U.S. patent application number 12/086797 was filed with the patent office on 2009-07-02 for piston for an internal combustion engine and method for its production.
Invention is credited to Klaus Keller, Peter Kemnitz.
Application Number | 20090165743 12/086797 |
Document ID | / |
Family ID | 37904010 |
Filed Date | 2009-07-02 |
United States Patent
Application |
20090165743 |
Kind Code |
A1 |
Kemnitz; Peter ; et
al. |
July 2, 2009 |
Piston for an Internal Combustion Engine and Method for Its
Production
Abstract
The present invention relates to a piston (10) for an internal
combustion engine, having at least two hub bores (18) for holding a
piston pin, wherein the hub bores (18) have at least one geometric
deviation from a cylindrical inner contour. It is provided
according to the invention that the hub bores (18) are formed from
bores (21) with a cylindrical inner contour, that the bores (21)
are provided with a coating (22) comprising a resin with solid
lubricant particles embedded therein, and that the coating (22)
forms the at least one geometric deviation from the cylindrical
inner contour of the hub bores (18). The present invention also
relates to a method for producing a piston of the type, in which
method bores (21) with a cylindrical inner contour are initially
produced, and a coating medium comprising a resin with solid
lubricant particles embedded therein is subsequently applied to the
inner faces of said bores (21) by means of a coating tool (30),
such that the resulting coating (22) forms the at least one
geometric deviation from the cylindrical inner contour of the hub
bores (18).
Inventors: |
Kemnitz; Peter; (Leutenbach,
DE) ; Keller; Klaus; (Lorch, DE) |
Correspondence
Address: |
COLLARD & ROE, P.C.
1077 NORTHERN BOULEVARD
ROSLYN
NY
11576
US
|
Family ID: |
37904010 |
Appl. No.: |
12/086797 |
Filed: |
December 15, 2006 |
PCT Filed: |
December 15, 2006 |
PCT NO: |
PCT/DE2006/002257 |
371 Date: |
June 19, 2008 |
Current U.S.
Class: |
123/193.6 ;
29/888.04; 92/187 |
Current CPC
Class: |
F02F 3/00 20130101; F16J
1/16 20130101; F16C 33/201 20130101; F05C 2251/14 20130101; F05C
2253/20 20130101; Y10T 29/49249 20150115 |
Class at
Publication: |
123/193.6 ;
92/187; 29/888.04 |
International
Class: |
F02F 3/10 20060101
F02F003/10; F16J 1/16 20060101 F16J001/16; B23P 15/10 20060101
B23P015/10 |
Foreign Application Data
Date |
Code |
Application Number |
Dec 21, 2005 |
DE |
10 2005 061 063.3 |
Claims
1: Piston (10) for an internal combustion engine, having at least
two pin bores (18) for accommodating a piston pin, whereby the pin
bores (18) have at least one geometric deviation from a cylindrical
inside contour, wherein the pin bores (18) are formed from bores
(21) having a cylindrical inside contour, that the bores (21) are
provided with a coating (22) comprising a resin with solid
lubricant particles embedded in it, and that the coating (22) forms
the at least one geometric deviation from the cylindrical inside
contour of the pin bores (18).
2: Piston according to claim 1, wherein the at least one geometric
deviation is configured as at least one stress relief pocket and/or
ovality and/or as a shaped bore.
3: Piston according to claim 1, wherein at least one oil collection
chamber (24, 25) is provided in the coating (22).
4: Piston according to claim 3, wherein the at least one oil
collection chamber is configured as a channel (24) that runs in the
pin boss axis direction.
5: Piston according to claim 3, wherein the at least one oil
collection chamber is configured as a channel that runs radially
relative to the pin boss axis direction, surrounding it entirely or
in part.
6: Piston according to claim 3, wherein the at least one oil
collection chamber is configured as a pocket-shaped recess.
7: Piston according to claim 1, wherein the minimum thickness of
the coating (22) amounts to 5 .mu.m to 20 .mu.m.
8: Piston according to claim 1, wherein the resin is a thermally
cured resin, particularly a polyamide imide resin.
