U.S. patent number 3,658,451 [Application Number 05/071,752] was granted by the patent office on 1972-04-25 for apex seal for rotary piston engine.
This patent grant is currently assigned to Toyo Kogyo Company Limited, Yoshiwa Kogyo Kabushiki Kaisha. Invention is credited to Nobuyasu Gomada.
United States Patent |
3,658,451 |
Gomada |
April 25, 1972 |
**Please see images for:
( Certificate of Correction ) ** |
APEX SEAL FOR ROTARY PISTON ENGINE
Abstract
An apex seal for a rotary piston engine, the apex seal being
made of cast iron and having an elongated shape, a roundish sliding
surface, the upper portion (including the sliding surface) with a
chilled structure containing a large proportion of cementite and
the lower portion with at least one-third of the height of the seal
and with no chilled structure; and a method of producing the
same.
Inventors: |
Gomada; Nobuyasu (Hiroshima,
JA) |
Assignee: |
Toyo Kogyo Company Limited
(Aki-gun, Hiroshima-ken, JA)
Yoshiwa Kogyo Kabushiki Kaisha (Aki-gun, Hiroshima-ken,
JA)
|
Family
ID: |
26414045 |
Appl.
No.: |
05/071,752 |
Filed: |
September 14, 1970 |
Foreign Application Priority Data
|
|
|
|
|
Sep 13, 1969 [JA] |
|
|
44/72912 |
Sep 13, 1969 [JA] |
|
|
44/72913 |
|
Current U.S.
Class: |
418/178; 277/406;
277/357; 418/179 |
Current CPC
Class: |
C21D
1/09 (20130101); F01C 19/005 (20130101); F05C
2201/0442 (20130101) |
Current International
Class: |
C21D
1/09 (20060101); F01C 19/00 (20060101); F04c
015/00 () |
Field of
Search: |
;418/178,179
;277/81P,236 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Bell, Jr.; Houston S.
Claims
What is claimed is:
1. An apex seal for a rotary piston engine, which is an integral
body made of cast iron or elongated shape and with a rounded
sliding top surface and which comprises an upper and a lower
portion, the former being a hardened portion including the sliding
surface and the latter being a non-hardened portion, the hardened
portion having chilled structure with a large proportion of
cementite and a Vickers hardness of not less than 550, and the
non-hardened portion being at least one-third of the seal in height
and having a Vickers hardness of not more than 400.
2. An apex seal according to claim 1 wherein the cast iron is
acicular cast iron.
Description
This invention relates to a cast iron made apex seal for rotary
piston engine. More particularly, it relates to an apex seal whose
surface has been treated to form a hardened layer of chilled
structure containing a large proportion of cementite and which is
in sliding contact with the inner surface of a casing that houses
the seal, and a method of producing the same.
The apex seal for a rotary piston engine is fitted at the apex of
the rotary piston and is adapted to make a planetary motion with
the piston while being pressed against the inner surface of the
casing by the combined action of elastic force of springs disposed
behind the apex seal, gas pressure in the operating chamber and
centrifugal force produced by rotation of the piston. As mentioned
above, it moves in sliding contact with said inner surface of the
casing while maintaining the airtightness therebetween. Therefore,
the apex seal used for this purpose must be one which has excellent
mechanical properties as well as high wear and heat resistances and
which also does not produce an excessive wear of the inner surface
of the casing and wavy abnormal abrasion, that is, so-called
chatter marks. Thus depending upon what quality the apex seal has,
it will exert a serious influence on the performance and durability
of the engine and cannot, therefore, be selected simply from the
standpoint of wear resistance unlike the ordinary mechanical
parts.
