 and 28, two such ports 70 and 72 being illustrated. While these ports are shown as having arectangular cross section, vthey may beformcd with variable areas to obtain advance and retard actuation of the shaft 24 at rates other than that obtained by rectangular ports or orifices. Oil and air-escape orifices are also provided in cover and are so circumferentially spaced from ports 70 and 72 that any of the vanes 26, 28, 42 and 44 may be positioned between any two adjacentports and orifices without covering either. Two such orices 74 and 76 are shown. The chamber 73 formed by adjacent vanes.26 and 42 and the chamber 8i) formed by adjacent vanes 28 and 44 act as'fluid receiving pockets. The chambers 82 and 84, respectively formed by vanes 26, 44 and 28, 42, act as torque damping chambers.
Shaft 24 is provided witha centrally drilled Huid supply passage 86 which terminates radially inward from hub 3S. Fluid under pressure, which may be engine lubricating oil, is supplied to this passage. Any uid all engine speeds to overcome Since the mechanisms timing action is not a function of the pressureto obtain hydraulic governor actuation, the pressure need not vary with engine speed. Radially extending 88 and 9i) are drilled through shaft 24, hub 38 and vanes 42, 44 and connect at their inner ends with axial passage 86 in shaft 24. Passages 88 and 90 terminate radiallyinward from the outer ends of vanes 42 and 44. Tangentially extending passages 92 and 94 are drilled in vanes 42 and 44 transversely of the axis of hub '38 and respectively connect passages 83 and 90 with-chambers V78 and Sti. Orices 96 and 98 are provided fo-r filling torque damping chambers 82 and 84 and are appreciably smaller in cross section area than passages;92 and 94. Oritces96 and 98 connect passages 88 and 9.0 with torque damping chambers 82 and 84.
When cover 46 is rotated relative to plate 58`by the centrifugal action of the governor ball Weights, vanepositioning ports 70 and 72, which are normally uncoveredVare rotatedrelative to. vanes 26 and 28 until the tiuid under pressure, which Vis supplied tochambers 78 and '80:through the above-described passages, is prevented .'fromescaping from those chambers due to the restriction of the positioning ports by vanes 26 and 28. This causesa buildup ofuid pressure in chambers 78 and 8.0 which acts on the respective vanes defining those chambers Aand causes vanes 42 and 44 torotate relative to vanes 26 and 28. This rotary movement is transmitted through hub 38 to shaft 24 and the shaft is therefore rotated relative to driving gear 1li. Fluid under pressure is continually delivered through passages 96 and 98 to torque-damping chambers 82 and 84. This tluid, and any air trapped in the damping chambers, is vented inoperative.
The mechanism for hydraulically adjusting the camshaft timing may be readily substituted in the space normally occupied by the camshaft drive gear with a minimum amount of changes. Oil under` pressure is normally supplied to a passage in the camshaft corresponding to passage S6 in order to lubricate the cams, eliminating the new uid supply system. The mechanism will cifectively control the camshaft timing through an engine speed sensitive hydraulically adjustable drive. Should the Huid pressure supply be interrupted, the drive and driven vanes will engage and continue to drive the camshaft in the position normally assumed at engine idle. This mechanical safety feature permits the engine to be operated as necessary Without undue strain on the system.
What is claimed is:
l. Means for advancing and retarding an engine camshaft with respect to an engine crankshaft, said means includingy a drive member and a driven member forming a fluid pressure chamber therebetween, said drive member being operatively connected for rotation with said crankshaft and said driven member being operatively and drivingly connected with said camshaft, and crankshaft speed responsive means for controlling the pressure of fluid in said chamber to advance and retard said camshaft with respect to said crankshaft.
2. In a mechanism for arcuately displacing a driven member relative to a drive member, a speed responsive device having drive and driven elements, said drive element being secured for rotation with said drive member, means: hydraulically connecting said drive member with said driven member, a source of hydraulic pressure and control-means actuated by said speed responsive device for controlling said. pressure in said hydraulic connecting means whereby said driven member is arcuately displaced relative to said driving member.
3. An advanceand retard mechanism for a camshaft in an internal combustion engine including a camshaft drive gear adapted to be driven by the crankshaft of said engine, said gear having a hub with a variable volume arcuate chamber formed therein, said camshaft extending coaxially through said hub and having a piston secured thereto, said piston being adapted to move in said chamber, means for supplying fluid under pressure to said chamber, a chamber cover having a chamber exhaust control orifice, said cover being coaxial with and rotatable relative to said gear and said camshaft, and means responsive to the speed of'said drive gear for arcuately positioning said cover and said orifice relative to said chamber whereby the volume of said chamber is varied in `accordance with drive. gear speed.
4. In combination in a hydraulic timing device having drive and driven members, a variable volume chamber adaptedto contain. hydraulicuid for transmitting torque hydraulically to said driven member from said drive member and control means responsive to the speed of said driving member for controlling said hydraulic fluid in said chamber.
5. A hydraulically actuated positioning mechanism for arcuately positioning a driven member relative to a drive member, said mechanism including a trst variable volume hydraulic chamber having iluid therein for transmitting torque from said drive member to said driven member and a seco-nd variable volume hydraulic chamber having fluid therein for damping torque fluctuations between said drive member and said driven member and means for controlling the volumes of said chambers whereby said driven member is arcuately positioned relative to said drive member in accordance with the speed of said drive member.
6. A hydraulically actuated timing mechanism including driving vanes and driven vanes and a source for delivering hydraulic uid under pressure intermediate said vanes and means for automatically controlling the application of said fluid under pressure intermediate said vanes to relatively displace said driving vanes and said driven vanes.
7. In combination, a driving member having an arcuate chamber formed therein, a driven member having a rotary piston positioned for arcuate movement within said chamber and means for moving said piston in said chamber in relation to the speed of said driving member.
8. In an advance and retard mechanism between two rotatable members, first means for hydraulically advancing and retarding and driving one of said members relative to the other of said members in accordance with the speed of one of said members and second means adapted to drive said o-ne member by said other member when said first means is inoperative.
References Cited in the le of this patent UNITED STATES PATENTS 1,957,181 Mitchel May 1, 1934 1,980,379 Burnett Nov. 13, 1934 1,987,307 Niven Ian. 8, 1935 2,057,354 Withers et al. Oct. 13, 1936 2,072,474 Helming Mar. 2, 1937 2,121,560 Duncan June 21, 1938 2,159,017 Duncan May 23, 1939 2,162,243 Browne June 13, 1939 2,785,668 Dehmer Mar. 19, 1957 FOREIGN PATENTS 841,286 France Feb. 1, 1939
US627799A 1956-12-12 1956-12-12 Hydraulic timer Expired - Lifetime US2861557A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US627799A US2861557A (en) 1956-12-12 1956-12-12 Hydraulic timer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US627799A US2861557A (en) 1956-12-12 1956-12-12 Hydraulic timer

