Information
-
Patent Grant
-
6691650
-
Patent Number
6,691,650
-
Date Filed
Wednesday, November 6, 200222 years ago
-
Date Issued
Tuesday, February 17, 200421 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Armstrong, Kratz, Quintos, Hanson & Brooks, LLP
-
CPC
-
US Classifications
Field of Search
-
International Classifications
-
Abstract
A piston valve type layered scavenging 2-cycle engine has a reduced engine height, is light and compact, and achieves an exhaust gas purification. An upper edge of a pilot air port provided in an inner wall of a cylinder is positioned at substantially the same height as that of an upper edge of an intake port. An extended portion extended to a lower side rather than a piston lower edge at a position opposing to the intake port is provided in a lower end portion at a position opposing to the pilot air port in the piston. An interval between the right and left extended portions is set to be larger than an outer width of a balance weight of a crank shaft. A piston groove which connects the pilot air port to the scavenging port at a time of an intake stroke is provided on an outer peripheral surface of the extended portion. A second scavenging flow passage having a simple structure is provided in a lower side of a first scavenging flow passage.
Description
TECHNICAL FIELD
The present invention relates to a piston valve type layered scavenging 2-cycle engine, and particularly to an improved arrangement of cylinder ports, piston shape and scavenging flow passage.
BACKGROUND ART
With respect to an arrangement of an intake port for an air-fuel mixture, a pilot air port and the like in a piston valve type layered scavenging 2-cycle engine (hereinafter, refer to as a layered scavenging 2-cycle engine), there is a structure disclosed in International Laid-Open No. WO98/57053 as one example. In accordance with this publication, a scavenging port
12
, a pilot air port
14
and an exhaust port (not shown) are open to a cylinder chamber
11
(an inner peripheral surface of a cylinder
10
) as shown in FIG.
13
. The cylinder
10
is provided with an intake port
15
, for an air-fuel mixture, which communicates with a crank chamber
3
. A scavenging flow passage
16
connects between the cylinder chamber
11
and the crank chamber
3
. Two pilot air ports
14
are provided in right and left sides with respect to the intake port
15
. The pilot air ports
14
are provided at positions a predetermined distance apart from the scavenging port
12
to a side of the crank chamber
3
in an axial direction of the cylinder
10
. The scavenging port
12
and the pilot air ports
14
are connected via a piston groove
34
a
provided in an outer peripheral portion of a piston
30
a,
whereby an air. Air is sucked into the scavenging flow passage
16
from the pilot air ports
14
via the scavenging port
12
at a time of an intake stroke. In order to prevent the pilot air ports
14
from being directly open to the cylinder chamber
11
during all the strokes of the piston
30
a,
a piston lower edge
31
is positioned below the pilot air ports
14
when at a top dead center of the piston shown by a solid line. A piston upper edge
35
is positioned above the pilot air ports
14
when at a bottom dead center of the piston shown by a narrow two-dot chain line. The piston lower edge
31
is positioned at a closest position to a crank shaft at which the piston lower edge does not interfere with an outer peripheral portion
23
a
of a balance weight
23
provided in the crank shaft, when at the bottom dead center of the piston. Since the intake port
15
is provided in parallel to a lateral direction to the pilot air ports
14
, a vertical groove
40
having a predetermined length F is provided in the piston lower edge
31
portion, in order to communicate the intake port
15
with the crank chamber
3
when at the top dead center of the piston.
In accordance with the structure mentioned above, since an interior portion of the cylinder chamber
11
is at first scavenged by the pilot air at a time of being exhausted, it is possible to prevent an unburned gas from being discharged due to a blow-by of the air-fuel mixture, so that the exhaust gas can be cleaned up.
In the structure of the layered scavenging 2-cycle engine mentioned above, in order to communicate the suction port
15
with the crank chamber
3
at the top dead center of the piston, there is provided the vertical groove
40
having the length F extending from the piston lower edge
31
to the intake port upper edge
15
a.
Accordingly, the piston lower edge
31
is positioned the length F below the intake port upper edge
15
a.
At a time when the piston is at the bottom dead center, the piston upper edge
35
is positioned above the intake port upper edge
15
a,
and the piston lower edge
31
is defined so as to be positioned above the outer peripheral portion
23
a
of the balance weight in the crank shaft
20
. At the top dead center of the piston, when setting a height from the intake port upper edge
15
a
to the piston upper edge
35
to H, it is necessary to set a piston height from the piston lower edge
31
to the piston upper edge
35
to +F.
