Camshaft Having a Decompression Device
20170292417 ยท 2017-10-12
Inventors
Cpc classification
F01L2810/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L13/085
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01L13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A camshaft has a decompression device for an internal combustion engine, wherein a valve lifter is rotatably supported in a base circle of a cam, which can be brought into operative connection with a gas exchange valve via rotation. The valve lifter is operatively connected to a centrifugal fly weight, which is arranged coaxially to the camshaft and which is rotatably supported, in such a way that the valve lifter forms a contour of the base circle in the region of action with the gas exchange valve from a certain rotational speed of the camshaft. The camshaft has a cavity in the region of the centrifugal fly weight, to which cavity lubricant pressure can be applied. A radial first bore from the cavity to the centrifugal fly weight is arranged in the camshaft. A slideable element that can be displaced by the lubricant pressure is arranged in the first bore. By way of the design of the camshaft, an unstable centrifugal fly weight is stabilized and thus acoustics are improved.
Claims
1. A camshaft having a decompression device for an internal combustion engine, comprising: a cam of the camshaft which is operationally connectable with a gas exchange valve through rotation, the cam having a base circle; a valve lifter rotatably mounted in the base circle of the cam; a rotatably mounted flyweight arranged coaxially with the camshaft, the valve lifter being operationally connected with the rotatably mounted flyweight such that the valve lifter, from a certain rotational speed of the camshaft, forms a contour of the base circle in an operational region with the gas exchange valve, wherein the camshaft in a region of the flyweight comprises a cavity to which lubricant pressure is applied, a first radial bore is arranged in the camshaft from the cavity to the flyweight, and in the first radial bore, a slideable element is arranged, the slideable element being displaceable via the lubricant pressure.
2. The camshaft according to claim 1, wherein lubricant is applied to the cavity via a second bore from a bearing region of the camshaft.
3. The camshaft according to claim 2, wherein the slideable element is displaceable by the lubricant in a direction of the flyweight against a spring force of a spring element.
4. The camshaft according to claim 1, wherein the slideable element is displaceable by the lubricant in a direction of the flyweight against a spring force of a spring element.
5. The camshaft according to claim 3, wherein the flyweight comprises a stop for the slideable element.
6. The camshaft according to claim 1, wherein the flyweight comprises a stop for the slideable element.
7. The camshaft according to claim 5, wherein the slideable element is a needle roller.
8. The camshaft according to claim 1, wherein the slideable element is a needle roller.
9. The camshaft according to claim 7, wherein the camshaft is an exhaust camshaft.
10. The camshaft according to claim 1, wherein the camshaft is an exhaust camshaft.
11. An internal combustion engine, comprising a camshaft according to claim 1.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0017]
[0018]
[0019]
[0020] In the following, the same reference numbers apply to identical components in the
DETAILED DESCRIPTION OF THE DRAWINGS
[0021]
[0022] In a base circle 2 of a cam 3, a valve lifter 4 is rotatably mounted, which is operationally connected with a rotatably mounted flyweight 5 that is arranged coaxially with the camshaft 1 such that the valve lifter 4 from a certain rotational speed of the camshaft 1, is turned by the flyweight 5 in such a manner that the valve lifter 4 constitutes a contour of the base circle 2. This means that from a certain rotational speed of the camshaft 1 the valve lifter 4 is quasi ineffective, and the gas exchange valve remains closed as usual.
[0023] During the starting of the internal combustion engine, or at a rotational speed that is less than the defined rotational speed, the flyweight, as is evident in
[0024] The camshaft 1 with the decompression device according to the invention is characterized in that the camshaft 1 in the region of the flyweight 5 has a cavity 6 (
[0025] In the present exemplary embodiment, the cams 3 each have a recess 12 for weight saving.
[0026]
[0027] Through the slideably arranged element 8, a section A-A in
[0028]
[0029] In the stationary state of the camshaft 1, the spring element 10, via a pressure element 13, pushes the flyweight 5 about the axis of rotation 14 with the stop 11 onto the slideable element 8. On the side facing away from the spring element 10, the flyweight 5 is operationally connected to the valve lifter 4. In the position shown in
[0030] When the internal combustion engine is now started, a lubricant pressure builds up in the cavity 6 while the flyweight 5 at the same time turns radially to the outside with a support of the lubricant pressure which pushes the slideable element 8 likewise radially to the outside. In the process, the flyweight 5 turns according to the arrow in clockwise direction and turns the valve lifter 4 in such a manner that it assumes the same contour in the base circle 2 as the base circle 2 itself. A decompression is thus securely avoided from a defined rotational speed.
[0031] As shown in
[0032] In other words, the slideable element 8 installed in the camshaft 1 is supplied with lubricant from the lubricant circuit. As soon as the internal combustion engine fires, the slideable element 8, preferably a needle roller, is radially displaced to the outside by the lubricant pressure that builds up in the cavity 6. As soon as the internal combustion engine fires, the slideable element 8 is displaced to the outside by centrifugal force. At the same time, the slideable element 8 is supported by lubricant pressure in the cavity 6 and remains in the desired radially outer position. In the process, the flyweight 5 is held stable in the deflection position and can no longer cause the acoustic abnormality. In the manner of the invention, this means no clicking of the decompression device and thus no unpleasant noises of the internal combustion engine.
List of Reference Numbers
[0033] 1 Camshaft [0034] 2 Base circle [0035] 3 Cam [0036] 4 Valve lifter [0037] 5 Flyweight [0038] 6 Cavity [0039] 7 First bore [0040] 8 Element [0041] 9 Bearing region [0042] 10 Spring element [0043] 11 Stop [0044] 12 Recess [0045] 13 Pressure body [0046] 14 Axis of rotation [0047] 15 Second bore
[0048] The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.