9: Piston according to claim 1, wherein the coating (22) contains
50 wt.-% to 60 wt.-% solid lubricant particles.
10: Piston according to claim 1, wherein the solid lubricant
particles consist of a material that is selected from the materials
group that comprises graphite, molybdenum sulfide, tungsten
disulfide, hexagonal boron nitride, and PTFE
(polytetrafluoroethylene).
11: Piston according to claim 1, wherein the solid lubricant
particles have a particle size of 1 .mu.m to 3 .mu.m.
12: Method for the production of a piston (10) for an internal
combustion engine, having at least two pin bores (18) for
accommodating a piston pin, whereby the pin bores (18) have at
least one geometric deviation from a cylindrical inside contour,
wherein first, bores (21) having a cylindrical inside contour are
produced, and subsequently, a coating agent comprising a resin with
solid lubricant particles embedded in it is applied to the inside
surfaces of these bores (21), by means of a coating tool (30), so
that the resulting coating (22) forms the at least one geometric
deviation from the cylindrical inside contour of the pin bores
(18).
13: Method according to claim 12, wherein the at least one
geometric deviation is configured by means of varying the amount of
the coating agent given off by the coating tool (30) and/or by
means of varying the advance of the coating tool (30).
14: Method according to claim 12, wherein the coating agent is
applied to inside surfaces of the bores (21) with a surface
roughness of Ra (average roughness value).ltoreq.0.8 .mu.m.
15: Method according to claim 12, wherein the coating agent is
applied by means of rotation atomization from a rotating nozzle
(34) introduced into the bore (21).
16: Method according to claim 15, wherein the rotation atomization
is carried out at a rotation speed of the nozzle of 14,000 to
18,000 rotations per minute.
17: Method according to claim 12, wherein the inside surfaces of
the bores (21) are pre-heated before and/or during application of
the coating agent, preferably up to a temperature of 50.degree. C.
to 80.degree. C.
18: Method according to claim 12, wherein a thermally curing
coating agent is used, which is subjected to heat treatment
immediately after completing the application, preferably at a
temperature of 200.degree. C.
Description
[0001] The invention relates to a piston for an internal combustion
engine and to a method for its production.
[0002] The piston pin connects the piston with the crankshaft of
the internal combustion engine by way of a connecting rod. The
piston pin is mounted in pin bores made in pin bosses, and can bend
as a result of the tremendous forces that act on the piston during
the oscillating movement of the piston. The pin bosses are among
the parts of a piston that are subject to the greatest stress.
Under great piston stresses, there is the risk of crack formation
at the pin bores. Therefore, ways are being sought to relieve
stress on the pin bores, particularly in light-metal pistons. This
is done, for example, by means of local geometric changes in the
usually cylindrical pin bore, which reduce the stress triggered by
the deformation of the piston pin. Such geometric changes can be,
for example, stress relief pockets, oval pin bores, or conical or
spherical bores adapted to the bending line of the piston pin (with
regard to the latter see, for example, WO 96/07841 A1). Such
geometric changes have been produced by means of complicated
precision machining of the pin bore until now.
[0003] Pistons having pin bores with slide bearing surfaces are
known from the German patent application 10 2004 059 392.9. The
slide bearing surfaces are coated with a self-lubricating coating
made of a resin with solid lubricant particles embedded in it.
[0004] It is the task of the present invention to make available a
piston whose pin bores can be provided with local geometric
deviations in particularly simple manner.
[0005] The solution consists in a piston having the characteristics
of claim 1 and a method having the characteristics of claim 12.
According to the invention, it is provided that the pin bores are
formed from bores having a cylindrical inside contour, that the
bores are provided with a coating comprising a resin with solid
lubricant particles embedded in it, and that the coating forms the
at least one geometric deviation from the cylindrical inside
contour of the pin bores. The method according to the invention is
characterized in that first, bores having a cylindrical inside
contour are produced, and subsequently, a coating agent comprising
a resin with solid lubricant particles embedded in it is applied to
the inside surfaces of this bore, by means of a coating tool, so
that the resulting coating forms the at least one geometric
deviation from the cylindrical inside contour of the pin bores.