There has been a requirement of making the height of the engine lower so as to make placing space as small as possible. There has been a strong desire to solve the problems that a length of a connecting rod is increased in correspondence to an increase of the piston height, therefore a height of the engine is increased, the placing space is increased, a weight thereof becomes heavy, and a cost is increased.
The layered scavenging 2-cycle engine has the scavenging flow passage which feeds the pilot air to the interior portion of the cylinder chamber so as to scavenge, in order to exhaust the gas within the cylinder after combustion to the external portion.
FIG. 14
is a front elevational cross sectional view of a layered scavenging 2-cycle engine in accordance with a conventional second example, and
FIG. 15
is a view along a line N—N in
FIG. 14. A
cylinder
82
is mounted to an upper surface of a crank case
81
. A piston
83
is inserted to into a cylinder
82
so as to freely slide in an axial direction of the cylinder
82
. A crank shaft
54
is rotatably mounted to the crank case
81
. The piston
83
and the crank shaft
54
are connected by a connecting rod
55
. An exhaust port
60
is open to a cylinder chamber
56
, a pair of scavenging ports
61
and
61
and a pair of pilot air ports
62
and
62
are provided on a wall surface of the cylinder
82
, and an air-fuel mixture port
63
open to a crank chamber
57
is provided thereon. A pair of scavenging flow passages
90
and
90
which respectively connect a pair of scavenging ports
51
and
51
to the crank chamber
57
are provided within a side wall of the cylinder
82
. Opening portions
91
and
91
are respectively provided in lower end portions of the scavenging flow passages
90
and
90
. A pair of grooves
84
and
84
for respectively connecting a pair of pilot air ports
62
and
62
to a pair of scavenging ports
61
and
61
near a top dead center of the piston are provided on a side surface of the piston
83
. The exhaust port
60
, the scavenging ports
61
and
61
, the pilot air ports
62
and
62
and the air-fuel mixture port
63
are opened and closed on the basis of an upward and downward motion of the piston
83
.
When the piston moves upward, a pressure of the crank chamber
57
is reduced, the pilot air is sucked from the pilot air ports
62
and
62
near the top dead center of the piston and is charged into the scavenging flow passages
90
and
90
from the scavenging ports
61
and
61
through the piston grooves
84
and
84
. At the same time, the air-fuel mixture is sucked within the crank chamber
57
from the air-fuel mixture port
63
. When the air-fuel mixture is ignited and burned in the cylinder chamber
56
, the piston
83
is pressed down, and the pilot air ports
62
and
62
and the air-fuel mixture ports
63
are closed. Thereafter, the exhaust port
60
is at first opened, whereby the exhaust gas is discharged, and next the scavenging ports
61
and
61
are opened. The pressure in the crank chamber
57
is increased, the pilot air within the scavenging flow passages
90
and
90
flows into the cylinder chamber
56
so as to discharge the exhaust gas to an external portion from the exhaust port
60
, and subsequently the air-fuel mixture within the crank chamber
57
flows into the cylinder chamber
56
from the scavenging ports
61
and
61
through the scavenging passages
90
and
90
. An amount of blow-by of the air-fuel mixture from the exhaust port
60
to the external portion is reduced, and the exhaust gas is purified. However, since an amount of the pilot air is equal to a volume of the scavenging flow passage
90
and the amount is insufficient, the blow-by of a part of the air-fuel mixture is generated, so that it is impossible to sufficiently purify the exhaust gas.
In order to solve this, Japanese Unexamined Patent Publication No.
58-5423
is proposed as a conventional third example.
FIG. 16
is a front elevational cross sectional view of a layered scavenging 2-cycle engine described in the publication. A cylinder
82
is mounted to an upper surface of a crank case
85
. A scavenging port
61
communicates with a crank chamber
57
via a scavenging flow passage
92
. The scavenging flow passage
92
passes through an interior portion of a side wall the cylinder
82
and passes through an interior portion of d side wall of the crank case
85
so as to communicate with an opening portion
93
provided in a bottom portion of the crank chamber
57
. That is, since the scavenging flow passage
92
is long and large, an amount of pilot air can be sufficiently secured, a blow-by of an air-fuel mixture is greatly reduced, and an exhaust gas is purified.