Publications (1)

Publication Number Publication Date
US2861557A true US2861557A (en) 1958-11-25

Family

ID=24516177

Family Applications (1)

Application Number Title Priority Date Filing Date
US627799A Expired - Lifetime US2861557A (en) 1956-12-12 1956-12-12 Hydraulic timer

Country Status (1)

Country Link
US (1) US2861557A (en)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1113609B (en) * 1958-12-03 1961-09-07 Daimler Benz Ag Injection timing adjusters for internal combustion engines
US3685499A (en) * 1970-09-16 1972-08-22 George B K Meacham Emission control device
US3877222A (en) * 1969-10-17 1975-04-15 Daimler Benz Ag Method for the operation of an internal combustion engine with afterburner chamber and installation for carrying out the method
US4091776A (en) * 1974-04-04 1978-05-30 Rockwell International Corporation Fluid actuated timing mechanism
US4545338A (en) * 1984-12-03 1985-10-08 Stephen E. Lawing Cam shaft timing control device
US5002023A (en) * 1989-10-16 1991-03-26 Borg-Warner Automotive, Inc. Variable camshaft timing for internal combustion engine
US5046460A (en) * 1989-10-16 1991-09-10 Borg-Warner Automotive Transmission & Engine Components Corporation Variable camshaft timing for internal combustion engine
US5117784A (en) * 1991-05-03 1992-06-02 Ford Motor Company Internal combustion engine camshaft phaseshift control system
US5121717A (en) * 1990-11-28 1992-06-16 Ford Motor Company Internal combustion engine camshaft phase shift control system
US5507254A (en) * 1989-01-13 1996-04-16 Melchior; Jean F. Variable phase coupling for the transmission of alternating torques
US5592857A (en) * 1994-02-16 1997-01-14 Unisia Jecs Corporation Variable camshaft phaser
US5645017A (en) * 1989-01-13 1997-07-08 Melchior; Jean Frederic Coupling for the transmission of alternating torques
EP1065348A2 (en) 1999-06-30 2001-01-03 BorgWarner Inc. Variable valve timing with actuator locking for internal combustion engine
US6247434B1 (en) 1999-12-28 2001-06-19 Borgwarner Inc. Multi-position variable camshaft timing system actuated by engine oil
US6263846B1 (en) 1999-12-28 2001-07-24 Borgwarner Inc. Control valve strategy for vane-type variable camshaft timing system
US6311655B1 (en) 2000-01-21 2001-11-06 Borgwarner Inc. Multi-position variable cam timing system having a vane-mounted locking-piston device
US20030196625A1 (en) * 2002-04-19 2003-10-23 Smith Franklin R. Air venting mechanism for variable camshaft timing devices
US6814037B1 (en) 2003-06-24 2004-11-09 Borgwarner Inc. Variable camshaft timing for internal combustion engine with actuator locking
US7228829B1 (en) 2004-10-26 2007-06-12 George Louie Continuously variable valve timing device
EP1985813A2 (en) 2007-04-27 2008-10-29 Schwäbische Hüttenwerke Automotive GmbH & Co. KG Cam shaft phaser and vacuum pump for a combustion engine
US20130042751A1 (en) * 2009-04-16 2013-02-21 Carl Romack Fluid-Actuated Controller Capable of Feedback Regulation
DE102013217017A1 (en) * 2013-08-27 2015-03-05 Schaeffler Technologies Gmbh & Co. Kg Multi-part rotor for a hydraulic camshaft adjuster with oil supply to the pressure chambers through the wings