The present inventors have made extensive studies on the material
of apex seal and have found that the most excellent apex seal,
which does not produce any chatter mark on the inner surface of the
casing and satisfies the various requirements for an apex seal, can
be produced by making a seal from cast iron and treating the seal
to form a hardened layer containing a large amount of cementite, or
so-called chilled structure, in the upper part thereof including
its sliding surface. This hardened layer of cementite, popularly
called as chilled structure, is a form of ledeburite of cementite
(Fe.sub.3 C) or a mixture form of ledeburite and pro-eutectic
cementite. As is well known, in the manufacture of conventional,
ordinary mechanical parts, there is used a method of rapidly
cooling a molten iron for the parts by the so-called chilling
effect of a chiller during the casting operation thereby allowing
the cast iron to have a chilled structure only at a specific
surface thereof. If there is also used such a method in
manufacturing very small and thin mechanical parts such as apex
seals of this invention, the whole body of a molten iron for the
parts will quickly be cooled to form the parts made of cast iron
having a chilled structure throughout it, with consequent reduction
of their strength. Thus it is almost impossible to obtain desired
chilled structure exclusively at the sliding surface of such small
and thin mechanical parts. It may also occur to cut out an apex
seal from a large cast iron block having a chilled surface.
However, since mottled cast iron is always present below a chilled
portion, it is also next to impossible to cut out an apex seal
which is chilled exclusively at the sliding surface from any
portion of the block. For these reasons, it has been considered
technically unattainable to obtain a cast iron made apex seal
having a chilled structure exclusively at its sliding surface, and
hence the apex seal such as proposed in the present invention has
never been thought of in the art.
According to the present invention which has been achieved from
such standpoint, there is provided a process for producing a
desired apex seal comprising the steps of first preparing an
elongated cast iron made blank material having a width equal to or
slightly larger than that of the final product apex seal, then
subjecting the top surface portion of said blank material to
application of electron beam, arc, laser light or plasma to cause
rapid melting of the material, then rapidly cooling the molten part
by chilling effect of the non-molten part, and finally giving final
working thereto with or without previous stress-relieving heat
treatment to thereby form a hardened layer of chilled structure
containing a large amount of cementite at the sliding surface of
the apex seal which surface is slidingly contacted with the inner
surface of the casing.
The apex seal obtained according to the present invention is formed
with a hardened layer of cementite to the depth of several mm
beflow its sliding surface without inviting substantially any
impairment of mechanical and physical properties of the base cast
iron material and is provided with various characteristics,
particularly excellent wear resistance, required for an apex seal
used in a rotary piston engine. Further, the cementite of the
hardened layer is extremely stable even under high temperature
atmosphere within the engine and the excellent impact decrement
characterized by the cast iron of which the seal is made, prevents
chatter marks (abnormal abrasion) from occurring, so it is possible
to maintain the initial seal performance unchanged for a long
time.
Now the present invention will be described in detail by way of its
preferred embodiments with reference to the accompanying drawings,
in which:
FIG. 1 is a perspective view illustrating a manner in which
electron beam is applied;
FIG. 2 is a perspective view illustrating external appearance in
each step of the apex seal manufacturing process according to an
embodiment of the present invention;
FIG. 3 is a diagram showing transition of hardness below the
sliding surface of the above-said apex seal, in comparison with a
trial product obtained according to a conventional method where a
chilling effect is used at the time of casting;
FIGS. 4 and 5 are the 100 times magnified micro-photographs showing
respectively the structures of the hardened layer and the boundary
section in the apex seal produced according to the first
embodiment;
FIG. 6 is a thrice-magnified photograph of an end face of an apex
seal produced according to the first embodiment of the present
invention; and
FIG. 7 is a photograph showing the conditions of the sliding
surfaces, just after the bench tests, of the apex seals according
to the first and second embodiments of the present invention, in
comparison with that of a conventional carbon-type article.
Referring first to FIG. 1, it will be appreciated that an elongated
cast iron blank 1 having a width b equal to or slightly larger than
the width of the final product apex seal is prepared either by
shaping from a cast mass or by cutting from a cast iron plate, cast
iron block or the like. In this case, the width b is of an extent
in which final work allowance of the side 2 of the blank 1, is
included, while the length dimension 1 is one which corresponds to
the length of one or several or more pieces of apex seal combined.
The term "elongated" as used herein is not limited in its meaning
to a single apex length. The cast iron material used may be of any
type in which chilling can be performed, including ordinary cast
iron, alloy cast iron, nodular graphite cast iron, malleable cast
iron and others which are involved within the general category of
cast iron. If desired, the cast iron material may be subjected
previously to refining heat treatment.