However, since the scavenging flow passage
92
is formed within the side wall of the crank case
85
, there are problems that a structure of the crank case
85
becomes complex, enlarged and heavy, and a cost is increased.
DISCLOSURE OF THE INVENTION
An object of the present invention is to provide a layered scavenging 2-cycle engine which can reduce a length of a piston in a direction of a cylinder shaft so as to reduce a height of an engine, thereby making a placing space small and reducing a weight. Another object is to provide an engine which can sufficiently secure an amount of pilot air so as to provide exhaust gas purification.
In accordance with a first aspect of the present invention, there is provided a piston valve type layered scavenging 2-cycle engine having: 1) a scavenging port, an exhaust gas port and a pilot air port which are open to an inner wall of a cylinder attached to an upper portion of a crank case connected to a cylinder chamber; 2) an intake port for an air-fuel mixture which is open to the inner wall of the cylinder and is in communication with a crank chamber; 3) a scavenging flow passage which connects the scavenging port and the crank chamber; and 4) a piston groove which is provided in an outer peripheral portion of the piston and connects the scavenging port and the pilot air port at a time of an intake stroke. The scavenging port, the exhaust port, the pilot air port and the intake port are opened and closed by an upward and downward motion of the piston.
A lower edge of the pilot air port is arranged at a position close to the crank chamber side rather than an upper edge of the intake port. An extended portion extended to a lower side, rather than a piston lower edge, at a position opposing to the intake port of the piston is provided in a lower portion at a position opposing to the pilot air port of the piston. The extended portion is positioned at an outer side in a direction of a crank shaft, rather than a balance weight attached to a web of the crank shaft, and has the piston groove on an outer peripheral surface thereof.
Since the lower edge of the pilot air port is arranged at the position close to the crank chamber side rather than the upper edge of the intake port, it is possible to dispose the upper edge of the pilot air port close to the crank chamber side. Accordingly, it is possible to dispose the position of the piston upper edge, when at a time of a bottom dead center of the piston, close to the crank chamber side. The piston lower edge portion in an outer side in an axial direction from the balance weight of the crank shaft is extended, and the piston groove connecting the pilot air port and the scavenging port is provided in this portion. Accordingly, it is possible to move the piston lower edge down to a position at which the piston lower edge does not interfere with the outer peripheral portion of the balance weight at a time of the bottom dead center of the piston. Accordingly, it is possible to reduce a piston height from the piston upper edge to the piston lower edge, and it is possible to obtain the layered scavenging 2-cycle engine which is low in an engine height, light and compact, and has a reduced cost.
In accordance with a second aspect of the present invention, there is provided a piston valve type layered scavenging 2-cycle engine, as recited in the first aspect, wherein the upper edge of the intake port and the upper edge of the pilot air port are positioned at substantially the same height.
It is possible to dispose the piston upper edge, at a time of the bottom dead center of the piston, to the crank chamber side up to the portion close to the intake port upper edge, and it is possible to further reduce the length of the piston in the direction of the cylinder shaft. Since it is possible to reduce the length of the connecting rod so as to reduce the engine height, it is possible to further reduce the weight, and the cost can be reduced.
In accordance with a third aspect of the present invention, there is provided a piston valve type layered scavenging 2-cycle engine having a scavenging port which is open to a cylinder chamber of a cylinder mounted on an upper surface of a crank case forming a crank chamber in an inner side thereof, and sucking a pilot air taken from an external portion so as to scavenge. A scavenging flow passage is provided in an outer side rather than a side wall surface of the cylinder chamber, and communicates the scavenging port and the crank chamber. The scavenging flow passage has a first scavenging passage which is provided in an outer side of a side wall surface of the cylinder so as to be substantially in parallel to an axis of the cylinder, and a second scavenging flow passage which is provided on an upper surface of the crank case opposing to the first scavenging passage so as to be expanded in a substantially perpendicular direction to the first scavenging passage. The second scavenging flow passage has an opening portion communicating with the crank chamber in a terminal portion. The opening portion and the second scavenging passage are formed by: 1) a recess portion which is provided on the upper surface of the crank case; 2) a cylinder base surface of the cylinder which is brought into contact with the upper surface of the crank case; 3) a cylinder skirt portion in a lower portion of a side surface of the cylinder; and 4) a cylinder skirt extended portion which is extended so as to make a portion opposing to the second scavenging passage in the cylinder skirt portion close to or in contact with a bottom surface portion of the recess portion.
