The invention relates to a method for measuring the light tightness of a piston ring that is provided with a joint and created so as to be non-round.
DD 148 982 B1 discloses a measuring system for determining impermissible gaps between rotation-symmetrical components, in particular for checking the sealing gaps of piston rings, using a light source and a photoreceiver. The piston ring to be checked is clamped into a ring gauge, and the optical axis of a pulsed light source is directed at the gap between the piston ring and the ring gauge by means of an interposed lens system, wherein a test receiver is disposed opposite the gap in the optical axis, the analog electrical signal of the test receiver, which is dependent on the gap width, being supplied to a selective amplifier, wherein it is possible, by means of a known electronic circuit, to retrieve, store and display the analog electrical signals that are detected over the course of a rotation of the ring gauge based on the circumference.
A method for ascertaining the shape-conforming capability of piston rings in a non-round cylinder liner became known from DE 100 30 368 A1. For this purpose, a dimensionally stable test liner is provided and accommodated in a shape testing device. The inner surface of the test liner is provided with an exactly circular cylindrical section corresponding to the nominal diameter of the piston ring and, axially adjoining, with a slight non-round section having four curved convexities of approximately 20 μm. The cross-sectional surface enclosed by an inscribable circle and by the convexities is used as a reference surface. The profile progression of the inner surface of the piston ring over the non-round section circumference is ascertained by way of conventional shape measurement of the piston ring that is inserted in the non-round test liner.
When piston rings are produced, high manufacturing capability must be available to maintain the light tightness under operation, which is associated with significant costs. Even piston rings that are produced at a high manufacturing level must be subjected to a light tightness check at least occasionally, so as to establish in this way to what degree impermissible tolerances have arisen in the manufacturing process.
It is the object of the invention to provide a method which makes it possible to check whether a piston ring is still suited for operation or must be regarded as scrap, even when larger manufacturing tolerances are accepted in the production of piston rings. Moreover, a device that operates according to the method and has a simple design is to be provided.
This object is achieved by a method for measuring the light tightness of a piston ring that is provided with a joint and produced so as to be non-round by clamping the open piston ring, while substantially closing the gap, by means of an accessory device in the circumferential direction, and by exerting a defined force in the region of at least one of the joint ends of the piston ring in the direction of a wall of the accessory device, wherein optical means are used to establish whether the joint region of the piston ring which is subjected to the action of the force is seated against the wall of the accessory device in a light-tight manner.
A device operating according to this method is characterized in that the accessory device is a control ring surrounding the piston ring, wherein a roller, which can be fed at least in the direction of the control ring, is positioned radially inside the control ring.
An alternative device operating according to this method is characterized in that the accessory device is a control ring surrounding the piston ring, and that a rigid body, comprising two pressure elements that are directed at the joint ends, can be fed radially in the direction of the joint ends within the control ring.
As a result of the method according to the invention and the alternative devices operating according to the same, it is now possible to establish whether a piston ring that is produced with larger tolerances is nonetheless sufficiently light-tight so as to still be suitable for the operating condition in an engine.
The action of the force on the particular joint end advantageously takes place radially from the inside.
According to a further idea of the invention, the respective joint region is pressed against the wall of the accessory device, which in particular is designed as a control ring, using a force between 0.5 and 50 N.
The amount of the force here is dependent on the diameter, the material of the piston ring and the radial wall thickness of the piston ring to be measured.
If needed, the method according to the invention can be integrated into the light gap testing process of pistons that is subsequently carried out anyhow, without any major complexity.
From a technical point of view, several embodiments for testing the light tightness of a piston ring exist, which are described hereafter:
The person skilled in the art will make the solution that has the simplest design and is also the most economical one available, depending on the application.
By analogy to the prior art according to DD 148 982 B2, with the method according to the invention, it is also possible to provide an optical source at approximately 90° with respect to the clamped piston ring, the source being operatively connected to a photoreceiver device.
The subject matter of the invention is shown in the drawings based on an exempla y embodiment and is described as follows.
In the drawings:
An optical monitoring system is used, which scans at least one defined circumferential section of at least one of the joint ends in relation to the surrounding wall of the control ring.
Number | Date | Country | Kind |
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10 2012 000 332 | Jan 2012 | DE | national |
Filing Document | Filing Date | Country | Kind |
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PCT/DE2012/001171 | 12/6/2012 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2013/104348 | 7/18/2013 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2433558 | Hurley, Jr. | Dec 1947 | A |
2441343 | Becker | May 1948 | A |
2487628 | Aller | Nov 1949 | A |
2487629 | Aller | Nov 1949 | A |
2558226 | Sparrow | Jun 1951 | A |
5380018 | Mader | Jan 1995 | A |
7096553 | Carruth | Aug 2006 | B1 |
8979094 | Esser | Mar 2015 | B2 |
9133933 | Feistel | Sep 2015 | B1 |
Number | Date | Country |
---|---|---|
201348498 | Nov 2009 | CN |
148 982 | Jul 1986 | DE |
100 30 368 | Jan 2002 | DE |
1 504 974 | Mar 1978 | GB |
Number | Date | Country | |
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20150122045 A1 | May 2015 | US |