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1957181A (en) * 1932-02-27 1934-05-01 Edward W Mitchel Automatic valve timing device
US1980379A (en) * 1933-07-19 1934-11-13 Charles S Burnett Valve operating mechanism
US1987307A (en) * 1929-09-23 1935-01-08 Continental Aircraft Engine Co Internal combustion engine
US2057354A (en) * 1935-11-04 1936-10-13 Withers William Harold Internal combustion engine automatic valve control
US2072474A (en) * 1935-04-03 1937-03-02 Vernon P Helming Internal combustion engine
US2121560A (en) * 1935-08-19 1938-06-21 Lewis P Threlkeld Variable timing device
FR841286A (en) * 1937-09-15 1939-05-15 Porsche Kg Internal combustion engine
US2159017A (en) * 1937-08-17 1939-05-23 Lewis P Threlkeld Control mechanism for internal combustion engines
US2162243A (en) * 1935-09-07 1939-06-13 Wright Aeronautical Corp Autoamtic magneto coupling
US2785668A (en) * 1953-11-11 1957-03-19 Fur Unternehmungen Der Eisen U Convertible internal combustion engine and compressor

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1987307A (en) * 1929-09-23 1935-01-08 Continental Aircraft Engine Co Internal combustion engine
US1957181A (en) * 1932-02-27 1934-05-01 Edward W Mitchel Automatic valve timing device
US1980379A (en) * 1933-07-19 1934-11-13 Charles S Burnett Valve operating mechanism
US2072474A (en) * 1935-04-03 1937-03-02 Vernon P Helming Internal combustion engine
US2121560A (en) * 1935-08-19 1938-06-21 Lewis P Threlkeld Variable timing device
US2162243A (en) * 1935-09-07 1939-06-13 Wright Aeronautical Corp Autoamtic magneto coupling
US2057354A (en) * 1935-11-04 1936-10-13 Withers William Harold Internal combustion engine automatic valve control
US2159017A (en) * 1937-08-17 1939-05-23 Lewis P Threlkeld Control mechanism for internal combustion engines
FR841286A (en) * 1937-09-15 1939-05-15 Porsche Kg Internal combustion engine
US2785668A (en) * 1953-11-11 1957-03-19 Fur Unternehmungen Der Eisen U Convertible internal combustion engine and compressor