Since the second scavenging flow passage which is provided with the recess portion on the upper surface of the crank case is provided in the lower side of the first scavenging flow passage which is provided in the outer side of the cylinder wall surface and communicates with the scavenging port, and the opening portion is provided in the terminal portion of the second scavenging flow passage, it is possible to secure a large capacity for the scavenging flow passage. Accordingly, it is possible to secure enough pilot air to scavenge, and it is possible to securely achieve an exhaust gas purification. Since the second scavenging flow passage and the opening portion thereof are formed by the recess portion which is provided on the upper surface of the crank case, the cylinder base surface, the cylinder skirt portion and the cylinder skirt extended portion, the structure can be made simple, the crank case can be made compact and light, and it is possible to obtain an inexpensive layered scavenging 2-cycle engine.
In accordance with a fourth aspect of the present invention, there is provided a piston valve type layered scavenging 2-cycle engine as recited in the first aspect, wherein the scavenging flow passage has a first scavenging passage which is provided in an outer side of a side wall surface of the cylinder so as to be substantially in parallel to an axis of the cylinder, and a second scavenging flow passage which is provided on an upper surface of the crank case opposing to the first scavenging passage so as to be expanded in a substantially perpendicular direction to the first scavenging passage. The second scavenging flow passage has an opening portion communicating with the crank chamber in a terminal portion. The opening portion and the second scavenging passage are formed by: 1) a recess portion which is provided on an upper surface of the crank case; 2) a cylinder base surface of the cylinder which is brought into contact with the upper surface of the crank case; 3) a cylinder skirt portion in a lower portion of a side surface of the cylinder; and 4) a cylinder skirt extended portion which is extended so as to make a portion opposing to the second scavenging passage in the cylinder skirt portion close to or in contact with a bottom surface portion of the recess portion.
It is possible to obtain a layered scavenging 2-cycle engine which becomes lighter and more compact, has a reduced cost and can securely achieve an exhaust gas purification.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a front elevational cross sectional view of a layered scavenging 2-cycle engine in accordance with a first embodiment of the present invention at a time of a top dead center of a piston;
FIG. 2
is a side elevational cross sectional view at a time of a top dead center of the piston in
FIG. 1
;
FIG. 3
is a cross sectional view of a cylinder along a line A—A in
FIG. 1
;
FIG. 4
is a side elevational cross sectional view at a time of a bottom dead center of the piston in
FIG. 1
;
FIG. 5
is a front elevational view of the piston in accordance with the first embodiment;
FIG. 6
is a view along a line B—B in
FIG. 5
;
FIG. 7
is a view along a line C—C in
FIG. 1
;
FIG. 8
is an expansion view along a line D—D in
FIG. 7
;
FIG. 9
is a front elevational cross sectional view of a cylinder and a crank case in accordance with a second embodiment of the present invention;
FIG. 10
is a view along a line K—K in
FIG. 9
;
FIG. 11
is a view along a line L—L in
FIG. 9
;
FIG. 12
is a view along a line M—M in
FIG. 9
;
FIG. 13
is a side elevational cross sectional view of a cylinder portion in a layered scavenging 2-cycle engine in accordance with a first example of the prior art;
FIG. 14
is a front elevational cross sectional view of a layered scavenging 2-cycle engine in accordance with a second example of the prior art;
FIG. 15
is a view along a line N—N in
FIG. 14
; and
FIG. 16
is a front elevational cross sectional view of a layered scavenging 2-cycle engine in accordance with a third example of the prior art.
BEST MODE FOR CARRYING OUT THE INVENTION
FIG. 1
is a front elevational cross sectional view of a layered scavenging 2-cycle engine in accordance with a first embodiment, and
FIG. 2
is a side elevational cross sectional view thereof and shows a state in which a piston is at a top dead center position. A cylinder
10
is attached to an upper portion of a crank case
2
. A piston
30
is inserted into the cylinder
10
so as to freely slide in an axial direction of the cylinder
10
. A cylinder chamber
11
is formed in a head side of the piston
30
, and a crank chamber
3
is formed in a bottom side. A crank shaft
20
is rotatably attached to the crank case
2
via a bearing
4
, and the piston
30
is connected by a connecting rod
5
. A balance weight
23
is provided at a position opposite to the crank pin
22
, in a web
21
of the crank shaft
20
, and an outer peripheral portion
23
a
thereof is formed in a circular arc shape. A scavenging port
12
connected to the cylinder chamber
11
, an exhaust port
13
and a pilot air port
14
are provided on an inner wall surface of the cylinder
10
. An intake port
15
for an air-fuel mixture is connected to the crank chamber
3
. A scavenging flow passage
16
connects the scavenging port
12
to the crank chamber
3
in the cylinder
10
.