Then, blank 1 is placed in an electron beam radiator in which
electron beams 3 are applied in a suitable manner to the top
surface 5 of blank 1 which is travelling longitudinally at moving
velocity V. Application of electron beams may be conducted, for
example, by projecting said beams continuously and swingingly in a
direction perpendicular to the longitudinal axis of blank 1 such as
to describe a zigzag trace 4, thereby to melt the blank material
down to the depth of several m./m. below the surface 5 of said
blank. In stead of using electron beams, it is also possible to
utilize arc, laser light, plasma or other means which can achieve
quick melting in a short time.
In this case, the non-molten portion 6 produces an effect similar
to that obtained when a chiller was attached, and the molten
portion 7 is rapidly cooled by this chilling effect, resulting in
formation of a chilled structure, namely, a hardened layer
containing a large amount of cementite. It is to be noted that
suitable selection of moving velocity of blank and electron beam
radiating conditions will allow the top surface 5' of said blank to
assume by itself after solidification a roundish configuration
closely resembling the desired top surface of the final apex seal
product due to surface tension of molten cast iron bath. Of course,
the top surface 5 of blank 1 may be previously chamferred or
otherwise worked into a desired roundish configuration. In either
way, it is possible to form the top surface 5' into a roundish
configuration. It is also possible to increase the chilling effect
by enlarging the height h of blank 1 more than necessary. Further,
the above-said melting operation may be conducted while cooling the
non-molten portion with suitable cooling means, for example, by
attaching a well heat conductive chiller such as a copper plate to
the side 2 and bottom surface 8 of said portion.
In this manner, hardened layer 9 containing cementite in abundance
is formed at the top surface, and then the structure, after or
without stress-relieving heat treatment, is subjected to final
working such as cutting or grinding to thereby produce a desired
apex seal. It should be noticed that since the top surface is
already shaped into a roundish configuration in a previous step, it
is possible to greatly save the time required for finish grinding
of the top surface. This is one of the important advantages of the
method of the present invention.
In FIG. 2 are shown external appearances that show up on the blank
after each step in the instant embodiment. Blank material 1a, which
is initially prepared, is worked in next step into an intermediate
or half-made article 1b having at its top surface a rounded
hardened layer 9, and then this intermediate article 1b is
subjected to finish work to form a final apex seal product 1c.
Although the foregoing discussion has been concentrated on an
integrated type apex seal, it will be understood that a split type
apex seal can also be produced in the same manner, this seal being
of the same type as the known split type.
EXAMPLE 1
An elongated intermediate blank 1a, which is rectangular in section
and has a size of 6.5 (b) .times. 12 (h) mm. and a length (l) of 70
mm., was prepared from nodular graphite cast iron (FCD 55- refer to
G5502 of Japanese Industrial Standards) as shown in FIG. 2. The
prepared blank was put in a welding chamber in an electron beam
welder with an output of 1.25 kw. and electron beams were applied
to said blank under the following conditions:
Degree of vacuum 5.times.10.sup..sup.-4 Torr.(mmHg) Acceleration
voltage 25 KV Beam current 22 mA Electromagnetic lens current 58 mA
Blank feeding velocity 32 mm/min Beam amplitude 6.5 mm Beam
amplitude period 2 sec/cycle
The top surface of the blank is instantaneously melted at a
temperature of approximately 1,500.degree. C. by the irradiation of
electron beam. The thus-melted portion is then solidified in
several seconds after the irradiation due to a chilling effect of
the non-melted portion to form a hardened layer.
The top surface of the intermediate blank 1b after electron beam
application, as shown in FIG. 2, had a roundish configuration
closely resembling the shape of the sliding surface of the final
apex, so that finish grinding work on the final top surface was
completed in an extremely short time, and as a result, a 6 .times.
10 .times. 60 mm. apex seal 1c having at its sliding surface a
hardened layer 9 containing a large proportion of cementite was
obtained. The end face of the produced apex seal as shown in FIG. 6
had a clearly visible hardened layer 9 (in FIG. 2), and this
hardened layer, as shown in FIG. 4, had an extremely compact,
perfectly chilled structure having Vickers hardness (VHN) of 780.