[0006] With the present invention, it is possible to produce pin
bores having at least one geometric deviation from the cylindrical
inside contour, and having a self-lubricating coating of their
inside surfaces, in one and the same work step. This means a
significant saving in time and costs. The complicated and very
complex cutting machining of the metallic inside surfaces of the
pin bores for the purpose of introducing a geometric deviation is
eliminated. Furthermore, bearing bushings are no longer necessary
to achieve sufficient lubrication and an anti-seizure effect of the
pin bores. The desired dimensional accuracy of the pin bores is
reliably achieved. The strength and therefore the useful lifetime
of the piston pin bearing are significantly improved, as a result
of the improved lubrication properties as compared with the
previously known coatings made of metal alloys.
[0007] Advantageous further developments are evident from the
dependent claims.
[0008] The at least one geometric deviation can be configured as at
least one stress-relief pocket and/or ovality (for example as a
heightwise or crosswise ovality) and/or as a shaped bore, as it is
disclosed in WO 96/07841 A1, for example.
[0009] In advantageous manner, at least one oil collection chamber
can be provided in the coating, in order to further improve the
lubrication of the piston pin bearing. The at least one oil
collection chamber can be configured as a channel that runs in the
pin boss axis direction, as a channel that runs radially with
regard to the pin boss axis direction, surrounding it entirely or
in part, and/or as a pocket-shaped recess.
[0010] The minimum thickness of the coating depends on the
requirements of the individual case and can amount to 5 .mu.m to 15
.mu.m, for example.
[0011] Preferably, the resin contained in the coating is a
thermally cured resin, particularly a polyamide resin, which is
very temperature-resistant and can withstand the stresses that the
piston pin bearing is subject to in operation particularly
well.
[0012] It has been shown that a proportion of 50 wt.-% to 60 wt.-%
of solid lubricant particles in the coating has particularly good
lubrication properties. In this connection, the solid lubricant
particles can particularly consist of a material that is selected
from the materials group that comprises graphite, molybdenum
sulfide, tungsten disulfide, hexagonal boron nitride, and PTFE
(polytetrafluoroethylene). In this connection, it is advantageous
if the solid lubricant particles consist of only one material. In
this connection, it is particularly advantageous if all the solid
lubricant particles consist of the same material, or if solid
lubricant particles that consist of two different materials are
mixed, for example solid lubricant particles of graphite with solid
lubricant particles of a metal sulfide. For particularly effective
lubrication, the solid lubricant particles have a particle size of
1 .mu.m to 3 .mu.m.
[0013] In the case of the method according to the invention, the at
least one geometric deviation can be configured by means of varying
the amount of the coating agent given off by the coating tool
and/or by means of varying the advance of the coating tool in the
bore to be coated.
[0014] A possible alternative, of course, consists in applying the
coating agent in a uniform thickness and configuring the at least
one geometric deviation by means of subsequent working of the
resulting coating. Of course, this is significantly more
complicated than making the at least one geometric deviation
directly during the coating process. However, the result, namely a
piston having pin bores whose coating forms the at least one
geometric deviation from the cylindrical inside contour of the pin
bores, is the same.
[0015] Method according to one of claims 12 to 14, characterized in
that the coating agent is applied to inside surfaces of the bores
with a surface roughness of Ra (average roughness value).ltoreq.0.8
.mu.m.
[0016] Method according to one of claims 12 to 15, characterized in
that the coating agent is applied by means of rotation atomization
from a rotating nozzle introduced into the bore.
[0017] Method according to claim 16, characterized in that the
rotation atomization is carried out at a rotation speed of the
nozzle of 14,000 to 18,000 rotations per minute.
[0018] In order to further improve the adhesion of the coating
agent to the inside surface of the bore, the inside surfaces of the
bores can be pre-heated before and/or during application of the
coating agent, preferably up to a temperature of 50.degree. C. to
80.degree. C.
[0019] A preferred further development of the method according to
the invention consists in using a thermally curing coating agent
and subjecting the same to heat treatment immediately after
completing the application, preferably at a temperature of
200.degree. C.