FIG. 3
is a cross sectional view of the cylinder
10
along a line A—A in FIG.
1
. Two pilot air ports
14
and
14
are provided in both sides of the intake port
15
. Each of pilot air port lower edges
14
b
and
14
b
is positioned in a lower side of an intake port upper edge
15
a.
The intake port upper edge
15
a
and pilot air port upper edges
14
a
and
14
a
are positioned at the same height. The scavenging ports
12
and
12
are provided in an upper side of the pilot air ports
14
and
14
at a predetermined interval, and are respectively connected to scavenging flow passages
16
and
16
.
FIG. 4
is a side elevational cross sectional view of the layered scavenging 2-cycle engine at a piston bottom dead center position. A piston lower edge
31
is set to a position closest to the crank shaft
20
at which the piston lower edge does not interfere with outer peripheral portions
23
a
and
23
a
of both balance weights
23
and
23
in the crank shaft
20
. This portion corresponds to a position opposing to the intake port
15
at a time when the piston
30
moves upward and downward. Extended portions
32
and
32
are provided in both lower end portions of the piston
30
in an axial direction of the crank shaft
20
so as to be extended to a lower side from the piston lower edge
31
. A piston groove
34
is provided in an outer periphery of the extended portion
32
, respectively. An inner width W
1
of the extended portion
32
is set to be larger than an outer width W
2
between both of the balance weights
23
and
23
in the direction of the crank shaft. An interval W
3
between two pilot air ports
14
and
14
, shown in
FIG. 3
, is set to be larger than the inner width W
1
of the extended portion
32
. An extended portion lower edge
33
is set at a position at which the extended portion lower edge does not interfere with an outer peripheral portion
6
a
of a boss
6
in which the bearing
4
provided in the crank chamber
3
is internally provided. The extended portion
32
is provided at a position opposing to the pilot air port
14
at a time when the piston
30
moves upward and downward. A piston groove
34
provided in the extended portion
32
connects the scavenging port
12
to the pilot air port
14
at the piston top dead center position, as shown in
FIG. 2. A
piston upper edge
35
is set so as to be positioned at an upper side, rather than the intake port upper edge
15
a,
and the pilot air port upper edge
14
a
at the piston bottom dead center position as shown in FIG.
4
.
FIG. 5
is a front elevational view of the piston
30
, and
FIG. 6
is a view along a line B—B in FIG.
5
. The extended portion
32
is provided in the lower end portion of the piston
30
so as to be extended to the lower side rather than to the piston lower edge
31
. The piston groove
34
is provided on an outer peripheral surface of the extended portion
32
. The piston lower edge
31
is set to a position at which the piston lower edge does not interfere with the balance weight outer peripheral portion
23
a.
The extended portion lower edge
33
is set to a position at which the extended portion lower edge does not interfere with the outer peripheral portion
6
a
of the boss
6
in the crank chamber
3
, respectively. A piston height from the piston upper edge
35
to the piston lower edge
31
is H.
FIG. 7
is a view along a line C—C in FIG.
1
. The exhaust port
13
is provided in an opposite side of the intake port
15
, and the pilot air ports
14
and
14
are provided in both sides of the intake port
15
. The scavenging ports
12
and
12
, and the scavenging flow passages
16
and
16
are provided in both sides in a perpendicular direction to a center line E—E connecting the intake port
15
to the exhaust port
13
. At the piston top dead center position, two piston grooves
34
and
34
respectively connect the pilot air ports
14
and
14
to the scavenging ports
16
and
16
.