FIG. 5 is a photograph showing the structure at the boundary
section. Structural difference between the hardened layer and the
base material of the apex seal is obvious from FIG. 5. Transition
or gradient of hardness below the sliding surface of the thus
obtained apex seal 1c is shown by a curve 10 in FIG. 3. As compared
with hardness transition curve 11 of a trial product according to a
conventional method using chiller at the time of casting, no
impairment of characteristics of the base material is observed in
the product of the present invention.
The apex seal produced by the conventional method has Vickers
hardness of about 660 at the sliding surface, but the hardness is
gradually lowered in proportion to the distance from the sliding
surface. Hardness at the bottom surface is also as high as more
than 450 in VHN. This means that the apex seal is chilled in its
entirety and that its mechanical strength is too lowered to stand
practical use. Whereas, the apex seal according to Example 1 of the
present invention has high hardness of more than 750 (VHN) at the
sliding surface and to the depth of about 2 mm. below said sliding
surface, but hardness is sharply reduced as the distance from the
sliding surface is increased up to about 5 mm. below the sliding
surface. Thereafter, however, hardness remains substantially
constant at 250 (in VHN), or same value as that of base material,
through the thickness down to the bottom. These facts dictate that
the apex seal of Example 1 of the present invention has a sliding
surface which maintains always high hardness during use even if it
is abraded, and that the characteristics of base material in the
lower half of the apex seal are not the least impaired, allowing
maintenance of mechanical strength sufficient to stand practical
use. In the present invention, sliding surface hardness of more
than 550 in VHN is sufficient for use, and best result is obtained
when said hardness is more than 700. It is also desirable that the
portion of at least one-third of the height of the apex seal
remains unchanged or original in hardness and it has hardness of
less than 400 in VHN.
In connection with the above-mentioned irradiating conditions, the
feeding rate of a blank may correspondingly be lowered if the beam
current is decreased, and the frequency of beam oscillation may be
increased if the feeding rate of the blank is lowered. The
amplitude of the electron beam is determined depending upon the
width of a desired apex seal and is desirable to be approximately
equal to, or somewhat small than, the width of the desired apex
seal. The conditions under which the electron beam irradiated,
widely vary with the size of a desired apex seal. The preferable
conditions are as follows:
Vacuum 1.times.10.sup..sup.-4 -5.times.10.sup..sup.-2 Torr. (mmHg)
Beam current 15-16 mA Beam Current 15-60 mA Frequency of beam
oscillation 0.5-3.5 sec/cycle
EXAMPLE 2
Similar steps to those in Example 1 were followed under the same
conditions as in Example 1 but by using common cast iron (FC 25 -
refer to G5501 of Japanese Industrial Standards) to obtain an apex
seal of the same size and configuration as those of the product in
the previous example. The hardened layer was a perfect chilled
structure having hardness of 720 (VHN).
EXAMPLE 3
This was prepared a blank 1a for apex seal consisting of 3.7
percent C, 2.3 percent Si, 0.35 percent Mn, 0.5 percent Cr, 1.0
percent Ni, 1.5 percent Mo, 0.9 percent Cu and the balance
comprising Fe and incidental elements such as P, S and the like,
from an acicular cast iron which is known as an alloy cast iron.
The blank 1a had the same size and shape as the one in Example 1.
The blank was subjected to electron beam irradiation under the same
conditions as in Example 1. It had hardness of 370 VHN before the
irradiation and had hardness of 900 VHN at its hardened layer after
the irradiation. The irradiated blank was then subjected to
stress-relieving heat treatment for about 2 hours with the result
that it decreased from 900 to 750 VHN in hardness at its hardened
layer and remained the same as the original hardness of 370 VHN at
its lower portion. The blank was subsequently given final working
to obtain a desired apex seal therefrom. If stress-relieving heat
treatment or stress relief tempering is effected in the
above-mentioned step, it will be effective in preventing the
hardened layer from breaking during the final working and also in
preventing the layer from changing in hardness due to the
temperature of an engine in which the apex seal obtained is
fitted.
