Turning – Process of turning
Reexamination Certificate
2000-09-18
2002-03-19
Tsai, Henry (Department: 3722)
Turning
Process of turning
C082S046000, C407S024000
Reexamination Certificate
active
06357325
ABSTRACT:
TECHNICAL AREA
The invention relates to a sealing arrangement providing a rotationally induced return flow effect by utilizing a groove with respect to a sealing surface, and a method for manufacturing the surfaces to be sealed.
BACKGROUND OF THE INVENTION
A sealing arrangement of this type and a method are disclosed in German Published Unexamined Application DE-OS 15 433. To achieve a rotationally induced return flow effect, provision is made for a shaft having grooves applied at an angle with respect to the longitudinal axis. The return flow effect, after a short period of operation, is eliminated at the place where the radial shaft sealing ring exerts the greatest pressure, due to the deformation and the wear associated therewith, so that the sealing ring cannot be subject to any further wear at all. In the immediate vicinity of this now eliminated return flow effect, the existing grooves continue to exhibit a return-flow effect, as before. The document indicates that a return-flow thread would destroy the sealing edge of the radial shaft sealing ring.
The grooves are produced by a simple plunge-cutting (gashing) procedure, as for example, by means of rotating grinding disks or using a polishing disk furnished with abrasive powder. In grinding the surfaces, a disadvantage lies in the unpredictable nature of the outcome, i.e., whether the sealing arrangement will provide an adequate sealing action during normal use. The ground surface has an unpredictable number of spiral-shaped, multi-thread grooves of various depths. The number and form of the threads continuously changes in unpredictable ways during the manufacturing of the surface, depending on the condition of the grinding disk, the vibration response of the drive shaft of the grinding disk, the vibration response of the drive shaft of the grinding disk, and/or of the surface to be ground, and the spacial relationship of the rotating axes with respect to each other. Given the typically randomly developed form of the multi-thread grooves on the surface, the volume of the medium to be sealed within the grooves may be so great that the radial shaft sealing ring is no longer able to convey the medium to be sealed back into the space to be sealed off.
SUMMARY OF THE INVENTION
The invention is based on the object of further refining a sealing arrangement of the type described above, such that the spiral grooving that gives rise to the return flow effect can be more reliably manufactured. Consequently, the surface properties, including the dimensions of the groove, can be measured on the surface with metrological means and suitably quantified. This permits clear, quantifiable associations to be formed between the geometry of the groove and the resulting sealing effects that the arrangement provides to the radial shaft sealing ring. The surface should be so constituted that the radial shaft sealing ring can, regardless of the direction of rotation of the machine element, return the volumes of fluid necessary for lubricating the sealing edge into the space to be sealed.
In brief, the invention provides a sealing arrangement, in which a rotationally symmetrical machine element having a surface against which a seal is established to be machine cut to produce a groove, the groove having a rounded groove bottom that is recessed into the surface. The groove bottom has a radius of curvature of 0.4 to 1.6 mm, and a depth of less than 15 &mgr;m. The radial shaft sealing ring has a polymeric sealing lip which contacts the surface of the machine element that bears the groove via a sealing edge that is formed by two intersecting conical surfaces, the first conical surface, facing in the direction of a space to be sealed off, having a steeper conical angle with respect to the axis of rotation of the machine element than the conical surface facing away therefrom. The width of sealing ring along which the seal is established is 1.5 to 4 times greater than the pitch of the groove.
In the invention, as noted, provision is made for a spiral-shaped groove having a rounded groove bottom to be machine-cut into the surface, and for the groove bottom to have a radius of curvature of 0.4 to 1.6 mm, and for the depth of the groove to be less than 15 &mgr;m. In contrast to ground surfaces, machine-cut surfaces are substantially less expensive to manufacture. Moreover, the return flow effect produced on the surface in the machine-cutting process has the advantage that it can be measured by metrological means, and quantified in terms of its effects on the sealing action of the radial shaft sealing rings. Therefore, it is possible to check, simply and cost-effectively, whether the machine-cut surface has been manufactured according to specifications, and whether the required parameters have been complied with. Depending on the direction of rotation, the machine-cut surf ace conveys the medium to be sealed off more or less vigorously along the surface in the axial direction. With a radius of curvature of 0.4 to 1.6 mm and a groove depth of less than 15 &mgr;m, the radial shaft sealing ring is able, regardless of the turning direction of the machine element, to return the volume s of medium to be sealed off needed for lubricating the sealing edge, into the space to be sealed. The reverse-flow effect of the radial shaft sealing ring is conditioned upon the two conical surfaces, the first conical surface, facing the space to be sealed off, forming a steeper cone angle with the axis of rotation than the second conical surface, facing away therefrom.
The groove depth is preferably no greater than 10 &mgr;m. As a result of the lesser groove depth, the wear that occurs during the course of operation at the sealing edge of the radial shaft sealing ring is reduced, so that the sealing arrangement of the present invention exhibits further improved working properties over a longer service life.
The adjacent groove spirals preferably are spaced apart at their midpoints by 0.03 to 0.3 mm. At mid point clearances of up to 0.3 mm, the delivery, conditional upon the rotationally induced return flow of the medium to be sealed off, out of the space to be sealed off, regardless of the direction of rotation of the machine element, is in any case so slight that reliable sealing action is assured by the radial shaft sealing ring. Midpoint distances of less than 0.03 mm are hardly practicable, since such a surface requires a comparatively long machining time, and it becomes clearly more difficult to measure the mechanical dimensions giving rise to the return flow effect using metrological means.
To achieve good working characteristics over a long service life, provision is made that the width of the sealing edge of the seal employed 1.5 be 4 times greater than the pitch of the groove.
The machine element can be constituted by a shaft or the barrel ring (or race) of a cassette seal.
The invention relates, moreover, to a method for manufacturing a sealing-arrangement surface to be sealed off. To achieve this object, machine-cutting takes place across the surface with a feed rate of 0.03 to 0.3 mm, a cutting speed of 80 to 400 m/min., and a cutting depth of 0.04 to 0.4 mm. Using such a method, one attains a mean roughness value R
a
, according to German Industrial standard DIN 4762, of 0.05 to 2 &mgr;m. The mean roughness value R, is the arithmetic mean of all profile values of the roughness profile. In addition, a peak-to-valley height R
z
of 0.2 to 10 &mgr;m, according to German Industrialstandard DIN 4768, is achieved. The mean peak-to-valley height R
z
is the mean value of the individual peak-to-valley heights of successive, individual measured distances.
The maximal peak-to-valley height R
max
, according to DIN 4768, is the largest individual peak-to-valley height within the entire measured distance and, in the above described method, amounts to a maximum of 15 &mgr;m.
REFERENCES:
patent: 2301100 (1942-11-01), Voss
patent: 4138927 (1979-02-01), Hamil
patent: 5775187 (1998-07-01), Nickolai et al.
patent: 5910199 (1999-06-01), Busick et al.
patent: 6170834 (2001-01-01), Vog
Firma Carl Freudenberg
Tsai Henry
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