FIG. 8
is an expansion view along a line D—D in
FIG. 7
, and shows a relational position between the respective ports provided on the cylinder inner wall surface and the piston. Solid lines show the scavenging ports
12
and
12
, the exhaust port
13
, the pilot air ports
14
and
14
, and the intake port
15
which are provided on the inner wall surface of the cylinder
10
. Narrow broken lines show the piston upper edge
35
, the piston lower edge
31
and the piston groove
34
at the top dead center position. Narrow two-dot chain lines show the piston upper edge
35
and the piston lower edge
31
at the bottom dead center, respectively. At the piston top dead center position, the piston groove
34
connects the pilot air port
14
to the scavenging port
12
. The piston lower edge
31
is positioned in the upper side of the intake port
15
. At the piston bottom dead center, the piston upper edge
35
is positioned in the lower side of the scavenging port
12
and the exhaust port
13
, and is positioned in the upper side of the pilot air port
14
and the intake port
15
. A distance from the piston upper edge
35
to the piston lower edge
31
is the piston height H shown in FIG.
5
.
Since the layered scavenging 2-cycle engine
1
in accordance with the first embodiment is structured in the manner mentioned above, it is possible to make a height of the piston
30
low. That is, in comparison with the conventional piston
30
a
shown in
FIG. 13
, it is possible to shift the positions of the intake port
15
and the pilot air port
14
to be close to the crank chamber
3
at a length F, and it is possible to shift the position of the piston upper edge
35
close to the crank chamber
3
at the length F. Accordingly, although the height of the conventional piston is +F the height of the piston in accordance with the present embodiment is H and can be made lower at. The height is reduced by the length F. Since it is possible to make the connecting rod
5
short shorter accordingly, it is possible to obtain the layered scavenging 2-cycle engine which has a reduced height, is light and compact and has a reduced cost.
FIG. 9
is a front elevational cross sectional view of a cylinder and a crank case in accordance with the second embodiment, and
FIG. 10
is a view along a line A—A in
FIG. 9. A
cylinder
52
is mounted on an upper surface
58
of a crank case
51
so as to bring a cylinder base surface
66
into contact with the crank case, and is fastened by bolts (not shown). An exhaust port
60
, a pair of scavenging ports
61
and
61
, a pair of pilot air ports
62
and
62
and an air-fuel mixture port
63
are open to an inner wall of the cylinder
52
. A pair of first scavenging flow passages
71
and
71
which communicate with the scavenging ports
61
and
61
in upper portions, have open portions in lower portions thereof, and are in parallel to a cylinder axis are provided within a side wall of the cylinder
2
. A pair of recess portions
74
and
74
which communicate respectively with the lower opening portions of a pair of first scavenging flow passages
71
and
71
and are expanded in a substantially perpendicular direction with respect to the first scavenging flow passages
71
and
71
are provided in the upper surface
58
of the crank case
51
. A pair of second scavenging flow passages
72
and
72
, which have an opening portion
73
communicating with the crank chamber
57
, are provided in terminal portions of the respective recess portions
74
and
74
. The scavenging flow passage
70
is constituted by the first and second scavenging flow passages
71
and
72
.
FIG. 11
is a view along a line L—L in
FIG. 9
, and shows a shape of a recess portion
64
formed on the crank case upper surface
58
. A cylinder skirt extended portion
68
is provided in a portion corresponding to the second scavenging flow passage
72
in a skirt portion
67
of the cylinder
52
, and a front end portion thereof is close to or brought into contact with a bottom surface of the recess portion
64
. That is, the second scavenging flow passage
72
is formed by the recess portion
64
, the cylinder base surface
66
, the cylinder skirt portion
67
, and the cylinder skirt extended portion
68
. The opening portion
73
is formed by the recess portion
64
, the cylinder base surface
66
and the cylinder skirt extended portion
68
, as shown in
FIG. 12
corresponding to a view along a line M—M in FIG.
9
.
Since the scavenging flow passage
70
of the layered scavenging 2-cycle engine in accordance with the present embodiment is constituted by the first and second scavenging flow passages
71
and
72
, the scavenging flow passage becomes larger than the conventional one at the volume of the second scavenging flow passage
72
. The amount of pilot air is increased at that amount, so that it is possible to securely achieve the exhaust gas purification. Since the second scavenging flow passage
72
and the opening portion
73
are formed by the recess portion
64
provided on the upper surface
58
of the crank case
5
, the cylinder base surface
66
, the cylinder skirt portion
67
and the cylinder skirt extended portion
68
, the structure is simple, and it is possible to reduce the thickness of the side wall of the crank case
51
in comparison with the case that the scavenging flow passage is provided within the side wall of the conventional crank case
51
. Accordingly, it is possible to make the structure compact and light, and the cost can be reduced.