[0020] An exemplary embodiment of the invention will be described
in greater detail below, using the attached drawings. These show,
in a representation not to scale:
[0021] FIG. 1 a representation, partly in section, of an embodiment
of a piston according to the invention;
[0022] FIG. 2 a partial representation of the pin bore of the
piston according to FIG. 1, in section;
[0023] FIG. 3 a view of the pin bore according to FIG. 2 in the
direction of the arrow A in FIG. 2;
[0024] FIG. 4 a schematic representation of a coating tool.
[0025] FIG. 1 shows an exemplary embodiment of a piston 10
according to the invention, which is a one-part piston 10 in this
case. The piston 10 consists, in known manner, of a light-metal
alloy, for example. The piston 10 has a piston head 11 having a
combustion bowl 12 and a ring-shaped circumferential side wall
having a top land 13 and a ring belt 14 for accommodating piston
rings (not shown). The piston 10 has a piston skirt 15 further
below the piston head 11. The piston skirt 15 has two pin boss
connections 16 that support themselves on the underside of the
piston head 11, which make a transition into two piston pin bosses
17. Each piston pin boss is provided with a pin bore 18 equipped
with a locking ring groove 19 for a piston ring (not shown).
Depending on the construction of the piston (two-part or
multi-part), of course, more than two piston pin bosses with
corresponding pin bores can be provided.
[0026] In the exemplary embodiment, the pin bores 18 are shaped
bores having a defined inside contour 23 that deviates from the
cylinder shape, as they are disclosed, for example, in WO 96/07841
A1. This configuration serves to relieve stress on the piston pin
during operation, in order to avoid the risk of pin boss cracks.
Other configurations of a pin bore that serve the same purpose are,
for example, pin bores provided with ovality (heightwise and/or
crosswise) or with stress relief pockets (not shown). These
configurations are known.
[0027] The pin bores 18 are configured, according to the invention,
in such a manner that they are composed of a cylindrical bore 21
and a coating 22. In this connection, the surface contour of the
coating 22 is structured in such a manner that the desired inside
contour 23 of the shaped bore, which deviates from the cylinder
shape, is obtained. In comparable manner, ovality or a stress
relief pocket can also be formed by the surface structure of the
coating 22 (not shown). The coating 22 essentially consists of a
resin with solid lubricant particles embedded in it, and is thus a
self-lubricating coating.
[0028] In the exemplary embodiment, the coating is furthermore
provided with oil collection chambers in the form of a channel 24
that extends in the direction of the pin boss axis, from which
pockets 25 extend radially. These oil collection chambers serve to
further improve the lubrication of the piston pin bearing. Of
course, they can be configured for any desired application, in any
desired shape and size, and can be disposed relative to one another
in any desired form.
[0029] To produce a pin bore 18, first the cylindrical bore 21 is
made in the piston pin boss 17, and mechanically finished in known
manner. The surface roughness Ra (average roughness value) can
correspond to the one indicated in DE 41 11 368 A1, whereby in
general, the Ra values amount to 0.63 .mu.m or less for bore
diameters of less than 30 mm, and Ra values of 0.8 .mu.m or less
are achieved for bore diameters between 30 mm and 60 mm. In the
exemplary embodiment, the bore diameter is selected, before
coating, in such a manner that the piston pin has a diametral play
of 10 .mu.m to 40 .mu.m in the finished pin bore 18. The
cylindrical bore 21 should be cleaned in such a manner that chips,
other particles, machining oils and the like are completely
removed. The inside surface of the cylindrical bore 21 can also be
phosphatized.
[0030] If additional oil collection chambers, for example in the
form of channels 24 or pockets 25, are supposed to be provided,
corresponding cover templates are affixed in the cylindrical bore
21 before coating takes place, in known manner. The cover templates
prevent coating of the covered region of the cylindrical bore 21.
As an alternative, the finished coating can subsequently be worked,
and can be provided with oil collection chambers in this way.