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1113609B (en) * 1958-12-03 1961-09-07 Daimler Benz Ag Injection timing adjusters for internal combustion engines
US3877222A (en) * 1969-10-17 1975-04-15 Daimler Benz Ag Method for the operation of an internal combustion engine with afterburner chamber and installation for carrying out the method
US3685499A (en) * 1970-09-16 1972-08-22 George B K Meacham Emission control device
US4091776A (en) * 1974-04-04 1978-05-30 Rockwell International Corporation Fluid actuated timing mechanism
US4545338A (en) * 1984-12-03 1985-10-08 Stephen E. Lawing Cam shaft timing control device
US5649506A (en) * 1989-01-13 1997-07-22 Melchior; Jean Frederic Coupling for the transmission of alternating torques
US5507254A (en) * 1989-01-13 1996-04-16 Melchior; Jean F. Variable phase coupling for the transmission of alternating torques
US5645017A (en) * 1989-01-13 1997-07-08 Melchior; Jean Frederic Coupling for the transmission of alternating torques
US5046460A (en) * 1989-10-16 1991-09-10 Borg-Warner Automotive Transmission & Engine Components Corporation Variable camshaft timing for internal combustion engine
US5002023A (en) * 1989-10-16 1991-03-26 Borg-Warner Automotive, Inc. Variable camshaft timing for internal combustion engine
US5121717A (en) * 1990-11-28 1992-06-16 Ford Motor Company Internal combustion engine camshaft phase shift control system
US5117784A (en) * 1991-05-03 1992-06-02 Ford Motor Company Internal combustion engine camshaft phaseshift control system
US5592857A (en) * 1994-02-16 1997-01-14 Unisia Jecs Corporation Variable camshaft phaser
US6382155B2 (en) 1999-06-30 2002-05-07 Borgwarner Inc. Variable valve timing with actuator locking for internal combustion engine
EP1065348A2 (en) 1999-06-30 2001-01-03 BorgWarner Inc. Variable valve timing with actuator locking for internal combustion engine
US6250265B1 (en) 1999-06-30 2001-06-26 Borgwarner Inc. Variable valve timing with actuator locking for internal combustion engine
US6247434B1 (en) 1999-12-28 2001-06-19 Borgwarner Inc. Multi-position variable camshaft timing system actuated by engine oil
US6374787B2 (en) * 1999-12-28 2002-04-23 Borgwarner Inc. Multi-position variable camshaft timing system actuated by engine oil pressure
US6263846B1 (en) 1999-12-28 2001-07-24 Borgwarner Inc. Control valve strategy for vane-type variable camshaft timing system
US6311655B1 (en) 2000-01-21 2001-11-06 Borgwarner Inc. Multi-position variable cam timing system having a vane-mounted locking-piston device
US20030196625A1 (en) * 2002-04-19 2003-10-23 Smith Franklin R. Air venting mechanism for variable camshaft timing devices
US6745735B2 (en) * 2002-04-19 2004-06-08 Borgwarner Inc. Air venting mechanism for variable camshaft timing devices
US6814037B1 (en) 2003-06-24 2004-11-09 Borgwarner Inc. Variable camshaft timing for internal combustion engine with actuator locking
US7228829B1 (en) 2004-10-26 2007-06-12 George Louie Continuously variable valve timing device
EP1985813A2 (en) 2007-04-27 2008-10-29 Schwäbische Hüttenwerke Automotive GmbH & Co. KG Cam shaft phaser and vacuum pump for a combustion engine
DE102007020431A1 (en) 2007-04-27 2008-10-30 Schwäbische Hüttenwerke Automotive GmbH & Co. KG Camshaft phaser and vacuum pump for an internal combustion engine
US20130042751A1 (en) * 2009-04-16 2013-02-21 Carl Romack Fluid-Actuated Controller Capable of Feedback Regulation
DE102013217017A1 (en) * 2013-08-27 2015-03-05 Schaeffler Technologies Gmbh & Co. Kg Multi-part rotor for a hydraulic camshaft adjuster with oil supply to the pressure chambers through the wings
US10174644B2 (en) 2013-08-27 2019-01-08 Schaeffler Technologies AG & Co. KG Multipart rotor for a hydraulic camshaft adjuster with a supply of oil to the pressure chambers through the vanes

Similar Documents

Publication Publication Date Title
US2861557A (en) Hydraulic timer
US5107804A (en) Variable camshaft timing for internal combustion engine
US5046460A (en) Variable camshaft timing for internal combustion engine
US5002023A (en) Variable camshaft timing for internal combustion engine
US4131096A (en) Valve timing mechanisms
US3516394A (en) Device for simultaneously advancing intake cam lobes and retarding exhaust cam lobes of an internal combustion engine while the engine is running
US5361736A (en) Variable valve timing
US3144009A (en) Variable valve timing mechanism
US4502426A (en) Variable valve lift and timing mechanism
US3294071A (en) Internal combustion rotary piston engine
US3258937A (en) Automatic hydraulic engine timing device
US5253622A (en) Cam phase change mechanism
US2969051A (en) Variable cam timing mechanism
US3109417A (en) Engine timing and balancing mechanism
CA1153943A (en) Phase controlling system for two rotatable shafts
US4389985A (en) Apparatus for establishing and terminating connections between crankshafts
US2159017A (en) Control mechanism for internal combustion engines
US5343834A (en) Device for adjusting the rotational angle relationship between a camshaft and its drive element
US3638624A (en) Engine valve control means
WO2008042622A1 (en) Variable event duration reduction (vedr) cam phaser
US2121560A (en) Variable timing device
US5179918A (en) Timing-range gear
US2977778A (en) Automatic timing device for engines
US2162243A (en) Autoamtic magneto coupling
US1798185A (en) Automatic poppet-valve control