Claims
- 1. A piston valve type layered scavenging 2-cycle engine (1) comprising:a cylinder (10) and a piston (30) to freely slide in an axial direction of the cylinder; a scavenging port (12), an exhaust gas port (13) and a pilot air port (14) which are open to an inner wall of the cylinder which is attached to an upper portion of a crank case (2), and which communicate with a cylinder chamber (11); an intake port (15) for an air-fuel mixture which is open to the inner wall of the cylinder, and is which communicates with a crank chamber (3); a scavenging flow passage (16) which connects the scavenging port and the crank chamber; and a position groove (34) which is provided in an outer peripheral portion of the piston and which connects the scavenging port and the pilot air port at a time of an intake stroke, wherein the scavenging port, the exhaust port, the pilot air port and the intake port are opened and closed by an upward and downward motion of the piston, a lower edge (14b) of said pilot air port is arranged at a position toward the crank chamber side displaced from an upper edge (15a) of said intake port, said piston includes an extended portion (32) extending beyond a piston lower edge (31) at a position opposing to the intake port of the cylinder, said extended portion being at a position opposing to the pilot air port of said cylinder, and the extended portion is positioned at an outer side of said piston in a direction of a crank shaft (20), and has said piston groove (34) on an outer peripheral surface thereof.
- 2. A piston valve type layered scavenging 2-cycle engine as claimed in claim 1, wherein the upper edge (15a) of said intake port and the upper edge (14a) of said pilot air port are positioned at substantially the same height.
- 3. A piston valve type layered scavenging 2-cycle engine comprising:a scavenging port (61) which is open to a cylinder chamber (56) of a cylinder (52) mounted on an upper surface of a crank case (51) forming a crank chamber (57) in an inner side thereof, and sucking a pilot air taken from an external portion so as to scavenge; and a scavenging flow passage (70) which is provided in an outer side of the cylinder chamber (56), and communicates the scavenging port and the crank chamber, wherein said scavenging flow passage (70) is constituted by a first scavenging passage (71) which is provided in an outer side of a side wall surface of said cylinder so as to be substantially in parallel to an axis of the cylinder, and a second scavenging flow passage (72) which is provided on an upper surface (58) of said crank case opposing to the first scavenging passage so as to be expanded in a substantially perpendicular direction to the first scavenging passage and has an opening portion (73) communicated with said crank chamber in a terminal portion, and wherein the opening portion and the second scavenging flow passage are formed by: a recess portion (64) which is provided on the upper surface of said crank case, a cylinder base surface (66) of said cylinder which is brought into contact with the upper surface of the crank case, a cylinder skirt portion (67) in a lower portion of a side surface of the cylinder, and a cylinder skirt extended portion (68) which is extended so as to make a portion opposing to the second scavenging passage in the cylinder skirt portion close to or in contact with a bottom surface portion (65) of the recess portion.
- 4. A piston valve type layered scavenging 2-cycle engine as claimed in claim 1, whereinsaid scavenging flow passage (70) is constituted by a first scavenging passage (71) which is provided in an outer side of a side wall surface of said cylinder so as to he substantially in parallel to an axis of the cylinder, and a second scavenging flow passage (72) which is provided on an upper surface of said crank case opposing to the first scavenging passage so as to be expanded in a substantially perpendicular direction to the first scavenging passage, said second scavenging flow passage having an opening portion (73) communicated with said crank chamber in a terminal portion, and the opening portion and the second scavenging passage are formed by: recess portion (64) which is provided on an upper surface of said crank case, a cylinder base surface (66) of said cylinder which is brought into contact with the upper surface of the crank case, a cylinder skirt portion (67) in a lower portion of a side surface of the cylinder, and a cylinder skirt extended portion (68) which is extended so as to make a portion opposing to the second scavenging passage in the cylinder skirt portion close to or in contact with a bottom surface portion (65) of the recess portion.
Priority Claims (2)
Number |
Date |
Country |
Kind |
11-355884 |
Dec 1999 |
JP |
|
2000-006859 |
Jan 2000 |
JP |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/JP00/08788 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO01/44634 |
6/21/2001 |
WO |
A |
Foreign Referenced Citations (4)
Number |
Date |
Country |
51-160721 |
Dec 1976 |
JP |
58-5423 |
Jan 1983 |
JP |
58-146822 |
Oct 1983 |
JP |
WO9857053 |
Dec 1998 |
WO |