Then, three apex seals obtained in Example 1 were incorporated in
the front side piston in a known 2 and 3 lobe type NSU-Wankel
rotary piston engine of 491 cc. .times. 2 piston system, while
three prior art apex seals prepared by impregnating carbon sintered
articles with aluminum were incorporated in the rear side piston in
the same engine. In the same manner, three apex seals obtained in
Examples 2 and 3 three above-said prior art apex seals were
incorporated in the respective pistons in other two engines of the
same type as said above. And these three rotary piston engines were
subjected to bench test under full load of 6,000 r.p.m. (95 ps) for
duration of 300 hours in succession. This bench test is equivalent
to about 50,000 km. actual running. During operation, completely no
trouble was witnessed, and overhall tests of the engines after
operation showed that both the casing applied with hard Cr plating
and the apex seals of the present invention suffered no abnormal
abrasion and were quite satisfactory. The post-operation conditions
on the sliding faces of the apex seals of Examples 1 and 2 and of
the prior art are shown in FIG. 7, by numbers 12 to 14,
respectively. In Table 1 below are shown the amounts of abrasion
that was observed on the respective apex seals and casings after
the test.
The apex seals of Examples 1, 2 and 3, which had been subjected to
the above test, were again incorporated in still another engine of
the same type and were subjected to additional 100-hour test
operation by varying rotational frequency of the engine. The
results showed no abnormality and suggested ability for practical
use.
---------------------------------------------------------------------------
TABLE 1
Apex Seal
Engine Abrasion Classifi- Abrasion No. cation rate (.mu./H) loss in
Sliding End face casing surface
__________________________________________________________________________
1 Example 1 0.5 0.01 max. 8.mu. 2 Prior art 1.8 0.06 max. 6.mu. 3
Example 2 0.7 0.01 max. 8.mu. 4 Prior art 1.8 0.08 max. 7.mu. 5
Example 3 0.3 0.01 max. 8.mu. 6 Prior art 1.8 0.08 max. 7.mu.
__________________________________________________________________________
As evident from FIG. 7 and Table 1 above, the apex seals according
to Examples 1, 2 and 3 of the present invention showed high
superiority in abrasion resistance over the conventional carbon
type products, and also the casings in which the apex seals of the
present invention were mounted suffered less abrasion loss. It was
also confirmed that the devices of the present invention bring
about remarkable improvement over the problem of reduction of gas
sealing ability due to abrasion of end faces observed in the
conventional carbon type or specific cast iron type products. The
Table also shows that the apex seal prepared from the acicular cast
iron has better performance probably because said cast iron is
superior in wear resistance and impact decrement.
As discussed above, the method for producing apex seals for rotary
piston engine according to the present invention comprises
substantially the steps of preparing an elongated cast iron blank
having a width equal to or slightly larger than that of the final
apex seal product, rapidly melting the top surface of said blank by
application of electron beams or by other suitable means, then
quickly cooling the molten portion by chilling effect of the
non-molten portion, and finally subjecting same to suitable final
works with or without previous stress-relieving heat treatment to
thereby form a hardened layer of chilled structure containing a
large amount of cementite at the sliding surface of the apex seal
which is slidingly contacted with the inner surface of the casing.
Thus, according to the present invention, a large amount of
cementite can be integrally formed on the body cast iron material
without impairing the characteristics of the latter to produce a
structure having combined characteristics of said both materials,
so that the resultant product has excellent properties such as
strength, abrasion resistance, heat resistance and so forth
required for practical use, as well as stabilized quality. The apex
seal according to the present invention can best be adapted in a
chrome-plated casing. Usually, a hardened layer of this type is so
hard that it sometimes proves difficult to exercise cutting or
grinding operation. However, according to the method of the present
invention, final finish grinding or cutting operation can be
completed in an extremely short time since the top surface of the
blank after melting has already a configuration very near to the
final shape of the sliding face of the finished apex seal. This,
coupled with inexpensiveness of blank material, allows manufacture
of the desired apex seals at low cost. Thus, the present invention
can be very highly appraised for its industrial utility.
* * * * *