[0031] The coating agent selected in the exemplary embodiment is
formed from a thermally curable resin with solid lubricant
particles of one or more of the materials graphite, molybdenum
sulfide, tungsten disulfide, hexagonal boron nitride, and PTFE
embedded in it. In the exemplary embodiment, the resin is a very
temperature-resistant polyamide imide, and the solid lubricant is a
mixture of molybdenum sulfide and graphite particles having a
particle size of 1 .mu.m to 3 .mu.m. In the exemplary embodiment,
the amount of the solid lubricant is selected in such a manner that
the finished coating contains about 50 to 60 wt.-% solid lubricant
particles. The viscosity of the coating agent is adjusted in such a
manner that droplet formation is prevented in the case of
sufficient application.
[0032] A device 30 for rotation atomization serves to apply the
coating to the inside surface of the cylindrical bore 21, in the
exemplary embodiment. The device 30 has a base body 31 that is
connected with a nozzle body 32. The nozzle body 32 is mounted to
rotate on the base body, by means of a bearing 33. The nozzle body
32 is with a nozzle 34 having an exit opening 35. The base body 31
possesses feed channels 36, 37, in each instance, which are
intended for the liquid coating material and for compressed air,
and end in a mixing chamber 38 for mixing and metering. An exit
channel 39 extends from the mixing chamber 38, through the nozzle
body 32, and opens into the exit opening 35. A baffle plate 41 is
disposed perpendicular to the exit opening 35, so that a
ring-shaped gap 42 having a width of 0.5 mm in the exemplary
embodiment is formed between the baffle plate 41 and the nozzle
body 32. The coating agent/air mixture exits through the gap 42, in
the form of a spray jet 43, radially and at a distance from the
nozzle body 32.
[0033] The nozzle body 32 is put into rotation by means of a drive
44, and rotates in the speed of rotation range from 14,000 to
18,000 rotations per minute in the exemplary embodiment. The
coating agent/air mixture that exits from the exit opening 35 is
accelerated by the centripetal forces that occur at the exit
opening 35, in such a manner that it exits radially as a
disk-shaped spray jet 43. Since the spray jet 43 is configured
narrow in the pin axis direction, the inside surface of the
cylindrical bore 21 that is to be coated can be sharply delimited,
in the pin axis direction, by means of simple feed control of the
coating agent/air mixture. In the exemplary embodiment, nozzles 34
having a diameter in the range between 5 and 25 mm and having
depths up to 50 mm are available, so that it is possible to coat
cylindrical bores 21 for pistons of all engine types with the
device 30. The diameter of the nozzle 34 is generally selected in
such a manner that it approximately corresponds to half the
diameter of the cylindrical bore 21.
[0034] A centrifuge device S-520 from Sprimag in Kirchheim is also
suitable for carrying out the coating method.
[0035] In the exemplary embodiment, application of the coating
agent/air mixture takes place onto the inside surface of the
cylindrical bore 21, which has been pre-heated to 50.degree. C. to
80.degree. C. The nozzle 34 is introduced centrally into the
cylindrical bore 21, from the outside to the inside. To configure
the geometric deviation from the cylindrical inside contour, for
example of the shaped bore shown in FIG. 1, the advance of the
nozzle 34 is varied in a range of 10 to 20 mm/s, for example. In
addition or as an alternative, the amount of the coating agent/air
mixture exiting from the exit opening 35 of the nozzle 34 can be
varied. For this purpose, it is practical that the device 30 works
with computer control. When the nozzle 34 has reached the end of
the cylindrical bore 21, the device 30 is turned off and
retracted.
[0036] If cover templates are provided in the cylindrical bore 21
to produce oil collection chambers, the feed of the coating
agent/air mixture is shut off when such a template is reached, so
that residues of the spray jet are sprayed onto the cover template.
When the end of the cover template has been reached, the feed of
the coating agent/air mixture is achieved again.
[0037] When the coating agent has been applied, it is thermally
hardened, in that the piston, i.e. the piston component that has
the coated pin bores 18 is placed in an oven and held at a
temperature of 200.degree. C. between 10 and 20 minutes there, in
the exemplary embodiment.
[0038] The finished coating 22 is approximately 5 .mu.m to 20 .mu.m
thick at its thinnest point, and the diametral pin play is about 10
.mu.m to 20 .mu.m. This close play is particularly advantageous for
avoiding noises caused by pin ticks. The coating 22 furthermore
guarantees that despite the close play, no seizing occurs.
* * * * *